Citation SERVICELETTER REASON - Cessna

Citation SERVICE LETTERSL560XL-05-05

TITLETIME LIMITS/MAINTENANCE CHECKS - MSG-3 SCHEDULED MAINTENANCE PROGRAM CHANGEBRIDGING DOCUMENT

EFFECTIVITYMODEL SERIAL NUMBERS

560XL (Citation Excel) -5002 thru -5372 incorporating SL560XL-05-03

560XL (Citation XLS) -5501 thru -5716 incorporating SL560XL-05-03,-5717 thru -5830

560XL (Citation XLS+) -6001 thru -6251

The equivalent of this service document has been incorporated on production airplanes -6252 and On.

REASONTo assist operators with the process of transitioning (bridging) from existing scheduled maintenanceprogram to the new scheduled maintenance program.

DESCRIPTIONThis service letter informs operators of scheduled maintenance and inspection program changes thatmay affect maintenance planning and scheduling. This service letter details improvements to theinspection program that change the base interval from 600 flight hours and/or 12 months to 800 flighthours or 12 months and multiples thereof. The existing Model 560XL Maintenance Manual, Chapter 4and Chapter 5 will be replaced in their entirety.

EXISTING 560XL MAINTENANCE MANUALCHAPTER REVISION

NEW 560XL MAINTENANCE MANUALCHAPTER REVISION

Chapter 4, Revision 13 Chapter 4, Revision 14


Other Inspection Program changes include:

EXISTING PROGRAM NEW PROGRAM38 Chapter 5 Inspection Documents 20 Chapter 5 Inspection Documents

Base interval 600 flight-hours and/or 12 monthswhichever occurs first Base interval 800 flight-hours or 12 months

Chapter 4 tasks duplicated in Chapter 5

Chapter 4 tasks are not duplicated in Chapter5. Added 4-10-01 table for all AirworthinessLimitations (same format as 5-10-01). Added4-12-00 airworthiness limitations inspection

documents (same format as 5-12-00)

4-11-00 and 5-11-00 Component Time LimitsDeleted 4-11-00 and 5-11-00, and added 4-10-01,Table 3 Component Time Limit tasks, and 5-10-01,

Table 2 Component Time Limit tasks

Inspection scheduling tolerance Added +/- 25 flight-hours, or +/-1 months, or +/- 25landings for all Chapter 5 and most Chapter 4 tasks

SL560XL-05-05August 8, 2018 of 12

Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States

in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991

COPYRIGHT © 2018

SL560XL-05-05 August 8, 2018


OTHER CHAPTER 5 IMPROVEMENTS ADDED OR CHANGED5-00-00 Chapter Contents Changed

5-10-00 Added Maintenance PlanningDocument (MPD) Added

5-10-01 Lists MSG-3 Derived Tasks Only Changed

5-10-02 Systems, APU, and Powerplant Tasks Added

5-10-03 Structures Tasks Added

5-10-04 Zonal Tasks Added

5-10-05 Enhanced Zonal Analysis Procedure(EZAP) Tasks Added

5-10-06 Lightning/High Intensity RadiatedFields (L/HIRF) Tasks Added

5-12-00 Added tables listing all inspectionrequirements (Including MSG-3-derived

Tasks and Inspection Documents, RegulatoryInspections/Time Limits, Airworthiness Directives,ICA Supplements, STC’s, SLs And SBs, Etc.) for

default CESCOM/CAMP Systems set-up.

Changed

5-13-00 Regulatory Inspections/Time Limits Added

5-14-00 Airworthiness Directives Added

5-15-00 Instructions for Continued Airworthiness(ICA) Supplements Added

5-16-00 Supplemental Type Certificates (STC) Added

5-17-00 Service Letters and Service Bulletins Added

5-18-00 Supplier Information Added

5-19-00 Discretionary Maintenance Added

COMPLIANCEINFORMATIONAL. This service document is for informational purposes only.

REFERENCESCessna Model 560XL Maintenance Manual

NOTE: A PDF copy of the existing Cessna Model 560XL Maintenance Manual, Chapter 4 (Revision 13)and Chapter 5 (Revision 44) are attached to this Service Letter to assist in the bridging process.

PUBLICATIONS AFFECTEDCessna Model 560XL Maintenance Manual

ACCOMPLISHMENT INSTRUCTIONS1. Implementation of the new inspection program involves understanding the new program changes. Table 1

and Table 2 below summarize the changes to the inspection program framework.

2. The following general information is applicable to the bridging document, which details changes from theexisting scheduled maintenance program to the new scheduled maintenance program.

A. CESCOM/CAMP Systems airplane records will automatically be updated to show projectedmaintenance coming due (associated to this change).


B. All added and changed tasks are due at intervals published in the Model 560XL MaintenanceManual, Chapter 4, Revision 14, and Chapter 5, Revision 45.

C. Deleted tasks and task changes that do not require any specific implementation changes havebeen omitted from the bridging document below for simplicity. This change replaces the existingairframe inspection program in its entirety.

D. Table 2. Pratt & Whitney Engine Inspection Program Change Summary – Bridging Documentbelow provides the changes to the Pratt & Whitney Engine Periodic Inspection Program andassociated New Inspection Document Interval Bridging Rule column. Deleted tasks and taskchanges that do not require any specific implementation procedures have been omitted from thebridging document for simplicity. The new tasks and intervals are currently published in the Pratt &Whitney Maintenance Manuals 30J1272 (PW545A), 30J2242 (PW545B), and 30J2302 (PW 545C),Chapter 5-20-00 Scheduled Maintenance Checks.

E. For additional explanation of this service letter or the bridging document below, contact TextronAviation, Maintenance Engineering, Department 753, 2121 South Hoover Road, Wichita, Kansas67209, Phone: 316-517-9370, email: [email protected].

Table 1 - Inspection Program Change Summary – Bridging Document

EXIST-ING IN-SPEC-TIONDOCU-MENT #

EXISTINGINTERVAL

NEWIN-

SPEC-TIONDOCU-MENT #

NEWINTERVAL

NEW INSPECTION DOCUMENTINTERVAL BRIDGING RULE

EFFECTIV-ITY

5-92-025-92-35 12 months 5-12-01 12 months

Set new ID 5-12-01 due time sameas previous ID 5-92-02 or ID 5-92-35

(whichever is due first)-5001 and

On

5-92-27 600 flight-hours 5-12-02 600 flight-

hoursSet new ID 5-12-02 due time same

as previous ID 5-92-27-5001 and

On

5-92-045-92-36 24 months 5-12-03 24 months

Set new ID 5-12-03 due time sameas previous ID 5-92-04 or ID 5-92-36

(whichever is due first)-5001 and

On

N/A N/A 5-12-04 1,200flight-hours

Set new ID 5-12-04 due 1,200 flight-hoursfrom previous ID 5-92-05

5001 thru-5555 not

incorporatingSB560XL-27-22

5-92-10 48 months 5-12-06 48 months Set new ID 5-12-06 due time sameas previous ID 5-92-10

-5001 andOn



-5001 andOn



-5001 andOn

5-92-1148 monthsthen every24 monthsthereafter

5-12-1148 monthsthen every24 monthsthereafter

Set new ID 5-12-11 due time sameas previous ID 5-92-11

-5001 andOn

5-92-38 60 months 5-12-12 60 months Set new ID 5-12-12 due 60 monthsfrom previous ID 5-92-02

-5001 andOn

SL560XL-05-05August 8, 2018

SL560XL-05-05 August 8, 2018



EXISTINGINTERVAL

NEWIN-


NEWINTERVAL


EFFECTIV-ITY

5-92-13 72 months 5-12-13 72 monthsSet new ID 5-12-13 due 72 months fromprevious ID 5-92-14 - if airworthiness is

72-95 months, due time at next ID 5-12-01-5001 and

On

5-92-51

500 vaporcyclecoolingsystem

compressor-hours

5-12-15

500 vaporcyclecoolingsystem

compressor-hours


-5001thru -5249incorporatingvapor cyclecooling

5-92-14 96 months 5-12-16 96 months Set new ID 5-12-16 due time sameas previous ID 5-92-14

-5001 andOn

N/A N/A 5-12-17

6,000 flight-hours, thenevery 1,600flight-hoursthereafter

Set new ID 5-12-17 due time at 6,000flight-hours - if above 6,000 flight-hours,due time at 1,600 flight-hours from

previous ID 5-92-05

-5001 andOn



as previous ID 5-92-24

-5001 thru-5196 not

incorporatingSB560XL-76-03



as previous ID 5-92-25-5001 and

On

5-92-23

100 flight-hours or12 months,whicheveroccurs first

5-12-20



Note: The inspection interval canbe adjusted after the water loss per

cell is established.

-5001 andOn with

Ni-Cad mainbattery

5-92-47

600 flight-hours or12 months,then 200flight-hoursor 3months

5-12-21


Set new ID 5-12-21 due 600 flight-hoursor 12 months, whichever occurs first

from previous ID 5-92-47

-5001 andOn withlead-acid

main battery



-5001 andOn



-5001 andOn

5-92-MB

3,000flight-hoursthen every1,500 flight

hours

4-12-MB3,000 flight-hours, thenevery 1,500flight-hours

Set new ID 4-12-MB due time sameas previous ID 5-92-MB

-5001 thru-5060



EXISTINGINTERVAL

NEWIN-


NEWINTERVAL


EFFECTIV-ITY

5-92-MD

6,000flight-hoursor ten yearswhicheveroccurs first,then every2,400

flight-hoursor ten yearswhicheveroccurs firstthereafter

4-12-MD6,000 flight-hours, thenevery 2,400flight-hours

Set new ID 4-12-MD due time sameas previous ID 5-92-MD

-5001 andOn

5-92-ME 15,000flight-hours 4-12-ME 15,000

flight-hoursSet new ID 4-12-ME due time same

as previous ID 5-92-ME-5001 and

On

5-92-MF

7,500flight-hours,

then every1,400

flight-hours

4-12-MF7,500 flight-hours, thenevery 1,400flight-hours

Set new ID 4-12-MF due time sameas previous ID 5-92-MF

-5001 andOn

5-92-MG

6,500flight-hours,

then every3,000

flight-hours

4-12-MG6,500 flight-hours, thenevery 3,000flight-hours

Set new ID 4-12-MG due time sameas previous ID 5-92-MG

-5001 thru-5020

5-92-MH

11,000flight-hours,

then every6,000

flight-hours

4-12-MH

11,000flight-hours,then every5,950

flight-hours

Set new ID 4-12-MH due time 5,950flight-hours after the previous ID 5-92-MHNote: Repeat interval has been reduced,however Chapter 4 has a 50 flight-hourtask tolerance for the task(s) in this

inspection document.

-5001 thru-5020

5-92-MI

5,000flight-hours,

then every2,500

flight-hours

4-12-MI5,000 flight-hours, thenevery 2,500flight-hours

Set new ID 4-12-MI due time sameas previous ID 5-92-MI

-5001 thru-5020

5-92-MJ 13,000flight-hours 4-12-MJ 13,000

flight-hoursSet new ID 4-12-MJ due time same

as previous ID 5-92-MJ-5001 thru-5060

5-92-MK

11,500flight-

hours, thenevery 9000flight-hours

4-12-MK

11,500flight-hours,then every9000 flight-

hours

Set new ID 4-12-MK due time sameas previous ID 5-92-MK

-5001 thru-5020

SL560XL-05-05August 8, 2018

SL560XL-05-05 August 8, 2018



EXISTINGINTERVAL

NEWIN-


NEWINTERVAL


EFFECTIV-ITY

5-92-ML

11,500flight-hours,

then every3,300

flight-hours

4-12-ML


flight-hours

Set new ID 4-12-ML due time sameas previous ID 5-92-ML

-5001 andOn

5-92-MM

11,000flight-hours,

then every4,200

flight-hours

4-12-MM

11,000flight-hoursthen every4,150

flight-hours

Set new ID 4-12-MM due time 4,150flight-hours after previous ID 5-92-MM

Note: Repeat interval has been reduced,however Chapter 4 has a 50 flight-hourtask tolerance for the task(s) in this


-5001 andOn

5-92-MN

9,000flight-hours,

then every3,400

flight-hours

4-12-MN9,000 flight-hours thenevery 3,400flight-hours

Set new ID 4-12-MN due time sameas previous ID 5-92-MN

-5001 andOn

5-92-MO

12,500flight-hours,

then every6,100

flight-hours

4-12-MO


flight-hours

Set new ID 4-12-MO due time 6,050flight-hours after previous ID 5-92-MO

Note: Repeat interval has been reduced,however Chapter 4 has a 50 flight-hourtask tolerance for the task(s) in this


-5001 andOn

5-92-MP 300 flight-hours 4-12-MP 300 flight-

hoursSet new ID 4-12-MP due time same

as previous ID 5-92-MP-5001 and

On

5-12-MR

10,000flight-hoursand every5,000

flight-hoursthereafter

4-12-MR

10,000flight-hoursand every5,000

flight-hoursthereafter

Set new ID 4-12-MR due time sameas previous ID 5-12-MR

-5001 thru-5020

N/A N/A 4-12-MS


flight-hours

Set new ID 4-12-MS due 6,700 flight-hours from previous ID 5-92-MJ

-5001 andOn

N/A N/A 4-12-MT


flight-hours

Set new ID 4-12-MT due time sameas previous ID 5-92-ME

-5001 andOn



EXISTINGINTERVAL

NEWIN-


NEWINTERVAL


EFFECTIV-ITY

N/A N/A 4-12-MU


flight-hours

Set new ID 4-12-MU due time sameas previous ID 5-92-ME

-5001 andOn

N/A N/A 4-12-MV


flight-hours

Set new ID 4-12-MV due time sameas previous ID 5-92-ME

-5001 andOn

NOTE: There were no existing Task Numbers or Inspection Documents listed in the Model 560XLMaintenance Manual associated to the Pratt and Whitney Engine.

NOTE: Airplanes -5001 thru -6000, Refer to PWC Pratt & Whitney Maintenance Manuals 30J1272(PW545A) or 30J2242 (PW545B), Chapter 5-20-00 Scheduled Maintenance Checks, asapplicable for all tasks listed in Table 2.

NOTE: Airplanes -6001 and On, Refer to PWC Pratt & Whitney 30J2302 (PW545C), Chapter 5-20-00Scheduled Maintenance Checks for all tasks listed in Table 2.

Table 2 - Pratt & Whitney Engine Inspection Program Change Summary – Bridging Document

MAINTENANCEMANUAL TASK

TITLE

EXIST-ING IN-TERVAL

NEWINTER-VAL

BRIDGING RULE EFFECTIV-ITY

Engine MountGeneral VisualInspection

600engine-hours

800engine-hours

Due 800 engine-hours fromlast compliance of task

-5001 andOn

External EngineGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Compressor InletGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

1. LPCompressorSection

Low PressureCompressor Section(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours

Due 5,000 engine-hoursfrom last compliance of task

-5001 andOn

Compressor Section(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

2. HPCompressorSection

High PressureCompressor Section(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

SL560XL-05-05August 8, 2018

SL560XL-05-05 August 8, 2018



TITLE

EXIST-ING IN-TERVAL

NEWINTER-VAL


Combustion Section(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

3. CombustionSection

Combustion Section(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Turbine Section(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

PerformanceCalibration (5 PointRun) FunctionalCheck

600engine-hours

800engine-hours


-5001 andOn

Acceleration/DecelerationFunctional Check

600engine-hours

800engine-hours


-5001 andOn

4. TurbineSection

Turbine Section(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Engine AccessoryGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

5. AccessoryGearbox

Accessory Gearbox(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Bypass Ducts andFairings GeneralVisual Inspection

600engine-hours

800engine-hours


-5001 andOn

Bypass Section(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

6. BypassSection

Bypass Section(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn



TITLE

EXIST-ING IN-TERVAL

NEWINTER-VAL


Fuel Distribution(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

External TubingGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Flexible TubingGeneral VisualInspection (EnginesNot IncorporatingSB30253)

150engine-hours

150engine-hours


-5001 thru-6000

Fuel Metering andControl ComponentsGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Fuel Oil HeatExchanger GeneralVisual Inspection

600engine-hours

800engine-hours


-5001 andOn

Fuel Filter ElementDetailed Inspection

600engine-hours

800engine-hours


-5001 andOn

Emergency FuelShutoff SystemDetailed Inspection

600engine-hours

800engine-hours


-5001 andOn

Emergency FuelShutoff SystemOperational Check

2,500engine-hours

2,500engine-hours


-5001 andOn

Fuel Filter ElementDiscard

900engine-hours

1200engine-hours

Due 1200 engine-hoursfrom last compliance of task

-5001 andOn

7. FuelDistribution

Fuel Distribution(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Engine WiringHarness GeneralVisual Inspection

600engine-hours

800engine-hours


-5001 andOn

Engine WiringHarness (Cleaning)Restoration

600engine-hours

800engine-hours


-5001 andOn

8. FuelControlling

Fuel Controlling(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

SL560XL-05-05August 8, 2018

SL560XL-05-05 August 8, 2018



TITLE

EXIST-ING IN-TERVAL

NEWINTER-VAL


Ignition ExciterGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Igniters (TipMeasurement)Functional Check(Engines NotIncorporatingSB30340)

300engine-hours

300engine-hours


-5001thru -6000(engines notincorporatingSB30340)

Igniters (TipMeasurement)FunctionalCheck (EnginesIncorporatingSB30340)

600engine-hours

800engine-hours


5001 thru-6000(enginesincorporatingSB30340)

Igniters (TipMeasurement)Functional Check

600engine-hours

800engine-hours


-5001 andOn

Ignition CablesGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Ignition (Engine HSI)Special DetailedInspection

2,500engine-hours

2,500engine-hours


-5001 andOn

Igniters OperationalCheck

600engine-hours

800engine-hours


-5001 andOn

9. Ignition

Ignition (Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn



TITLE

EXIST-ING IN-TERVAL

NEWINTER-VAL


Anti-ice Valve andP3 Anti Ice Tube(Leak Check) GeneralVisual Inspection

600engine-hours

800engine-hours


-5001 andOn

P3 Bellows Seal &Bleed Air TransferTube General VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Bleed Off ValveGeneral VisualInspection

600engine-hours

800engine-hours


-5001 andOn

Air System (EngineHSI) Special DetailedInspection

2,500engine-hours

2,500engine-hours


-5001 andOn

10. Air System

Air System (EngineTBO) Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Engine WiringHarness GeneralVisual Inspection

600engine-hours

800engine-hours


-5001 andOn

Engine IndicatingSpeed Sensor(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

Engine WiringHarness (Cleaning)Restoration

600engine-hours

800engine-hours


-5001 andOn

11. EngineIndicating (N1,N2, and ITT)

Engine IndicatingSpeed SensorSystem (Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

Engine Exhaust(Engine HSI) SpecialDetailed Inspection

2,500engine-hours

2,500engine-hours


-5001 andOn

Emergency Fuel ShutOff Lever and CableDetailed Inspection

900engine-hours

1600engine-hours

Due 1600 engine-hoursfrom last compliance of task

-5001 andOn

12. EngineExhaust

Engine Exhaust(Engine TBO)Restoration

5,000engine-hours

5,000engine-hours


-5001 andOn

3. Make an entry in the airplane logbook stating that this service letter was used as a guide to change fromthe maintenance and inspection program changes in the following documents:

SL560XL-05-05August 8, 2018

SL560XL-05-05 August 8, 2018


EXISTING 560XL MAINTENANCE MANUALCHAPTER REVISION

NEW 560XL MAINTENANCE MANUALCHAPTER REVISION



NOTE: Textron Aviation recommends that compliance with all service documents is reported to CampSystems International.• Complete a record of compliance. (Maintenance Transaction Report, Log Book Entry, or

other record of compliance.)• Put a copy of the completed record of compliance in the airplane logbook.• Send a copy of the completed record of compliance to: Camp Systems International

Incorporated, 8201 East 34th Street North, Building 1100 Suite 1101 Wichita, KS 67226.

MATERIAL INFORMATIONNo parts are required to complete this service document.

CESSNA AIRCRAFT COMPANYMODEL 560XL

MAINTENANCE MANUAL

CHAPTER

AIRWORTHINESSLIMITATIONS

THE AIRWORTHINESS LIMITATIONS SECTION IS FAA APPROVED AND GIVES INSPECTIONS ANDMAINTENANCE THAT ARE REQUIRED BY PARTS 43.16 AND 91.403 OF TITLE 14 OF THE CODE OF FEDERALREGULATIONS, UNLESS AN ALTERNATIVE PROGRAM HAS BEEN FAA APPROVED.

22 APRIL 1998REVISION 13 23 APRIL 2012


MAINTENANCE MANUAL

LIST OF EFFECTIVE PAGES

CHAPTER-SECTION-SUBJECT PAGE DATE

04-List of Effective Pages

04-Record of Temporary Revisions

04-Contents

4-00-00 Page 1 Apr 23/2012

4-10-00 Pages 1-2 Apr 23/2012

4-11-00 Pages 1-2 Apr 23/2012

4-11-02 Pages 1-2 Apr 23/2012

4 - LIST OF EFFECTIVE PAGES Page 1 of 1© Cessna Aircraft Company Apr 23/2012

CESSNA AIRCRAFT COMPANYMAINTENANCE MANUAL

RECORD OF TEMPORARY REVISIONS

Temporary RevisionNumber Page Number Issue Date By Date Removed By


MAINTENANCE MANUAL

CONTENTS

AIRWORTHINESS LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-00-00 Page 1Scope. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-00-00 Page 1Definition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-00-00 Page 1Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-00-00 Page 1

INSPECTION TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-10-00 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-10-00 Page 1Structural Inspection Schedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-10-00 Page 1

REPLACEMENT TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11-00 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11-00 Page 1Replacement Schedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11-00 Page 1

RUSSIAN-CERTIFIED AIRPLANES REPLACEMENT TIME LIMITS . . . . . . . . . . . . . . . . . . 4-11-02 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11-02 Page 1Replacement Schedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11-02 Page 1

4 - CONTENTS Page 1 of 1© Cessna Aircraft Company Apr 23/2012


MAINTENANCE MANUAL

AIRWORTHINESS LIMITATIONS

1. Scope

A. This chapter outlines the mandatory replacement times and inspection intervals for componentsand airplane structures considered to be life limited, or to require monitoring through scheduledinspections. This chapter applies to items such as fatigue components and structures which areconsidered a part of the certification process.

NOTE: The Airworthiness Limitations section is FAA Approved and specifies inspection andmaintenance required under Parts 43.16 and 91.409 of Title 14 of the Code of FederalRegulations, unless an alternative program has been FAA approved.

2. Definition

A. This chapter contains two sections as outlined below.(1) Inspection Time Limits (4-10-00) describes and lists systems and components which are required

to be inspected at specified intervals. The intervals specified represent the maximum timeallowable between inspections.

(2) Replacement Time Limits (4-11-00) describes and lists life limited components which are to bereplaced at a specific time.

(3) Russian-Certified Airplanes Replacement Time Limits (4-11-02) describes and lists life limitedcomponents which are to be replaced at a specific time on airplanes that are certified in Russia.

3. Limitations

A. Composite Control Surface Paint Colors(1) The upper surface of flaps must have a color of paint having a reflectance value of 26 or greater.

For additional information, refer to Chapter 20, Exterior Finish - Cleaning/Painting.

4-00-00 Page 1© Cessna Aircraft Company Apr 23/2012


MAINTENANCE MANUAL

INSPECTION TIME LIMITS

1. General

A. Inspection time limits apply to the systems and components presented in this section and are themaximum inspection limits.

2. Inspection Schedule

NOTE: The following locations require an initial and recurring inspection. Detailed inspection andmaintenance check procedures are described in the associated tasks elsewhere in this manual.

NOTE: Inspection intervals, unless otherwise indicated, are for initial inspection. Intervals for recurringinspections are being evaluated and will be published as determined.

A. Air Conditioning (Chapter 21)(1) Vapor Cycle Cooling System Hourmeter Check (Compressor Motors 1134104-1, -5) - Examine

every 300 hours. Refer to Task 21-52-00-210.

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and Component MaintenanceManual 21-00-06.

B. Fuselage (Part Number 6610000-1) (Chapter 53)(1) Upper Skin from right stringer 13 to left stringer 13 - Inspect at 13,000 hours. Task 53-30-01-210.(2) Lower Skin from right stringer 13 to left stringer 13 - Inspect at 15,000 hours. Task 53-30-01-210.(3) Upper Skin Splice at BL 0 - Inspect at 15,000 hours. Task 53-30-01-251(4) Lower Skin Splices at Stringer 13 - Inspect at 15,000 hours. Task 53-30-01-252(5) Forward Pressure Bulkhead - Inspect at the first 6000 hours or 10 years, whichever occurs first,

and then every 2400 hours or 10 years, whichever occurs first thereafter. Task 53-10-11-251(6) Aft Pressure Bulkhead - Inspect at 15,000 hours. Task 53-10-11-252(7) Cabin Door - Inspect at 15,000 hours. Task 52-10-00-210(8) Escape Hatch - Inspect at 15,000 hours. Task 52-20-00-210

C. Vertical Stabilizers (Part Number 6631000-20) (Chapter 55)

NOTE: Inspect the following vertical stabilizer structure components for Airplanes -5001 thru-5020.

(1) Vertical Stabilizer Forward Spar Strap at WL 150 - Inspect at the first 11,500 hours and thenevery 9000 hours thereafter. Task 55-30-01-253

(2) Vertical Stabilizer Forward Spar Strap at WL 188 - Inspect at the first 10,000 hours and thenevery 5000 hours thereafter.

(3) Vertical Stabilizer Rear Spar Cap at WL 146 - Inspect at the first 6500 hours and then every3000 hours thereafter. Task 55-30-01-250.

(4) Vertical Stabilizer Rear Spar Nested Angle at WL 146 - Inspect at the first 11,000 hours and thenevery 6000 hours thereafter. Task 55-30-01-251.

(5) Vertical Stabilizer Rear Spar Strap at WL 146 - Inspect at the first 5000 hours and then every2500 hours thereafter. Task 55-30-01-252.

D. Wings (Part Number 6622100-1) (Chapter 57)(1) Lower Wing Main Spar Skin Splice at WS 11.50 - Inspect at the first 11,500 hours and then every

3300 hours thereafter. Task 57-10-00-251 and Task 57-10-00-271(2) Lower Wing Main Spar Lower Skin Splice at WS 22.50 - Inspect at the first 7500 hours and then

every 1400 hours thereafter. Task 57-10-00-250 and Task 57-10-00-270.(3) Lower Wing Main Spar at WS 114.57 - Inspect at the first 11,000 hours and then every 4200

hours thereafter. Task 57-10-00-252.(4) Lower Wing Main Spar at WS 131.07 - Inspect at the first 9000 hours and then every 3400 hours

thereafter. Task 57-10-00-252(5) Lower Wing Main Spar at WS 149.57 - Inspect at the first 12,500 hours and then every 6100

hours thereafter. Task 57-10-00-252



MAINTENANCE MANUAL

E. Power Plant (Items below are part of the Fuselage Structure Assembly Part Number 6610000-1)(Chapter 71)

NOTE: Inspect the following engine support structure for Airplanes -5001 thru -5060.

(1) Aft Engine Beam visual inspection - Inspect at the first 3000 hours and then every 1500 hoursthereafter. Task 71-22-00-210

(2) Forward Engine Beam, upper angles, horizontal cap flange, at BL 30.5 thru BL 42.0 - Inspect at13,000 hours.

F. Engine Controls (Chapter 76)(1) On Airplanes -6001 and On, complete a Time Limited Dispatch (TLD) Operational Check at a

periodic interval, not to exceed 170 flight hours. The repair of any detected faults found betweeninspections may be deferred until the end of the interval and the airplane can be dispatched withfaults until the end of the interval. Refer to Task 76-16-00-710.

NOTE: TLD faults, inspection intervals and dispatch limitations are defined by the PW545CEngine Maintenance Manual, Airworthiness Limitations section. The tasks andintervals specified are mandatory and cannot be changed, escalated or deletedwithout concurrence of the responsible Aircraft Certification Office (ACO).



MAINTENANCE MANUAL

REPLACEMENT TIME LIMITS

1. General

A. The following life-limited components are to be replaced at the specified time. It is recommendedthat the components be scheduled for replacement during the airplane's inspection interval coincidingwith, or occurring just before the expiration of the specified time limit. Procedures for replacement ofthe components are described in the applicable chapters in this Maintenance Manual.

2. Replacement Schedule

A. Air Conditioning (Chapter 21)(1) Compressor Drive Motor Brushes (Compressor Motors 1134104-1, -5) - Replace every 500

compressor hours.


B. Flight Controls (Chapter 27)(1) Inboard and Outboard Flap Rollers (Part Number S3049-5F8) - Replace every 5000 landings.

C. Landing Gear (Chapter 32)(1) Main Landing Gear

NOTE: Attaching hardware (bolts, bearings, bushings, trunnion pins, and trunnion/link pinsrelated to the installation of the components given below) is replaced whenever therelated component is replaced. Refer to the applicable section in Chapter 32 for moreinformation.

(a) Trunnion Subassembly1 Left Trunnion Subassembly (Part Number 6641640-5) - Replace every 7600 landings.2 Right Trunnion Subassembly (Part Number 6641640-6) - Replace every 7600

landings.3 Left Trunnion Subassembly (Part Number 6641640-39) - Replace every 7300

landings.4 Right Trunnion Subassembly (Part Number 6641640-40) - Replace every 7300

landings.5 Left Trunnion Subassembly (Part Number 6641630-5) - Replace every 6900 landings.6 Right Trunnion Subassembly (Part Number 6641630-6) - Replace every 6900

landings.7 Left Trunnion Subassembly (Part Number 6641630-27, 39, 41) - Replace every

33,300 landings.8 Right Trunnion Subassembly (Part Number 6641630-28, 40, 42) - Replace every

33,300 landings.(b) Trailing Link Assembly

1 Left Trailing Link Assembly (Part Number 6641640-15) - Replace every 6400landings.

2 Right Trailing Link Assembly (Part Number 6641640-16) - Replace every 6400landings.

3 Left Trailing Link Assembly (Part Number 6641648-1, -7) - Replace every 6400landings.

4 Right Trailing Link Assembly (Part Number 6641648-2, -8) - Replace every 6400landings.

5 Left Trailing Link Assembly (Part Number 6641648-9, -15) - Replace every 40,300landings.

6 Right Trailing Link Assembly (Part Number 6641648-10, -14) - Replace every 40,300landings.

7 Left Trailing Link Assembly (Part Number 6641530-1) - Replace every 33,300landings.



MAINTENANCE MANUAL

8 Right Trailing Link Assembly (Part Number 6641530-2) - Replace every 33,300landings.

(c) Oleo Assembly1 Oleo Assembly (Part Number 6641615-3, -4), except the part that follows - Replace

every 38,000 landings.a Oleo Upper Cap (Part Number 6641616-3) - Replace every 4600 landings.

2 Oleo Assembly (Part Number 6641615-5, -6, -7), except the part that follows -Replace every 38,000 landings.a Oleo Upper Cap (Part Number 6641616-4, -5) - Replace every 14,900 landings.

(d) Actuator Assembly1 Left Actuator Assembly (Part Number 9912537-1, -3, -5) - Replace every 70,200

landings.2 Right Actuator Assembly (Part Number 9912537-2, -4, -6) - Replace every 70,200

landings.(e) Trailing Link Spacer

1 Trailing Link Spacer (Part Number 6641618-9, -12) - Replace every 6200 landings.2 Trailing Link Spacer (Part Number 6641533-1, -2) - Replace every 33,300 landings.

(2) Nose Landing Gear


(a) Nose Landing Gear Assembly (Part Number 6642610-3) - Replace every 33,300 landings.(b) Nose Landing Gear Assembly (Part Number 6642614-1) - Replace every 33,300 landings.(c) Nose Landing Gear Assembly (Part Number 6642625-1, -5, -6, -8, -10, -12, -14) - Replace

every 33,300 landings.(d) Nose Landing Gear Actuator (Part Number 9912491-2, -3, -4 -5, -6) - Replace every 33,300

landings.

D. Fuselage (Chapter 53)(1) Trunnion Attach Fitting Assemblies

(a) Left Nose Landing Gear Trunnion Support Assembly (Part Number 6613020-1, -55, -63) -Replace every 25,500 landings.

(b) Right Nose Landing Gear Trunnion Support Assembly (Part Number 6613020-2, -56, -64)- Replace every 25,500 landings.

(2) Actuator Fitting Assemblies(a) Actuator Fitting Assembly on Airplanes 560-5001 thru 560-5500, (Part Number 6211191-2,

-3) - Replace every 25,500 landings.(b) Actuator Fitting Assembly on Airplanes 560-5501 and On, (Part Number 6611591-9, -10)

- Replace every 25,500 landings.

E. Wing (Chapter 57)(1) Trunnion Attach Fitting Assemblies

(a) Left Forward Fitting Assembly (Part Number 6622123-1, -5) - Replace every 23,800landings.

(b) Right Forward Fitting Assembly (Part Number 6622123-2, -6) - Replace every 23,800landings.

(c) Left Aft Fitting Assembly (Part Number 6622124-1, -5) - Replace every 23,800 landings.(d) Right Aft Fitting Assembly (Part Number 6622124-2, -6) - Replace every 23,800 landings.

(2) Actuator Attach Fitting Assemblies(a) Left Actuator Attach Fitting Assembly (Part Number 6621125-1, -5, -9) - Replace every

23,800 landings.(b) Right Actuator Attach Fitting Assembly (Part Number 6621125-2, -6, -10) - Replace every

23,800 landings.



MAINTENANCE MANUAL

RUSSIAN-CERTIFIED AIRPLANES REPLACEMENT TIME LIMITS

1. General

A. The following life-limited components are to be replaced at the specified time. It is recommendedthat the components be scheduled for replacement during the airplane's inspection interval coincidingwith, or occurring just before the expiration of the specified time limit. Procedures for replacement ofthe components are described in the applicable chapters in this Maintenance Manual.

2. Replacement Schedule

A. Air Conditioning (Chapter 21)(1) Compressor Drive Motor Brushes (Compressor Motors 1134104-1, -5) - Replace every 500

compressor hours.


B. Flight Controls (Chapter 27)(1) Inboard and Outboard Flap Rollers (Part Number S3049-5F8) - Replace every 5000 landings.

C. Landing Gear (Chapter 32)(1) Main Landing Gear


















MAINTENANCE MANUAL




2 Oleo Assembly (Part Number 6641615-5, -6, -7), except the part that follows -Replace every 22,800 landings.a Oleo Upper Cap (Part Number 6641616-4, -5) - Replace every 8900 landings.









landings.

D. Fuselage (Chapter 53)(1) Trunnion Attach Fitting Assemblies




-3) - Replace every 15,300 landings.(b) Actuator Fitting Assembly on Airplanes 560-5501 and On, (Part Number 6611591-9, -10)

- Replace every 15,300 landings.

E. Wing (Chapter 57)(1) Trunnion Attach Fitting Assemblies






14,300 landings.


REVISION

MODEL 560XLMAINTENANCE MANUAL

CHAPTER 5REVISION 441 OCTOBER 2017

56XCH5-44

Please replace Chapter 5.

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PROGRAM CHANGE SUMMARY

1. General

A. This section gives a list of changes that were made to the inspection program during Revision 44. Thislist gives Operators and Maintenance Personnel a record of the changes to the inspection programand is for information only.

2. Chapter 5 Changes

A. Changes made to Chapter 5 topics are as follows.(1) 5-90-01 MSG-3 Inspection Time Limits

(a) Added Item Code B262014(2) 5-92-38 Inspection Document 38

(a) Created new Inspection Document for inspections completed every 5 years in accordancewith (IAW) the manufacturer's instructions.

(b) Added Item Code B262014

B. Changes to Tasks(1) The following Inspection Tasks were changed in this revision.

Task Number Task Title Status

12-19-02-160 Water Separator Restoration (Cleaning) Revised

12-21-01-641Horizontal Stabilizer Actuator Reservoir Oil LeakageAcceptance Criteria and Oil Level Check

Revised

12-21-01-642Lubricate Horizontal Stabilizer Scissor Fitting Bolts and AftPivot Bolts

Revised

12-21-02-640 Nose Landing Gear Lubrication Revised

12-90-20-641 Landing Gear System Lubrication Revised

22-11-01-220Aileron, Rudder, and Elevator Autopilot Servo CablesInspection

Revised

23-11-00-210 High Frequency Antenna and Tension Unit Inspection Revised

24-90-50-721 Ni-Cad Battery (Saft) Functional Check (Capacity Check) Revised

24-90-50-722 Ni-Cad Battery (Marathon) Functional Check (Capacity Check) Revised

26-90-20-723 Optional Aft Vanity Fire Extinguisher Bottle Functional Check(Weight Check)

Added

27-90-10-721 Aileron and Aileron Trim Tab Control System Functional Check Revised

27-90-20-721 Rudder and Rudder Trim Control System Functional Check Revised

27-90-40-720 Two-Position Horizontal Stabilizer Functional Check Revised

32-30-08-210 Emergency Gear Extension System Cable Inspection Revised

32-42-00-901 Hydraulic Pack Assembly Filter Replacement Revised

32-42-00-902 Brake Reservoir Air Filter Replacement Revised

32-42-00-710 Antiskid System Functional Test Revised

32-44-00-961 Hydraulic Pump Assembly Filter Replacement Revised

32-44-00-960 Vent Filter Element Replacement Revised

32-44-00-710 Antiskid System Functional Test Revised

32-50-00-730 Nose Wheel Steering Control Cables Inspection/Check Revised

INSPECTION PROGRAM CHANGE SUMMARY Page 1© TEXTRON AVIATION INC. Oct 1/2017

CESSNA®MODEL 560XL

MAINTENANCE MANUAL


32-90-40-210External Zonal Inspection of the Nose and Main Landing GearWheel Wells

Revised

32-90-40-960 Brake System Filters Discard (Airplanes -5501 and On) Revised

34-11-09-710 Air Data Systems Check Revised

34-90-10-210Pitot-Static System Functional Check (Airplanes -5001 thru-6000)

Revised

35-01-00-710 Passenger Oxygen System Functional Check Revised

53-10-10-211 Radome Surface Mounted Lightning Diverter Strips Inspection Revised

53-10-11-210 Inspect Fuselage Internal Components Revised

53-10-11-251 Forward Pressure Bulkhead Inspection (Eddy Current) Revised

53-10-12-210 Inspect Aft Tailcone Components Revised

53-10-12-211 Inspect Forward Tailcone Components. Revised

53-30-01-250Fuselage External Surface Special Detailed Inspection (EddyCurrent)

Revised

53-30-01-251 Upper Skin Splice at BL 0.00 Inspection (Eddy Current) Revised

53-30-01-252 Lower Skin Splice at Stringer 13 Inspection (Eddy Current) Revised

53-90-00-211 External Zonal Inspection of the Fuselage Revised

53-90-00-212 Internal Zonal Inspection of the Cabin Section Revised

53-90-00-213 Internal Zonal Inspection of the Cockpit Below Floorline Revised

53-90-00-214 Internal Zonal Inspection of the Cockpit Above Floorline Revised

53-90-00-215 Internal Zonal Inspection of the Tail Section Revised

53-90-00-216 Internal Zonal Inspection of the Nose Section Revised

53-90-00-217 Internal Zonal Inspection of the APU in the Tail Section Revised

53-90-10-210 Internal Zonal Inspection of the Empennage Revised

53-90-10-211 External Zonal Inspection of the Empennage Revised

53-90-50-210 Internal Zonal Inspection of the Fuselage Fairing Revised

54-50-10-250Forward Engine Beam, Upper Angles, Horizontal Cap Flangeat BL 30.5 to BL 42.0 Special Detailed Inspection (EddyCurrent)

Revised

55-10-01-212Horizontal Stabilizer Aft Spar Area General Visual Inspection(Corrosion Inspection)

Revised

57-10-00-210Main Landing Gear Wheel Well General Visual Inspection(Corrosion Inspection)

Revised

57-10-00-211Aft Wing Spar Area General Visual Inspection (CorrosionInspection)

Revised

57-10-00-250 Lower Wing Main Spar Lower Skin Splice at WS 22.50 (EddyCurrent Inspection)

Revised

57-10-00-251 Lower Wing Main Spar Skin Splice Flange at WS 11.50 (EddyCurrent Inspection)

Revised


CESSNA®MODEL 560XL

MAINTENANCE MANUAL


57-10-00-252Lower Wing Main Spar at WS 114.57, WS 131.07, or WS149.57 (Eddy Current Inspection)

Revised

57-10-00-270 Lower Wing Main Spar Lower Skin Splice at WS 22.50(Ultrasonic Inspection)

Revised

57-10-00-271 Lower Wing Main Spar and Skin Splice at WS 11.50 (UltrasonicInspection)

Revised

57-90-00-210 External Zonal Inspection of the Wings Revised

71-00-00-210 Engine General Inspection Revised

71-90-00-210 Internal Zonal Inspection of the Engines and Pylons Revised

71-90-00-211 External Zonal Inspection of the Engines and Pylons Revised


Maintenance ManualChapter 5

Time Limits/Maintenance Checks

MODEL 560XL(560XL -5001 THRU -5500)(560XL -5501 THRU -6000)

(560XL -6001 AND ON)

Member of GAMA

FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN.

COPYRIGHT © 1998TEXTRON AVIATION INC.WICHITA, KANSAS, USA 6 APRIL 1998

56XCH5-44 REVISION 44 1 OCTOBER 2017

CHAPTER

5TIME LIMITS/

MAINTENANCECHECKS

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

LIST OF EFFECTIVE PAGES

CHAPTER-SECTION-SUBJECT PAGE DATE

05-Title05-List of Effective Pages Pages 1-3 Oct 1/201705-Record of Temporary Revisions05-Contents Pages 1-8 Oct 1/20175-00-00 Pages 1-4 Apr 1/20105-10-00 Pages 1-5 Apr 1/20175-10-01 Pages 1-19 Apr 1/20175-11-00 Pages 1-5 Jul 1/20165-12-00 Pages 1-7 Apr 1/20105-12-01 Pages 1-2 Jul 1/20155-12-02 Pages 1-2 Jul 1/20155-12-03 Page 1 Jul 1/20125-12-04 Pages 1-2 Jul 1/20155-12-0B Pages 1-2 Jul 1/20155-12-05 Pages 1-7 Jul 1/20155-12-06 Page 1 DELETED5-12-07 Page 1 Apr 1/20095-12-08 Page 1 Apr 1/20095-12-09 Page 1 Apr 1/20095-12-18 Pages 1-2 Jul 1/20165-12-20 Page 1 Jan 1/20145-12-21 Page 1 Jan 1/20155-12-22 Page 1 DELETED5-12-23 Page 1 DELETED5-12-28 Page 1 Jan 1/20155-12-30 Page 1 Apr 1/20095-12-49 Page 1 Apr 1/20095-12-51 Page 1 Apr 1/20095-12-52 Page 1 Apr 1/20095-12-53 Page 1 Apr 1/20095-12-58 Page 1 Apr 1/20095-12-59 Page 1 Jul 1/20155-12-60 Page 1 Apr 1/20095-12-63 Pages 1-2 Apr 1/20175-12-66 Page 1 Apr 1/20095-12-67 Page 1 Apr 1/20095-12-68 Page 1 Apr 1/20165-12-69 Page 1 Apr 1/20135-12-70 Page 1 Jan 1/20145-12-71 Page 1 Apr 1/20165-12-MB Page 1 Oct 1/20115-12-MD Page 1 Apr 1/20135-12-ME Page 1 Apr 1/20095-12-MF Page 1 Apr 1/2009

05 - LIST OF EFFECTIVE PAGES Page 1 of 3© TEXTRON AVIATION INC. Oct 1/2017

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

5-12-MG Page 1 Oct 1/20105-12-MH Page 1 Oct 1/20105-12-MI Page 1 Oct 1/20105-12-MJ Page 1 Oct 1/20115-12-MK Page 1 Oct 1/20105-12-ML Page 1 Apr 1/20095-12-MM Page 1 Apr 1/20095-12-MN Page 1 Apr 1/20095-12-MO Page 1 Apr 1/20095-12-MP Page 1 Jul 1/20125-12-MQ Page 1 Apr 1/20135-19-00 Pages 1-2 Oct 1/20175-50-00 Pages 1-10 Apr 1/20175-90-00 Pages 1-9 Apr 1/20175-90-01 Pages 1-20 Oct 1/20175-91-00 Pages 1-5 Jul 1/20165-92-00 Pages 1-4 Apr 1/20105-92-01 Pages 1-2 Apr 1/20105-92-02 Pages 1-2 Jul 1/20165-92-03 Page 1 Apr 1/20125-92-04 Pages 1-2 Jan 1/20155-92-05 Page 1 Apr 1/20135-92-06 Page 1 Apr 1/20095-92-07 Page 1 Apr 1/20095-92-08 Pages 1-2 Apr 1/20095-92-09 Page 1 Apr 1/20095-92-10 Pages 1-2 Oct 1/20115-92-11 Page 1 Apr 1/20095-92-12 Page 1 Apr 1/20095-92-13 Page 1 Jul 1/20155-92-14 Pages 1-2 Oct 1/20115-92-15 Page 1 Oct 1/20115-92-16 Page 1 Apr 1/20095-92-17 Page 1 Apr 1/20095-92-18 Page 1 Apr 1/20095-92-19 Page 1 Apr 1/20095-92-22 Page 1 DELETED5-92-23 Page 1 Jan 1/20155-92-24 Page 1 Apr 1/20095-92-25 Page 1 Oct 1/20105-92-26 Page 1 Apr 1/20095-92-27 Page 1 Apr 1/20095-92-30 Page 1 Apr 1/20095-92-34 Page 1 Apr 1/20095-92-35 Page 1 Apr 1/20095-92-36 Page 1 Apr 1/20095-92-37 Page 1 DELETED


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

5-92-38 Page 1 Oct 1/2017

5-92-40 Page 1 Apr 1/2009

5-92-41 Page 1 DELETED

5-92-43 Page 1 Apr 1/2009

5-92-44 Pages 1-2 Apr 1/2017

5-92-45 Page 1 Apr 1/2009

5-92-47 Page 1 Apr 1/2016

5-92-48 Page 1 Apr 1/2016

5-92-50 Page 1 Apr 1/2013

5-92-51 Page 1 Jan 1/2014

5-92-52 Page 1 Apr 1/2016

5-92-MB Page 1 Oct 1/2011

5-92-MD Page 1 Apr 1/2013

5-92-ME Page 1 Apr 1/2009

5-92-MF Page 1 Apr 1/2009

5-92-MG Page 1 Oct 1/2010

5-92-MH Page 1 Oct 1/2010

5-92-MI Page 1 Oct 1/2010

5-92-MJ Page 1 Oct 1/2011

5-92-MK Page 1 Oct 1/2010

5-92-ML Page 1 Apr 1/2009

5-92-MM Page 1 Apr 1/2009

5-92-MN Page 1 Apr 1/2009

5-92-MO Page 1 Apr 1/2009

5-92-MP Page 1 Jul 1/2012

5-92-MQ Page 1 Jul 1/2012

5-92-MR Page 1 Apr 1/2013


CESSNA AIRCRAFT COMPANYMAINTENANCE MANUAL

RECORD OF TEMPORARY REVISIONS

Temporary RevisionNumber Page Number Issue Date By Date Removed By

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

CONTENTS

TIME LIMITS/MAINTENANCE CHECKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 1Scope. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 1Inspection Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 1Maintenance Steering Group - 3 (MSG-3) Scheduled Maintenance Development . 5-00-00 Page 1Continuous Inspection Requirements for Reduced Vertical Separation Minimum

(RVSM) Certified Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 2Continuous Airworthiness Inspection Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 4Supplemental Type Certification Installations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-00-00 Page 4

INSPECTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-00 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-00 Page 1Interval and Phase Cross-Reference for INSPECTION TIME LIMITS: . . . . . . . . . . . . 5-10-00 Page 1Tasks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-00 Page 3Definitions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-00 Page 5

INSPECTION TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-01 Page 1Inspection Items . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10-01 Page 1

COMPONENT TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-11-00 Page 1Component Time Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-11-00 Page 1Schedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-11-00 Page 1

CONTINUOUS INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 1Continuous Airworthiness Inspection Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 1Title 14 of the Code of Federal Regulations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 1Construction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 2Continuous Inspection Program Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 2Inspection Time Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 4Program Startup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 5Logbook Forms, Pilot Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 5Maintenance Transaction Report . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-00 Page 6

INSPECTION PHASE 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-01 Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-01 Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-01 Page 1




INSPECTION PHASE B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-0B Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-0B Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-0B Page 1



05 - CONTENTS Page 1 of 8© TEXTRON AVIATION INC. Oct 1/2017

CESSNA®MODEL 560XL

MAINTENANCE MANUAL



INSPECTION PHASE 18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-18 Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-18 Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-18 Page 1















CESSNA®MODEL 560XL

MAINTENANCE MANUAL






INSPECTION PHASE MB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MB Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MB Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MB Page 1

INSPECTION PHASE MD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MD Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MD Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MD Page 1

INSPECTION PHASE ME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ME Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ME Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ME Page 1

INSPECTION PHASE MF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MF Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MF Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MF Page 1

INSPECTION PHASE MG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MG Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MG Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MG Page 1

INSPECTION PHASE MH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MH Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MH Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MH Page 1

INSPECTION PHASE MI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MI Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MI Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MI Page 1

INSPECTION PHASE MJ. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MJ Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MJ Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MJ Page 1

INSPECTION PHASE MK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MK Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MK Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MK Page 1

INSPECTION PHASE ML. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ML Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ML Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-ML Page 1

INSPECTION PHASE MM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MM Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MM Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MM Page 1


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MN Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MN Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MN Page 1

INSPECTION PHASE MO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MO Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MO Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MO Page 1

INSPECTION PHASE MP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MP Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MP Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MP Page 1

INSPECTION PHASE MQ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MQ Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MQ Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12-MQ Page 1

DISCRETIONARY MAINTENANCE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-19-00 Page 1Scope. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-19-00 Page 1

UNSCHEDULED MAINTENANCE CHECKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 1Unscheduled Maintenance Checks Defined . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 1Hard or Overweight Landing Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 3Overspeed Check (Above 8000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 3Overspeed Check (Below 8000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 3Flap System Overspeed Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 4Landing Gear Assembly Overspeed Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 4Severe Turbulence and/or Maneuver Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 4Inadvertent In-Flight Thrust Reverser Deployment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 5Lightning Strike Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 5Foreign Object Damage Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 6Towing with Large Fuel Unbalance or High Drag/Side Loads Due to Ground

Handling Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 6Airplane Operation Through Deep Standing Water . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 6Nose Landing Gear Tow Limits Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 6Exposure to High Winds While the Aircraft is Parked Check. . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 10Interior Cabin/Tailcone Fluid Spill . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-50-00 Page 10

MSG-3 INSPECTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-00 Page 1General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-00 Page 1Inspection and Document Cross-Reference for Inspection Time Limits: . . . . . . . . . . 5-90-00 Page 1Inspection Time Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-00 Page 6Task Identification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-00 Page 7Definitions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-00 Page 9

MSG-3 INSPECTION TIME LIMITS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-01 Page 1Inspection Items . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-90-01 Page 1

MSG-3 COMPONENT TIME LIMITS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-91-00 Page 1Component Time Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-91-00 Page 1Schedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-91-00 Page 1

MSG-3 CONTINUOUS INSPECTION PROGRAM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 1Purpose and Use . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 1Title 14 of the Code of Federal Regulations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 1Construction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 2Maintenance Manual - Compact Disc - Read Only Memory (CD-ROM). . . . . . . . . . . 5-92-00 Page 2Logbook Forms, Pilot Information. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 2Maintenance Transaction Report . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-00 Page 4


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-01 Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-01 Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-01 Page 1









INSPECTION DOCUMENT 10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-10 Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-10 Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-10 Page 1








CESSNA®MODEL 560XL

MAINTENANCE MANUAL


















CESSNA®MODEL 560XL

MAINTENANCE MANUAL







INSPECTION DOCUMENT MB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MB Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MB Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MB Page 1

INSPECTION DOCUMENT MD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MD Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MD Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MD Page 1

INSPECTION DOCUMENT ME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ME Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ME Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ME Page 1

INSPECTION DOCUMENT MF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MF Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MF Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MF Page 1

INSPECTION DOCUMENT MG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MG Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MG Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MG Page 1

INSPECTION DOCUMENT MH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MH Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MH Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MH Page 1

INSPECTION DOCUMENT MI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MI Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MI Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MI Page 1

INSPECTION DOCUMENT MJ. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MJ Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MJ Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MJ Page 1

INSPECTION DOCUMENT MK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MK Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MK Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MK Page 1

INSPECTION DOCUMENT ML. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ML Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ML Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-ML Page 1


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MM Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MM Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MM Page 1

INSPECTION DOCUMENT MN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MN Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MN Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MN Page 1

INSPECTION DOCUMENT MO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MO Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MO Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MO Page 1

INSPECTION DOCUMENT MP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MP Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MP Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MP Page 1

INSPECTION DOCUMENT MQ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MQ Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MQ Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MQ Page 1

INSPECTION DOCUMENT MR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MR Page 1Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MR Page 1General Inspection Criteria. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-92-MR Page 1


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

TIME LIMITS/MAINTENANCE CHECKS

1. Scope

A. This chapter provides the time limits and maintenance checks for the Model 560XL Airplane. It isdivided into sections, each with a specific purpose toward providing information necessary to establishinspection criteria. Refer to the Description section for detailed information concerning each of thesesections.

NOTE: In accordance with FAR 25.1529, Chapter 4 (Airworthiness Limitations) of this manual ispublished as a separate document. Refer to Chapter 4 for those components having amandatory inspection and/or components replacement schedule.

B. Chapter 4 of this manual is FAA approved and issued separately from the maintenance manual. Someinspection interval and life limit requirements of Chapter 4 may not agree with the current Chapter5. When a conflict is presented between the two chapters, Chapter 4 requirements always takeprecedence. Chapter 5 requirements are brought into conformity with Chapter 4 at the next revisionto the manual.

2. Inspection Requirements

A. Federal Aviation Regulations Part 91.409(e) defines the inspection requirements for turbojetmulti-engine airplanes. The inspection requirements defined in this chapter are the manufacturer'srecommended procedures and are tailored to satisfy the requirements of Part 91.409(e) and (f)(3).

B. For airplanes registered in countries other than the United States, the procedures specified by theAirworthiness Authority of that country should be followed.

C. All nondestructive testing procedures required in this chapter are defined in the Nondestructive TestingManual. These procedures must be performed by personnel and at facilities that have been certifiedby Cessna Aircraft Company. For details of certification program, refer to Nondestructive TestingManual, Part 1, General.

3. Maintenance Steering Group - 3 (MSG-3) Scheduled Maintenance Development

A. The MSG-3 Scheduled Inspection program is for Model 560XL Airplanes -5717 and On, and Model560XL Airplanes -5002 thru -5716 Incorporating SB560XL-05-01.

B. The Cessna MSG-3 group used the concepts of the Air Transport Authority (ATA) MSG-3 to make thetime limits and maintenance checks for the Model 560XL Airplane.(1) An analysis of the airplane's Maintenance Significant Items (MSI) and Structural Significant Items

(SSI) was made by the Cessna MSG-3 Group.(2) Each of these MSI were reviewed by Working Group(s) that had specialist representatives of

operators, Cessna staff, and the regulatory authority.(3) After each MSI was approved by the Working Group, it was then given to an Industry Steering

Committee (ISC). The ISC made sure that the MSG-3 process identified all of the MSI and SSIand whether or not a task was made from the analysis.

(4) The initial scheduled maintenance tasks and intervals have been specified in a MaintenanceReview Board (MRB) report completed by the Cessna MSG-3 Group.

C. Refer to the Citation 560XL/XLS (CE-560XL) Maintenance Review Board Report (MRBR) foradditional information about the Model 560XL MSG-3 Program. The MRBR also has informationabout MSG-3 concepts and methods that maintenance personnel must understand.

4. Continuous Inspection Requirements for Reduced Vertical Separation Minimum (RVSM) CertifiedAirplanes

A. The inspection requirements for RVSM certified airplanes are contained in the regular continuousinspection program. The requirements include those inspections required by FAR 91.411 as definedfor the specific air data computer installed and a verification that the static ports are within tolerances.Refer to Chapter 34, Pitot/Static Systems - Maintenance Practices .

5-00-00 Page 1© TEXTRON AVIATION INC. Apr 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

B. The only special inspection requirement occurs if the airplane has been damaged and repaired,painted or polished/buffed in the static port area. The static ports must be inspected to ensure theyare within the tolerances. Refer to Chapter 34, Pitot/Static Systems - Maintenance Practices .

5. Description

NOTE: Listed below is a detailed description and intended purpose of each section of this chapter.

A. Section 5-00-00, Time Limits/Maintenance Checks - General. This section provides a description andpurpose of each section of this chapter.

B. Section 5-10-01, Inspection Time Limits.(1) This section lists, in chart format, all inspection and servicing requirements which must be

performed. Each page contains the following columns:(a) Revision Status provides the date that a given item was added, deleted or revised. A blank

entry in this column indicates no change since issuance of the manual.1 New inspection requirements and changes to existing inspection requirements

become effective on the revision date of the change. Unless otherwise noted,compliance of a new or revised inspection requirement must be accomplished nolater than the next scheduled interval of the changed item, following receipt of therevision. Unless otherwise noted, an inspection in progress at the time of newrevision becomes effective may be completed, utilizing the inspection criteria ineffect when the inspection was initiated.

(b) Inspection Item Code Number is a seven-digit, alpha-numeric number permanentlyassigned to a scheduled maintenance item. A given inspection item code number willnever change and will not be reused in the event the scheduled maintenance item isdeleted. The alpha character at the beginning of the code can be: A - Indicates inspectionrequirement B - Indicates functional or operational test requirement C - Indicates alubrication requirement D - Indicates a clean/service requirement

(c) Inspection Requirements provide a description of the maintenance item and are listed inchapter order.

(d) Interval indicates the minimum frequency at which the item is to be inspected. As eachoperator establishes his inspection program, these intervals must be adhered to.

(e) Applicable Phase(s) indicates the applicable inspection phase currently containing theinspection item.

(f) Applicable Zone refers to the physical location(s) in the airplane affected by the item. Mostfunctional and operational tests do not list a zone but instead list a code which indicatesspecial conditions required to perform the test. The codes and conditions are as follows:

ENG One or both airplane engines to be running.

AUX External source of electrical, hydraulic or pneumatic power or a combinationof these. Airplane engine power sources should not be used for these tests.(See note below.)

BAT These tests must be performed with the component powered by the airplanesbatteries or the batteries built into the individual component in the case of thestandby gyro, ELT or other components with internal battery power.

LAB Used when special equipment which requires that the component be removedfrom the airplane and taken to a place equipped to perform the check orcalibration.

FLT Test is to be performed during a flight.

NOTE 1: It is possible to perform many of the tests in the AUX category using the airplanes battery power.However, it is not recommended due to the power drain on the batteries.

(2) Primary purpose of the Inspection Time Limits section is to provide a complete listing of allinspection items in an order that allows easy access for the information listed previously.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

C. Section 5-11-00, Component Time Limits.

This section provides a list of overhaul or replacement intervals for components in chapter order.These requirements are not listed in the 5-10-01 Inspection Time Limits section. The componentoverhaul or replacement criteria must be utilized as a guideline for determining proper action regardingthe components listed. These requirements must be worked into the continuous inspection programto provide a complete inspection program.

D. Section 5-12-00, Continuous Inspection Program.

This section outlines the continuous inspection program which is Cessna Aircraft Company'srecommended inspection program. The program is divided into five primary phases which coverall inspection requirements up through the 1200-hour interval inspection items. The remainingphases cover inspections which are at intervals other than what the five primary phases cover. Referto Continuous Inspection Program for a more detailed description of the Continuous InspectionProgram.

E. Section 5-50-00, Unscheduled Maintenance Checks.

This section includes inspections and checks which may be required due to special or unusualcircumstances and do not have regular repetitive intervals for accomplishment.

F. Section 5-90-00, MSG-3 Inspections.(1) This section gives the inspection criteria, a cross-reference for inspection time limits, inspection

time limitations, and task identification.

G. Section 5-90-01, MSG-3 Inspection Time Limits.(1) This section lists, in chart format, all inspection and servicing requirements which are necessary

for the Model 560XL MSG-3 program. Each page contains the following columns:(a) Revision Status provides the date that a given item was added, deleted or revised. A blank

entry in this column indicates no change since issuance of the manual.(b) New inspection requirements and changes to existing inspection requirements become

effective on the revision date of the change. Unless otherwise noted, compliance of a newor revised inspection requirement must be accomplished no later than the next scheduledinterval of the changed item, following receipt of the revision. Unless otherwise noted, aninspection in progress at the time a new revision becomes effective may be completedutilizing the inspection criteria in effect when the inspection was initiated.

(c) Inspection Item Code Number is a seven-digit, alphanumeric number permanentlyassigned to a scheduled maintenance item. A given inspection item code number willnever change and will not be reused in the event the scheduled maintenance item isdeleted. The alpha character at the beginning of the code can be:

A - Indicates inspection requirementB - Indicates functional or operational test requirementC - Indicates a lubrication requirementD - Indicates a clean/service requirement.

(d) Inspection Requirements provide a description of the maintenance item and are listed inchapter order.

(e) Interval indicates the minimum frequency for which the item is to be inspected. As eachoperator establishes his inspection program, these intervals must be adhered to.

(f) CH-SE-SU - shows the inspections and includes both the time interval and method ofinspection.

(g) Applicable Zone refers to the physical location(s) on the airplane affected by the item. Mostfunctional and operational tests do not list a zone but instead list a code which indicatesspecial conditions required to complete the test. The codes and conditions are as follows:1 ENG - One or both airplane engines to be running.

NOTE: It is possible to complete many of the tests in the AUX category usingthe airplane's battery power. However, it is not recommended due tothe power drain on the batteries.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

2 AUX - External source of electrical, hydraulic or pneumatic power or a combinationof these. Airplane engine power sources should not be used for these tests.

3 BAT - These tests must be completed with the component powered by the airplane’sbatteries or the batteries built into the individual component in the case of the ELT orother components with internal battery power.

4 LAB - Used when it necessary because of special equipment requirements that thecomponent be removed from the airplane and taken to a place equipped to completethe check or calibration.

5 FLT - Test is to be completed during a flight.(2) The primary function of the Inspection Time Limits section is to give a complete listing of all

inspection items in an order that allows easy access for the information listed previously.

H. Section 5-91-00, MSG-3 Components Time Limits.(1) This section supplies a list of overhaul or replacement intervals for components in chapter order.

These requirements are not listed in the 5-90-01 MSG-3 Inspection Time Limits section. Thecomponent overhaul or replacement criteria must be used as a guideline for determining properaction regarding the components listed. You must include these requirements in the continuousinspection program to supply a complete inspection program.

I. Section 5-92-00 explains the MSG-3 Continuous Inspection Programs.(1) Each section of 5-92-XX contains the Inspection Document noted by the last two characters of

the chapter/section/subject identification.

6. Continuous Airworthiness Inspection Program

A. Purpose and Use.(1) As detailed in Part 91.409, paragraph (e), of the Federal Aviation Regulations, turbo jet airplanes

must be inspected in accordance with an authorized inspection schedule. This section presentsthe basis for a continuous inspection program for the Model 560XL, recommended by CessnaAircraft Company.

(2) An operator may elect to perform the recommended inspections on a schedule other thanthat specified. Any inspection schedule requiring the various inspection items detailed in thischapter to be performed at a frequency equal to that specified herein or more frequently isacceptable. Any inspection item performed at a time period in excess of that specified hereinmust be approved by the appropriate regulating agency.

7. Supplemental Type Certification Installations

A. Inspection requirements for Supplemental Type Certification (STC) installations are not includedin this manual. When an STC installation is incorporated on the airplane, those portions of theairplane affected by the installation must be inspected in accordance with the inspection programpublished by the owner of the STC. Since STC installations may change systems interface, operatingcharacteristics and component loads or stresses on adjacent structures, Cessna provided inspectioncriteria may not be valid for airplanes with STC installations.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTIONS

1. General

A. General inspection criteria.(1) While doing each of the specific inspections listed in this chapter, additional general inspections

of surrounding areas are to be performed while access is available. These general inspectionsare intended to detect obvious conditions which warrant further action.

(2) When an area is exposed, wire bundles are to be examined for chafing, proper security andsupport. Make sure that wire bundles are not attached to hydraulic tubes or lines.

(3) Inspection items listed are for specific components and systems, however, the entire inspectionprogram requires and expects a high degree of professionalism and judgment by inspectionpersonnel. This will make sure that all components and systems are maintained and examinedto supply the highest safety standards.

(4) If a component or system is disturbed (due to maintenance being performed) after completionof an initially required operational or functional test, then that specific test must be confirmedagain after the completion of any maintenance before returning the system or component toservice. Refer to the appropriate chapter in this Maintenance Manual for removal, installation,operational tests and functional tests of components and/or systems.

(5) Some items or components require lubrication. Refer to Chapter 12, Scheduled Servicing -Description and Operation, for lubricant, lubricating points and method.

(6) Refer to Chapter 6, Airplane Zoning - Description and Operation, for airplane zone definition.(7) Do a preflight inspection after completion of the applicable inspection to make sure all required

items are properly serviced. Refer to the Approved Airplane Flight Manual.(8) For record-keeping purposes, inspection items that are also required for Chapter 4,

Airworthiness Limitations, have been placed in intervals that begin with M. The interval forthese items is defined by Chapter 4 and must be accomplished at or before the listed interval.Chapter 4 items do not have a grace period.

2. Interval and Phase Cross-Reference for INSPECTION TIME LIMITS:

NOTE: Inspection requirements for engine, APU, vapor cycle cooling system, wheels and brakesare defined by component manufacturer. To ensure that the latest inspection requirementsas defined by manufacturer are performed, refer to and perform the requirements at intervalspublished in those inspection documents.

NOTE: A calendar month starts on the first day of the month. All inspections for that interval becomedue by the last day of that month.

A - Phase 6 - Recommended every 14 days for operators who routinely operate or base theirairplane in areas subject to saltwater or other corrosion effects. (Not currentlyused)

B - Phase 7 - Every 300 hours.

D - Phase B - Every 150 hours.

E - Phase 1, 2,3, or 4

- Every 300 hours or 24 calendar months, whichever occurs first.

F - Phase 5 - Every 1200 hours or 36 calendar months, whichever occurs first.

G - Phase 8 - Every 6 calendar months.

H - Phase 9 - Every 900 hours, +50 or -50 hours, or 24 calendar months, whichever occurs first.

I - Phase 28 - Every 100 hours, or 12 calendar months.

J - Phase 30 - Every 600 hours.

K - Phase 18 - Every one year.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

L - Phase 19 - Two years from date of manufacture and every two years thereafter. (Notcurrently used)

M - Phase 20 - Every 24 calendar months as required by 14 CFR 91.411, 91.413 and RVSMcertification. (No grace period.)

N - Phase 21 - Every 2 years.

O - Phase 22 - Every 3 years. (Not currently used)

P - Phase 23 - Every 5 years. (Not currently used)

Q - Phase 48 - Every 6 years. (Not currently used)

R - Phase 47 - Every 12 years. (Not currently used)

S - Phase 11 - Every 3 to 6 calendar months. (Not currently used)

T - Phase 51 - Every 2400 hours.

U - Phase 52 - Every 600 hours or 12 calendar months whichever occurs first and every 200hours or 3 calendar months whichever occurs first, thereafter.

V - Phase 53 - Every 900 hours or 12 calendar months, whichever occurs first.

W - Phase 49 - First 6 years or 2400 hours, whichever occurs first, and every 1200 hours or 36calendar months, whichever occurs first, thereafter.

X - Phase 54 - First 10 years from date of manufacture and every 5 years thereafter (based upondate of previous hydrostatic test).

Y - Phase 55 - First 6000 hours or 10 years, whichever occurs first, and every 2400 hours or 10years, whichever occurs first thereafter. (Not currently used)

Z - Phase 56 - Every 150 hours (No grace period). (Not currently used)

AA - Phase 57 - First 150 hours and every 150 hours or 24 calendar months thereafter, whicheveroccurs first (no grace period). (Not currently used)

AB - Phase 58 - Every 500 operating hours of the Auxiliary Power Unit (APU) starter-generator.Phase 58 is to be performed prior to the APU starter-generator overhaul asrequired in Chapter 5-11-00.

AC - Phase 59 - Every 600 hours or 12 calendar months whichever occurs first.

AD - Phase 60 - Inspect initially at 2400 hours and then every 1200 hours thereafter.

AE - Phase 61 - Inspect every 1200 hours. (Not currently used)

AF - Phase 62 - Thrust Reverser Lubrication. Refer to the Nordam Group Thrust ReverserComponent Maintenance Manual for the lubrication intervals and procedures.(Not currently used)

AG - Phase 63 - Every 12 calendar months as required by 14 CFR 91.207. (No grace period.)

AH - Phase 64 - Every 800 hours. (Not currently used)

AI - Phase 65 - Every 1500 hours. (Not currently used)

AJ - Phase 66 - Every 3000 hours.

AK - Phase 67 - Every 400 hours or 12 calendar months whichever occurs first.

AL - Phase 68 - Every 500 hours.

AM - Phase 69 - Every 6 calendar months (for airplanes that operate in moderate or severecorrosion environments. Refer to Chapter 51, Corrosion Severity Maps -Description and Operation).

AN - Phase 70 - Every 500 compressor hours on the vapor cycle cooling system.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

AO - Phase 71 - First 6000 hours, then every 1200 hours thereafter.

MA - Phase MA - Every 500 hours. (This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.) (Not currently used)

MB - Phase MB - First 3000 hours, then every 1500 hours thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

MC - Phase MC - First 180 hours and every 180 hours or 24 calendar months thereafter, whicheveroccurs first. (This inspection is a Chapter 4 requirement, and as such, the intervallimitation CANNOT be exceeded.) (Not currently used)

MD - Phase MD - First 6000 hours or 10 years, whichever occurs first, and every 2400 hoursor 10 years, whichever occurs first thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

ME - Phase ME - Every 15,000 hours. (This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.)

MF - Phase MF - First 7500 hours, then every 1400 hours thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

MG - Phase MG - First 6500 hours, then every 3000 hours thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

MH - Phase MH - First 11,000 hours, then every 6000 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

MI - Phase MI - First 5000 hours, then every 2500 hours thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

MJ - Phase MJ - Every 13,000 hours. (This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.)

MK - Phase MK - First 11,500 hours, then every 9000 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

ML - Phase ML - First 11,500 hours, then every 3300 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

MM - Phase MM - First 11,000 hours, then every 4200 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

MN - Phase MN - First 9000 hours, then every 3400 hours thereafter. (This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.)

MO - Phase MO - First 12,500 hours, then every 6100 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

MP - Phase MP - Every 300 hours. (This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.)

MQ - Phase MQ - First 10,000 hours, then every 5000 hours thereafter. (This inspection is a Chapter4 requirement, and as such, the interval limitation CANNOT be exceeded.)

NOTE 1: Landing includes full-stop and touch-and-go landings.

3. Tasks

A. Inspection items identified as having tasks associated with them are more complex than can bedescribed in Inspection Time Limits. Tasks are identified with an ATA Chapter-Section-Subsection-Function number. Each task has a unique number. The Chapter-Section-Subsection numberidentifies the specific location of the procedure in the Maintenance Manual, while the last three digitsare assigned to correspond to the tasks specific functions.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

B. The example illustrates a sample task number. Beginning with the word Task, the numbers that followindicate the chapter, section and subsection that inspection task text can be found. The two-digitfunction number indicates the general classification of the task. See function number identification inTable 1. The last digit indicates the sequence number. If the same chapter-section-subsection andfunction is used for a different task, the sequence number increments by one.

C. CD-ROM users may link from a highlighted task number to the task text. Task numbers may be foundin the Inspection Time Limits table or at any point throughout this manual where a task number isreferenced.

D. Task functions which may be used in this manual are listed in Table 1.

NOTE: Third digit of function is assigned sequentially beginning with zero to ensure a uniquenine-digit task number.

E. Supplemental Type Certificate Installations.(1) Inspection requirements for STC installations are not included in this manual. When an

STC installation is incorporated on the airplane, those portions of the airplane affected bythe installation must be inspected in accordance with the inspection program published bythe owner of the STC. Since STC installations may change systems interface, operatingcharacteristics and component loads or stresses on adjacent structures, Cessna providedinspection criteria may not be valid for airplanes with STC installations.

Table 1. Function Number Identification

10 CLEANING 60 SERVICING, PRESERVING,LUBRICATION

11 Chemical 61 Servicing

12 Abrasive 64 Lubricating

13 Ultrasonic 65 Fueling, Defueling

14 Mechanical 67 Disinfect, Sanitize

15 Stripping 68 Drain Fluid

16 Miscellaneous Cleaning 70 TESTING, CHECKING

17 Flushing 71 Operational

20 INSPECTION, CHECK 72 Functional

21 General Visual 75 Special

22 Detailed Dimensional 76 Electrical


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Function Number Identification (continued)

23 Penetrant 78 Pressure

24 Magnetic 79 Leak

25 Eddy Current 80 MISCELLANEOUS

26 X-Ray 81 Fault Isolation

27 Ultrasonic 82 Adjusting, aligning, calibration,rigging

28 Specific, Special 87 Bleeding

29 Borescope 90 CHANGE, REMOVE, INSTALL

96 Replace

4. Definitions

A. Lubrication or Servicing Task(1) Any act of lubrication or servicing for the purpose of maintaining inherent design capabilities.

B. Visual Check(1) A visual check is an observation to determine that an item is fulfilling its intended purpose. The

check does not require quantitative tolerances. This is a failure finding task.

C. General Visual (Surveillance) Inspection(1) A visual examination of an interior or exterior area, installation or assembly to detect obvious

damage, failure, or irregularity. This level of inspection is made under normally available lightingconditions such as daylight, hangar lighting, flashlight, or drop-light and may require removalor opening of access panels or doors. Stands, ladders, or platforms may be required to gainproximity to the area being checked.

D. Detailed Inspection(1) An intensive visual examination of a specific structural area, system, installation or assembly to

detect damage, failure, or irregularity. Available lighting is normally supplemented with a directsource of good lighting at an intensity deemed appropriate by the inspector. Inspection aidssuch as mirrors, magnifying lenses, etc. may be used. Surface cleaning and elaborate accessprocedures may be required.

E. Special Detailed Inspection(1) An intensive examination of a specific item(s), installation or assembly to detect damage,

failure, or irregularity. The examination is likely to make extensive use of specialized inspectiontechniques and/or equipment. Intricate cleaning and substantial access or disassemblyprocedure may be required.

F. Operational Check(1) An operational check is a task to determine that an item is fulfilling its intended purpose. The


G. Functional Check(1) A functional check is a quantitative check to determine if one or more functions of an item perform

within specified limits.

H. Restoration Task(1) That work necessary to return the item to a specific standard. Since restoration may vary from

cleaning or replacement of single parts up to a complete overhaul, the scope of each assignedrestoration task has to be specified.

I. Discard Task(1) The removal from service of an item at a specified life limit. Discard tasks are normally applied

to so-called single parts such as cartridges, canisters, cylinders, engine disks, and safe-lifestructural members.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION TIME LIMITS

1. Inspection Items

REVISIONSTATUS

ITEM CODENUMBER

TASK INTERVAL CH SE SU ZONE

Added Jan3/05

A110001 Required Interior and ExteriorPlacards and Decals - Examine forsecurity of installation and legibility.Task 11-00-00-210

F 05-12-05 All Zones

DeletedJan 3/05

A112002

DeletedJan 3/05

A112003

DeletedJan 3/05

A113001

RevisedJul 1/07

A212002 Cabin Air Distribution CheckValves Detailed Inspection Task21-22-00-210

F 05-12-05 161, 162

RevisedJan 1/10

B213000 Pressurization System FunctionalCheck Task 21-30-00-721

F 05-12-05 ENG

RevisedJul 1/07

B213002 Cabin Altitude Pressure SwitchFunctional Test Task 21-31-05-720

F 05-12-05 245

DeletedApr 1/13

D213003

B215000 Environmental System - Performoperational check. Task 21-51-00-710

F 05-12-05 ENG

RevisedJan 1/10

B215001 Emergency Pressurization SystemOperational Check Task 21-51-00-712

E 05-12-04 ENG

RevisedJul 1/12

A215201 Vapor Cycle Cooling System HourMeter Check Task 21-52-00-210

MP 05-12-MP 332

DeletedJul 1/12

A215202

DeletedJul 1/12

A215203

Added Jan1/14

A215207 Vapor Cycle Cooling System 500Compressor-Hour Maintenance Task21-52-00-211

AN 05-12-70 321, 322

Added Jan1/14

A215208 Vapor Cycle Cooling System12-Month Maintenance Task21-52-00-212

K 05-12-18 321, 322

B216001 Nose Avionics Cooling Fan - Performoperational check. Task 21-25-00-710

F 05-12-05 AUX

Added Jan4/99

A216001 Nose Avionics Cooling Fan - Inspect.Task 21-25-00-210

F 05-12-05 110

B216002 Instrument Panel Cooling - Performoperational check. Task 21-24-00-710

F 05-12-05 AUX


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Jan4/99

A216002 Cockpit Zone Temperature Assembly- Inspect. Task 21-61-00-710

F 05-12-05 246

Added Jan4/99

A216003 Cabin Zone Temperature Assembly -Inspect. Task 21-61-00-711

F 05-12-05 261

RevisedJul 1/07

D217001 Water Separator Restoration(Cleaning) Task 12-19-02-160

J 05-12-30 312

RevisedJul 1/15

A217002 Aspirator (Water Separator Nozzle)- Inspect nozzle for heat or otherdamage. Task 21-51-00-210

F 05-12-05 312

RevisedJul 1/07

D217002 Ozone Converters Restoration(Cleaning) Task 12-19-02-161

AJ 05-12-66 321, 322

A221001 Aileron Servo Mount and Actuator -Inspect. Task 22-11-01-210

F 05-12-05 314

A221002 Rudder Servo Mount and Actuator -Inspect. Task 22-11-01-211

F 05-12-05 321

A221003 Elevator Servo Mount and Actuator -Inspect. Task 22-11-01-211

F 05-12-05 321

B221004 Autopilot Disengagement andWarning System - Perform operationaltest. Task 22-11-03-710

F 05-12-05 AUX

Added Jan3/05

A221004 Aileron, Rudder, and ElevatorAutopilot Servo Cables - Examine.Task 22-11-01-220

T 05-12-51 314, 321,340

A231001 High Frequency Antenna andTensioning Unit - Inspect. Task23-11-00-210

F 05-12-05 312, 340

RevisedJul 1/08

A236001 Static Discharging System FunctionalCheck Task 23-90-60-720

F 05-12-05 331, 332,532, 540,632, 640

A237001 Cockpit Voice Recorder and ULD -Inspect. Task 23-70-00-210

N 05-12-21 312

RevisedJan 5/04

B237002 Cockpit Voice Recorder System(Fairchild A200S) - Complete anoperational test. Task 23-70-00-710

E 05-12-01 AUX

RevisedJan 1/10

B237003 Underwater Locator Beacon Installedon Cockpit Voice Recorder - Performpinger test using DuKane PL-1 tester.Task 23-90-70-720

N 05-12-21 312

Added Jan5/04

B237004 Cockpit Voice Recorder System(Fairchild FA2100) - Complete anoperational test. Task 23-70-00-711

E 05-12-01 AUX

RevisedApr 1/16

B238001 Standby Nav/Com Control UnitOperational Check (Airplanes -5001thru -6000) Task 23-80-01-710

AL 05-12-68 AUX


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedAug 9/99

A242001 Nose Area Electrical Components -Inspect. Task 24-00-00-210

F 05-12-05 110, 211,212, 221,222

DeletedJan 1/15

D243002

B243003 Overvoltage System - PerformFunctional Test. Task 24-41-02-710

E 05-12-01 AUX

Added Jul3/00

B243300 Lead Acid Batteries - Checkgeneral condition and security.Check terminals for overheating orburning. Perform battery checks andcapacity test as necessary. NOTE:The inspection schedule may beadjusted after the useful battery lifeis established, based on operations.Task 24-33-00-760

U 05-12-52 313

A245001 Cockpit Circuit Breaker Panels -Inspect. Task 24-50-02-210

K 05-12-18 245, 246

A245002 Side Console Equipment Panel -Inspect. Task 24-50-02-211

F 05-12-05 245, 246

Added Jan1/15

B245002 Ni-Cad Battery (Saft) FunctionalCheck (Capacity Check) Theinspection interval can be adjustedafter the water loss per cell isestablished. Refer to the BatteryService Table. Task 24-90-50-721

I 05-12-28 321, 322

RevisedJan 4/99

A245003 Aft Power Junction Box - Inspect.Task 24-50-03-210

F 05-12-05 311, 312

Added Jan1/15

B245003 Ni-Cad Battery (Marathon) FunctionalCheck (Capacity Check) Theinspection interval can be adjustedafter the water loss per cell isestablished. Refer to the BatteryService Table. Task 24-90-50-722

I 05-12-28 321, 322

Added Apr5/99

A245005 Interior Junction Box Components -Inspect. Task 24-50-05-210

F 05-12-05 261

A251001 Crew and Cabin Seats - Inspect. Task25-11-01-210

F 05-12-05 241, 242,251, 252,261, 262

RevisedJul 1/15

A251002 Pilot and Copilot Seat Track Stops -Inspect for damage and security ofinstallation. Task 25-11-01-211

F 05-12-05 241, 242

RevisedApr 1/06

B256001 ELT 110-4 Emergency LocatorBeacon System - Visually examineand complete an operational test.Test required by Title 14 of the Codeof Federal Regulations 91.207. Task25-61-03-710

AG 05-12-63 BAT


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/06

A256002 First Aid Kit Detailed Inspection -Perform Task 25-60-01-210

K 05-12-18 262

RevisedAug 9/99

A256003 Life Preserver(s) - Inspect. Task25-60-00-210

K 05-12-18 241, 242,251, 252,261, 262

Added Apr1/06

A256004 Artex C406-2 Emergency LocatorTransmitter - Complete a visualexamination. Required by Title 14of the Code of Federal Regulations91.207. Task 25-61-04-210

AG 05-12-63 BAT

Added Apr1/06

B256004 Artex C406-2 Emergency LocatorTransmitter - Complete an operationaltest. Required by Title 14 of the Codeof Federal Regulations 91.207. Task25-61-04-720

AG 05-12-63 BAT

Added Apr1/06

A256005 Artex C406-N Emergency LocatorTransmitter - Complete a visualexamination. Required by Title 14of the Code of Federal Regulations91.207. Task 25-61-05-210

AG 05-12-63 BAT

Added Apr1/06

B256005 Artex C406-N Emergency LocatorTransmitter - Complete an operationaltest. Required by Title 14 of the Codeof Federal Regulations 91.207. Task25-61-05-720

AG 05-12-63 BAT

Added Apr1/17

A256106 Artex 110-406 Emergency LocatorInspection Task 25-61-06-210

AG 05-12-63 BAT

Added Apr1/17

B256106 Artex 110-406 Emergency LocatorFunctional Test Task 25-61-06-720

AG 05-12-63 BAT

RevisedApr 1/06

A262002 Portable Fire ExtinguisherBottle Detailed Inspection Task26-22-00-750

G 05-12-08 242, 262

DeletedJan 1/15

B262002

DeletedJan 1/15

B262003

DeletedJul 1/15

B262007

B262010 Fire Extinguishing System - Performfunctional test. Task 26-21-00-720

F 05-12-05 AUX

RevisedOct 1/11

A271001 Aileron and Aileron Trim Tab Securityof Installation - Examine. Task27-10-00-211

F 05-12-05 244, 247,248, 532

RevisedJul 1/07

B271001 Aileron Trim Tab Functional Test (FreePlay) Task 27-10-00-220

E 05-12-02 532


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJan 4/99

C271001 Aileron Trim Tab Actuator - Lubricate.Task 12-21-01-640

E 05-12-02 532

B271002 Aileron and Trim Tab - Check Travel.Task 27-10-00-221

F 05-12-05 532, 632

RevisedJul 5/04

A271003 Aileron Fuselage and Inboard WingControl Cables - Inspect. Task27-10-00-210

AD 05-12-60 141, 142,152, 161,162, 247,248

RevisedJul 1/07

A271004 Aileron Outboard Wing Control CableFunctional Test Task 27-10-00-212

F 05-12-05 512, 522,532, 612,622, 632

RevisedOct 1/06

A271005 Aileron Trim Tab Control Cables -Examine. Task 27-10-00-222

T 05-12-51 141, 153,163, 512,522,

DeletedNov 1/07

A271006

A272001 Rudder and Rudder Trim Tab -Inspect. Task 27-20-00-223

E 05-12-02 340

RevisedJul 1/07

B272002 Rudder Trim Tab Functional Test(Free Play) Task 27-20-00-220

J 05-12-30 340

RevisedJan 4/99

C272002 Rudder Trim Tab Actuator - Lubricate.Task 12-21-01-640

E 05-12-02 340

RevisedApr 5/99

B272003 Rudder - Check rudder and ruddertrim tab travel. Task 27-20-00-221

F 05-12-05 340

A272004 Rudder Pedals - Inspect. Task27-20-00-224

F 05-12-05 241, 242

RevisedFeb 23/04

A272005 Rudder Control Cables - Inspect.Task 27-20-00-225

AD 05-12-60 141, 151,161, 241,311, 321,322

Added Jan3/05

A272006 Rudder Trim Tab Control Cables -Examine. Task 27-20-00-226

T 05-12-51 141, 142,153, 163,166, 321,322

Added Jan3/05

A272007 Rudder Bias Control Cables -Examine. Task 27-20-00-227

T 05-12-51 322

DeletedNov 1/07

A272008

RevisedJun 3/02

A273001 Elevator and Elevator Trim TabExternal Visual Inspection. Task27-31-00-211

F 05-12-05 351, 352

RevisedApr 5/99

C273002 Elevator Trim Tab Actuators -Lubricate. Task 12-21-01-640

E 05-12-02 351, 352

RevisedApr 5/99

B273003 Elevator and Elevator Trim Tab -Check travel. Task 27-31-00-221

F 05-12-05 351, 352


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 5/04

B273004 Elevator Trim Tab - Check elevatortrim tab free play. Task 27-31-00-220

F 05-12-05 351, 352

RevisedJan 5/04

A273007 Control Column - Examine. Task27-31-02-210

F 05-12-05 141, 142,241, 242

RevisedFeb 23/04

A273008 Elevator Control Cables - Inspect.Task 27-31-00-210

AD 05-12-60 141, 142,151, 161,311, 321

Added Jan4/99

A273009 Elevator Linkage - Inspect. Task27-31-00-212

F 05-12-05 340

RevisedOct 1/06

A273010 Elevator Trim Tab Control Cables -Examine. Task 27-31-00-222

T 05-12-60 141, 142,153, 163,165, 321

DeletedNov 1/07

A273011

B274001 Takeoff Warning System Sensors- Operational check. Task27-40-00-712

F 05-12-05 AUX

B274002 Two Position Horizontal Stabilizer- Operational check. Task27-40-00-710

F 05-12-05 AUX

RevisedDec 6/99

C274002 Horizontal Stabilizer ActuatorReservoir - Oil leakage acceptancecriteria and oil level check. Task12-21-01-641

F 05-12-05 340

RevisedJul 1/08

A275001 Flap Drive System - Inspect. Task27-51-00-210

F 05-12-05 142, 153,163, 166

Added Jul5/04

C275001 Flap Rollers Lubrication - PerformTask 12-21-01-643

E 05-12-03 512, 522,612, 622

DeletedNov 4/02

B275002

B275003 Flaps - Check flap travel. Task27-51-00-220

F 05-12-05 512, 522,612, 622

B275004 Flap Approach Warning Switch -Perform operational check. Task27-51-00-710

F 05-12-05 AUX

RevisedJul 1/07

A276001 Speed Brake System DetailedInspection Task 27-61-00-210

F 05-12-05 512, 522,612, 622

RevisedJul 1/15

A277002 Control Lock Assembly - Inspectfor security of installation, wear andcorrosion. Task 27-71-00-210

F 05-12-05 151

RevisedJul 1/07

B277003 Control (Gust) Lock SystemOperational Check Task 27-71-00-710

F 05-12-05 235


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/07

A281001 Fuel Storage System DetailedInspection Task 28-10-00-210

F 05-12-05 511, 512,521, 522,531, 532,611, 612,621, 622,631, 632

DeletedJan 5/04

A281002

RevisedJul 1/07

A281003 Fuel Filler Cap Lubrication Task28-11-04-210

G 05-12-08 531, 631

B282001 Fuel Boost Pump and ScavengeEjector Pump - Perform operationaltest. Task 28-20-00-710

F 05-12-05 AUX

RevisedJul 1/07

B284001 Low Fuel Warning System FunctionalTest Task 28-42-00-710

F 05-12-05 AUX

A291001 Hydraulic Panel Assembly andComponents - Inspect. Task29-11-06-210

F 05-12-05 313

RevisedJul 1/07

D291002 Hydraulic System Filters Discard Task29-11-04-901

F 05-12-05 313

RevisedJul 1/08

B301001 Bleed Air Anti-Ice SystemsOperational Check (Airplanes-5001 thru -6000) Task 30-11-00-710

F 05-12-05 ENG

B301002 Pneumatic Deice System - Performoperational test. Task 30-12-00-710

E 05-12-02 ENG

RevisedJul 1/15

A301003 Deice Boots, Empennage - Inspect forsecurity of installation and evidenceof damage. Task 30-12-01-210

E 05-12-02 351, 352

RevisedJul 1/15

A301004 Deice Control Valves - Inspect forcorrosion, security of installation.Task 30-12-02-210

F 05-12-05 311, 321

RevisedJul 1/15

A301005 Deice Pressure Switches - Inspectfor corrosion, security of installationand damaged electrical components.Task 30-12-02-211

F 05-12-05 322

RevisedJul 1/07

B304001 Nose Compartment OvertemperatureSwitch Functional Test Task30-40-00-710

F 05-12-05 AUX

RevisedApr 5/99

A311001 Instrument Panel Area - Inspect. Task31-10-00-210

F 05-12-05 235

RevisedJul 1/16

D312001 Davtron Digital Clock Battery -Discard Task 31-20-01-960

K 05-12-18 235

Added Apr5/99

A313001 Flight Data Recorder and UnderwaterLocating Device (ULD) - Inspect. Task31-30-01-210

N 05-12-21 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr5/99

B313001 Underwater Locating Device (ULD)located on the Flight Data Recorder- Perform operational test. Task31-30-01-720

N 05-12-21 322

RevisedJan 1/12

B313004 Flight Data Recorder SystemFunctional Check Task 31-90-30-720

F 05-12-05 322

B320001 Landing Gear Extension andRetraction - Perform functional test.Task 32-01-00-720

E 05-12-02 AUX

Added Apr1/13

A320003 Landing Gear General VisualInspection (Corrosion Inspection)Task 32-00-00-210

AM 05-12-69 710, 720,730

Added Apr1/13


K 05-12-18 710, 720,730

RevisedApr 1/06

A321001 Main Gear - Inspect. Task32-10-00-210

E 05-12-02 720, 730

RevisedJul 1/07

D321001 Main Landing Gear Breather VentDiscard Task 32-10-00-960

E 05-12-02 720, 730

RevisedJan 4/99

A322001 Nose Gear - Inspect. Task32-20-00-210

E 05-12-02 710

RevisedJul 1/15

A322002 Shimmy Damper - Inspect for security,evidence of damage and properservice. Task 32-20-01-610

D 05-12-02 710

RevisedJul 7/98

C322003 Nose Landing Gear - Lubricate. Task12-21-02-640

E 05-12-02 710

DeletedJan 5/04

C322004

Added Apr5/99

C322005 Main Landing Gear Lubrication -Perform. Task 12-21-02-642

E 05-12-02 720, 730

DeletedJan 5/04

C322006

A323001 Uplock Assembly - Inspect. Task32-30-05-210

E 05-12-02 710, 720,730

A323002 Emergency Extension System Cables- Inspect. Task 32-30-08-210

F 05-12-05 141, 151,161, 512,612, 710

A323003 Emergency Gear Release RiggingFunctional Check. Task 32-30-08-720

F 05-12-05 512, 612

DeletedJul 1/15

B323004

DeletedApr 1/06

A324001

DeletedApr 1/06

A324002


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/15

A324003 Main Gear Wheel Brakes - Checkbrake wear. Task 32-42-01-220

D 05-12-02 720, 730

RevisedJul 1/15

B324003 Main Gear Wheel Brakes - Checkparking brake for operation. Task32-44-00-711

E 05-12-04 ENG

RevisedApr 1/09

A324005 Brake Reservoir Visual Inspection(Airplanes -5001 thru -5500) Task32-42-00-210

F 05-12-05 221

RevisedApr 1/09

D324006 Brake Reservoir Air FilterReplacement (Airplanes -5001thru -5500) Task 32-42-00-902

F 05-12-05 222

RevisedApr 1/09

D324007 Reservoir Supply Line Filter Cleaning(Airplanes -5001 thru -5500) Task32-42-00-131

F 05-12-05 221

RevisedApr 1/09

D324008 Hydraulic Pack Assembly FilterReplacement (Airplanes -5001 thru-5500) Task 32-42-00-901

F 05-12-05 211

RevisedApr 1/09

B324009 Antiskid System Functional Test(Airplanes -5001 thru -5500) Task32-42-00-710

F 05-12-05 AUX

B324010 Emergency Brake System - Performoperational test. Task 32-42-09-710

F 05-12-05 AUX

RevisedJul 1/15

A324011 Brake Master Cylinders (Airplanes-5001 thru -5500) - Inspect for leaksand security. Inspect hoses forchafing and evidence of damage.Task 32-42-02-210

E 05-12-01 241, 242

Added Apr1/09

A324400 Brake Reservoir Visual Inspection(Airplanes -5501 and On) Task32-44-00-210

F 05-12-05 313

Added Apr1/09

D324400 Vent Filter Element Replacement(Airplanes -5501 and On) Task32-44-00-960

F 05-12-05 313

Added Jan3/05

B324401 Antiskid Brake System (Airplanes-5501 and On) - Complete a functionaltest. Task 32-44-00-710

F 05-12-05 AUX

Added Apr1/09

D324401 Hydraulic Pump Assembly FilterReplacement (Airplanes -5501 andOn) Task 32-44-00-961

F 05-12-05 313

RevisedJul 1/15

A325001 Nose Steering Arm and SupportBracket, Bungee and Bellcrank -Inspect for security, wear, corrosion,failed fasteners and evidence ofdamage. Task 32-50-00-210

F 05-12-05 710

A325002 Nose Steering Cables - Inspect. Task32-50-00-730

F 05-12-05 211, 241


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/15

A332001 Indirect Cabin Fluorescent Lighting(Airplanes -5001 thru -5349) -Inspect high voltage wiring aboveheadliner for security of installationand condition of electrical wire. Task33-20-01-210

F 05-12-05 251, 252,261, 262

A335001 Emergency Lighting Battery Packs -Inspect. Task 33-50-00-210

F 05-12-05 241, 261

RevisedJul 1/07

B335001 Emergency Lighting SystemOperational Check Task 33-50-00-710

E 05-12-01 BAT

RevisedJul 1/15

A335002 Emergency Exit Lights - Inspectfor security of installation. Task33-50-02-210

E 05-12-01 164, 166,251, 252,261, 262

DeletedOct 2/00

B341001

DeletedOct 2/00

B341002

DeletedOct 2/00

B341003

DeletedOct 2/00

B341004

B341005 Angle-of-Attack System - PerformSelf-Test Procedure and the LandingGear Extended and Squat SwitchLogic Test. Task 34-14-01-720

F 05-12-05 AUX

RevisedJan 5/04

B341006 Air Data Systems (Airplanes -0001thru -5356) - Perform calibrationrequired by Title 14 of the Code ofFederal Regulations 91.411. Task34-11-08-710

M 05-12-20 AUX

RevisedOct 2/00

B341007 Perform RVSM Skin WavinessInspection. Task 34-11-01-220

M 05-12-20 141, 142

RevisedJan 1/14

B341008 Air Data Systems (Airplanes -5357thru -6000) - Perform calibrationrequired by Title 14 of the Code ofFederal Regulations 91.411. Task34-11-09-710

M 05-12-20 AUX

RevisedOct 1/10

A342001 Magnetic Compass Inspection(Airplanes -5001 thru -5500,and Airplanes -5501 thru -6000Incorporating SB560XL-34-61) -Examine for correct installation, aclean surface, and signs of damage.Make sure that the current compasscard is installed. Task 34-24-01-210

F 05-12-05 241

RevisedJul 5/04

B342001 AHRS, Standby HIS-315 and StandbyMagnetic Compass Accuracy Check -Perform Task 34-21-01-710

F 05-12-05 ENG


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/07

B342002 L3 Com Standby Battery PackFunctional Test (Capacity Check)Task 34-20-00-762

K 05-12-18 LAB

DeletedJan 5/04

B342003

RevisedJul 1/07

B342004 Securaplane Standby BatteryOperational Check (Energy Level)Task 34-20-00-763

J 05-12-30 211

RevisedApr 1/09

B345001 Transponder Functional Check(Required by 14 CFR 91.413) Task23-90-20-720

M 05-12-20 AUX

RevisedJul 1/15

A351001 Oxygen Cylinder, Supply PressureRegulator and Shutoff Valve - Inspectfor security of installation, corrosion,cleanliness of the area and evidenceof damage. Verify valve is safetied inthe ON position. Task 35-01-00-210

F 05-12-05 212

RevisedJul 1/07

B351001 Passenger Oxygen SystemFunctional Test Task 35-01-00-710

F 05-12-05 AUX

RevisedJul 1/15

A351002 Crew Oxygen Mask - Inspectmasks and hoses for deterioration,cleanliness and proper stowage. Task35-10-01-210

F 05-12-05 241, 242

DeletedOct 1/11

B351003

RevisedJul 1/15

A351004 Passenger Mask - Inspect masksand hoses for deterioration,cleanliness and proper stowage. Task35-20-02-210

K 05-12-18 251, 261

DeletedOct 1/11

B351005

Added Apr1/10

A353001 Protective Breathing EquipmentDetailed Inspection Task35-30-00-220

K 05-12-18 251, 252,261, 262

RevisedApr 1/13

D361001 Particulate Trap Restoration(Cleaning) NOTE: This suppliesdata to clean the Cabin Door andOutflow Valve particulate traps. Task36-15-00-170

F 05-12-05 161

RevisedApr 1/10

A361101 Precooler Heat Exchanger GeneralVisual Inspection Task 36-11-03-210

AC 05-12-59 411, 412

RevisedJul 1/08

B383001 Externally Serviceable ToiletFunctional Check Task 38-30-02-720

F 05-12-05 262

A383002 Externally Serviceable Toilet - Inspectall toilet plumbing, including the tank,for signs of leakage or damage. Task38-30-02-210

K 05-12-18 262


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


B383003 Drain Lines - Perform an operationalcheck. Task 38-30-00-710

F 05-12-05 151, 162

Added Jul3/00

A490001 Auxiliary Power Unit - Inspect. Task49-00-00-210

V 05-12-53 321, 322

DeletedApr 1/17

A511003

C521000 Door Locks - Lubricate lock tumblers. D 05-12-01 211, 212,323, 331,810

RevisedJul 1/15

A521001 Cabin Door Inflatable Seal, SecondarySeal - Inspect for security ofinstallation, wear, deteriorationand evidence of damage. Task52-10-04-210

E 05-12-01 810

DeletedJul 1/07

C521002

A521003 Cabin Door and Door frame -Inspect for cracks, loose or failedfasteners, damaged locking pins,worn or damaged receptacles andindications of structural damage. Task52-10-00-211

F 05-12-05 251

RevisedJul 1/07

A521004 Cabin Door Detailed Inspection Task52-10-00-210

F 05-12-05 810

Added Apr1/09

A521008 Cabin Door Detailed Inspection(Chapter 4 Item) Task 52-10-00-210

ME 05-12-ME 810

RevisedJul 1/07

A522001 Emergency Exit Door DetailedInspection Task 52-20-00-210

F 05-12-05 820

Added Apr1/09

A522004 Emergency Exit Door DetailedInspection (Chapter 4 Item) Task52-20-00-210

ME 05-12-ME 820

RevisedJul 1/15

A524001 Tailcone Access Door - Inspect forproper operation and evidence ofdamage. Task 52-40-00-210

F 05-12-05 312

RevisedApr 5/99

A524002 Nose Compartment Doors - Inspectfor security of installation. Task52-40-01-210

F 05-12-05 211, 212

B527001 Door Warning System - Performoperational check. Task 52-70-00-710

E 05-12-01 AUX

RevisedJul 1/15

A528001 Main Landing Gear Door - Inspecthinge for corrosion and doorsfor evidence of damage. Task32-10-00-211

E 05-12-02 720, 730

RevisedJul 1/15

A528002 Nose Landing Gear Door - Inspectdoors for evidence of damage andsigns of tire rub. Task 32-20-00-211

D 05-12-02 710


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


A530001 Pressurized Area Moisture Seals -Inspect. Task 53-10-05-160

F 05-12-05 141, 151,161, 162

RevisedJul 1/15

A530002 Moisture Drain Holes - Inspectairplane unpressurized area drainholes for obstruction and evidence ofcorrosion. Task 53-10-05-210

E 05-12-01 211, 212,411, 412,511, 512,611, 612

Added Apr1/13

A530013 Nose Landing Gear Wheel WellGeneral Visual Inspection (CorrosionInspection). Task 53-00-00-210

AM 05-12-69 710

Added Apr1/13


K 05-12-18 710

Added Jan1/15

A530015 Tailcone Area General VisualInspection Task 53-90-00-218

K 05-12-18 313, 321,322

Added Jan1/15

A530016 Tailcone Under Floor Areaand Tailcone Stinger GVI Task53-90-00-219

N 05-12-21 313, 321,322

DeletedJan 4/99

A531003

A531004 Aft Tailcone Components - Inspect.Task 53-10-12-210

F 05-12-05 321, 322

A531005 Forward Tailcone Components -Inspect. Task 53-10-12-211

F 05-12-05 311, 312

A531006 Fuselage Internal Components -Inspect. Task 53-10-11-210

F 05-12-05 141, 142,151, 152,161, 162

DeletedOct 5/98

A531008

RevisedJul 1/15

A531009 Emergency Exit Door Frame - Inspectfor cracks, loose or failed fastenersand any indication of structuraldamage. Task 53-10-11-212

F 05-12-05 820

RevisedOct 1/07

A531010 Aft Pressure Bulkhead - Visuallyinspect forward side for cracks, failedfasteners, corrosion and evidence ofstructural damage (Chapter 4 Item).Task 53-10-11-252

ME 05-12-ME 311, 312

RevisedJul 1/15

A531011 Nose Area - Inspect all structuresfor security of installation, cracks,corrosion. Task 53-90-00-216

F 05-12-05 110, 211,212, 221,222

RevisedJan 4/99

A531012 Control Pedestal - Inspect. Task53-20-02-210

F 05-12-05 243

RevisedJul 1/15

A531013 Stinger Assembly - Inspect for securityof installation, corrosion and evidenceof damage. Task 53-90-00-215

F 05-12-05 321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/15

A531015 Radome Surface Mounted LightningDiverter Strips - Inspect for missingsegments, corrosion, damage andelectrical continuity to airplanestructure. Task 53-10-10-211

E 05-12-01 110

A531016 Radome - Inspect. Task 53-10-10-210 F 05-12-05 110

B531017 Radome - Check electrical bond.Task 53-10-10-760

E 05-12-01 110

DeletedJan 4/99

A531018

A531019 Inspect for corrosion in the lavatory,vanity and refreshment center area.Task 53-10-11-211

K 05-12-18 161, 162

RevisedApr 1/13

A531020 Forward Pressure Bulkhead - Visuallyinspect forward side for cracks, failedfasteners, corrosion and evidenceof structural damage. Include theweb and supporting structure on theforward side and the periphery angleson the aft side (Chapter 4 Item). Task53-10-11-251

MD 05-12-MD 221, 222

RevisedJul 1/15

A532002 Nose Gear Wheel Well - Inspectnose landing gear attach fittings,supporting structure and remainder ofwheel well for cracks, failed fasteners,corrosion and evidence of damage.Task 53-00-00-210

F 05-12-05 710

RevisedJul 1/15

A532003 Main Gear Wheel Well - Inspectmain landing gear attach fittings,supporting structure and remainder ofwheel well for cracks, failed fasteners,corrosion and evidence of damage.Task 57-10-00-210

F 05-12-05 720, 730

RevisedJul 1/15

A533001 Fuselage Exterior Skin - Inspect forcracks, loose or failed fasteners andevidence of structural damage. Task53-30-01-211

F 05-12-05 141, 142,151, 152,161, 162,231, 232,241, 242,251, 252,261, 262

RevisedJul 1/07

A533002 Fuselage External Surface SpecialDetailed Inspection (Eddy Current)Task 53-30-01-250

W 05-12-49 141, 142,151, 152,161, 162,241, 242,251, 252,261, 262

Added Apr1/09

A533004 Upper Skin Splice at BL 0.00 (Chapter4 Item) Task 53-30-01-251

ME 05-12-ME 251, 252,261, 262


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/09

A533006 Lower Skin Splice at Stringer 13(Chapter 4 Item) Task 53-30-01-252

ME 05-12-ME 141, 142,151, 152,161, 162

Added Apr1/09

A533008 Lower Skin from Right Stringer 13 toLeft Stringer 13 (Chapter 4 Item) Task53-30-01-210

ME 05-12-ME 141, 142,151, 152,161, 162,321, 322

Added Apr1/09

A533010 Upper Skin from Right Stringer 13 toLeft Stringer 13 (Chapter 4 Item) Task53-30-01-210

MJ 05-12-MJ 241, 242,251, 252,261, 262,311, 312,321, 322

RevisedJul 1/15

A541001 Nacelle Firewall - Inspect for damage,deteriorated firewall sealant andcorrosion. Task 54-50-01-210

F 05-12-05 411, 412

RevisedJul 1/15

A541002 Pylon - Inspect for failed fasteners,evidence of structural damage andpylon skin cracks. Task 54-50-01-211

F 05-12-05 411, 412

Added Oct1/11

A545000 Forward Engine Beam, Upper Angles,Horizontal Cap Flange at BL 30.5to BL 42.0 (Chapter 4 Item) Task54-50-10-250

MJ 05-12-MJ 311, 312,411, 412

RevisedDec 6/99

A551001 Horizontal Stabilizer ExternalInspection - Inspect. Task55-10-01-210

E 05-12-02 351, 352

RevisedJul 1/15

A551002 Horizontal and Vertical Stabilizer AftEdge - Visually inspect for separationof the bond between the skin anddoubler. Task 55-00-00-210

E 05-12-02 351, 352,340

Added Jun3/02

C551003 Horizontal Stabilizer Scissor FittingBolts Lubrication - Perform. Task12-21-01-642

F 05-12-05 340

Added Jan5/04

A551003 Horizontal Stabilizer InternalExamination - Inspect. Task55-10-01-211

F 05-12-05 351, 352

Added Apr1/13

A551006 Horizontal Stabilizer Aft Spar AreaGeneral Visual Inspection (CorrosionInspection) Task 55-10-01-212

AM 05-12-69 351, 352

Added Apr1/13

A551007 Horizontal Stabilizer Aft Spar AreaGeneral Visual Inspection (CorrosionInspection) Task 55-10-01-212

K 05-12-18 351, 352

RevisedJan 5/04

A553001 Vertical Stabilizer ExternalExamination - Inspect. Task55-30-01-210

E 05-12-02 340


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/13

A553002 Vertical Spar Pivot Fitting LowerFlange and Clip Inspection (Thisinspection is necessary for Airplanesthat have not replaced the one-piececlip with a two-piece assembly.) Task55-30-01-211

F 05-12-05 340

Added Jan5/04

A553003 Vertical Stabilizer InternalExamination - Inspect. Task55-30-01-212

AO 05-12-05 340

RevisedOct 1/10

A553005 Vertical Stabilizer Rear Spar Capat WL 146.00 (Airplanes -5001thru -5020) (Chapter 4 item) Task55-30-01-250

MG 05-12-MG 340

RevisedOct 1/10

A553006 Vertical Stabilizer Rear Spar NestedAngle at WL 146.00 (Airplanes -5001thru -5020) (Chapter 4 item) Task55-30-01-251

MH 05-12-MH 340

RevisedOct 1/10

A553007 Vertical Stabilizer Rear Spar Strapat WL 146.00 (Airplanes -5001thru -5020) (Chapter 4 item) Task55-30-01-252

MI 05-12-MI 340

RevisedOct 1/10

A553011 Vertical Stabilizer Forward SparStrap at WL 150.00 (Airplanes -5001thru -5020) (Chapter 4 Item) Task55-30-01-253

MK 05-12-MK 321, 322

Added Apr1/13

A553013 Vertical Stabilizer Forward Spar Strapat WL 188.00 (Airplanes -5001 thru-5020) (Chapter 4 requirement) Task55-30-01-254

MQ 05-12-MQ 340

Added Apr1/13

A553017 Vertical Stabilizer Aft Spar AssemblyGeneral Visual Inspection (CorrosionInspection) Task 55-30-01-213

AM 05-12-69 340

Added Apr1/13


K 05-12-18 340

Added Apr1/16

A553020 Vertical Stabilizer Internal Inspection(NOTE: This inspection is for thehorizontal pivot fitting assembly.)Task 55-30-01-212

AO 05-12-71 340

RevisedJul 1/15

A555001 Horizontal Stabilizer - Inspect theelevator attach points and carry-thrufor evidence of damage. Task55-00-00-211

F 05-12-05 351, 352

RevisedJul 1/15

A555002 Vertical Stabilizer - Inspect therudder and vertical stabilizer attachpoints for evidence of damage. Task55-00-00-212

F 05-12-05 340


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/07

A561001 Cockpit Windshield and Side WindowsDetailed Inspection (Delamination)Task 56-11-00-212

F 05-12-05 241, 242

RevisedApr 1/08

B561001 Windshield Surface Seal TreatmentFunctional Check Task 56-11-00-720

AK 05-12-67 241, 242

RevisedJul 1/07

A561002 Windshield Retainer ScrewsFunctional Test (Torque Inspection)Task 56-11-00-280

F 05-12-05 241, 242

RevisedJul 1/07

A561003 Windshield Humpseal DetailedInspection Task 56-11-00-210

D 05-12-01 241, 242

Added Apr1/13

A561104 Cockpit Openable Aft Side WindowHinge and Latch Inspection Task56-11-00-213

AC 05-12-59 241, 242

RevisedJul 1/15

A562001 Cabin Windows - Inspect windowsfor scratches, cracks, crazing anddeformities. Task 56-20-00-210

E 05-12-01 251, 252,261, 262

RevisedApr 1/09

A571000 Lower Wing Main Spar Lower SkinSplice at WS 22.50 (Chapter 4 item)Task 57-10-00-250

MF 05-12-MF 511, 512,611, 612

RevisedApr 1/09

A571002 Lower Wing Main Spar Lower SkinSplice at WS 22.50 (Chapter 4 item)Task 57-10-00-270

MF 05-12-MF 511, 512,611, 612

Added Apr1/09

A571004 Lower Wing Main Spar Skin SpliceFlange at WS 11.50 (Chapter 4 item)Task 57-10-00-251

ML 05-12-ML 511, 512,611, 612

Added Apr1/09

A571006 Lower Wing Main Spar and SkinSplice at WS 11.50 (Chapter 4 item)Task 57-10-00-271

ML 05-12-ML 511, 512,611, 612

Added Apr1/09

A571008 Lower Wing Main Spar at WS 114.57(Chapter 4 item) Task 57-10-00-252

MM 05-12-MM 521, 522,621, 622

Added Apr1/09


MN 05-12-MN 521, 522,621, 622

Added Apr1/09


MO 05-12-MO 521, 522,621, 622

Added Apr1/13

A571016 Aft Wing Spar Area General VisualInspection (Corrosion Inspection)Task 57-10-00-211

AM 05-12-69 512, 522,532, 612,622, 632

Added Apr1/13


K 05-12-18 512, 522,532, 612,622, 632

Added Apr1/13

A571020 Main Landing Gear Wheel WellGeneral Visual Inspection (CorrosionInspection) Task 57-10-00-210

AM 05-12-69 512, 612

Added Apr1/13


K 05-12-18 512, 612


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/15

A573001 Wings - Inspect external skin andaccess panels for cracks, failedfasteners and evidence of damage.Task 57-10-00-212

F 05-12-05 511, 512,521, 522,531, 532,540, 611,612, 621,622, 631,632, 641

A575002 Flaps - Check drain holes forobstruction. Task 57-50-04-211

E 05-12-02 512, 522,612, 622

A575003 Flaps and Flap Tracks - Inspect. Task57-50-04-210

F 05-12-05 512, 522,612, 622

Added Jan4/99

A575004 Flaps - Perform coin tap inspection.Task 57-50-04-212

F 05-12-05 512, 522,612, 622

DeletedOct 1/01

B710001

RevisedJul 1/15

A711001 Nacelle and Cowling - Inspect theupper and lower cowls, inlet, aftcowling, inboard cowling, oil fillerdoor and access panels for failedfasteners, security of installationand evidence of damage. Task71-90-00-212

E 05-12-04 410, 420

RevisedJul 1/07

A711002 Upper Cowling Camloc Hole DetailedInspection Task 71-11-00-220

F 05-12-05 410, 420

RevisedJul 1/07

A711003 Forward and Aft Upper CowlingEdge Detailed Inspection Task71-11-00-221

F 05-12-05 410, 420

RevisedOct 1/11

A712200 Aft Engine Beam Inspection (Chapter4 Item) NOTE: This engine supportstructure inspection is for Airplanes-5001 thru -5060. Task 71-22-00-210

MB 05-12-MB 311, 312,411, 412

RevisedJul 1/15

A720001 Engine Minor Inspection - Completethe scheduled maintenance checks.Refer to the Model PW545A orPW545B Pratt & Whitney CanadaMaintenance Manual, Chapter5, Section 05-20-00, ScheduledMaintenance Checks. Task71-90-00-610

AC 05-12-59 410, 420

RevisedJan 4/99

A720003 Engine - Perform general inspection.Task 71-00-00-210

E 05-12-04 410, 420

DeletedAug 9/99

B742001

DeletedJul 1/08

B743101


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedJul 1/07

A761101 Fuel Control Unit (FCU) ThrottleLever Cutoff Functional Test(Airplanes-5001 thru -5196 NotIncorporating SB560XL-76-03) Task76-10-00-620

D 05-12-02 410, 420

RevisedOct 1/10

A761102 Fuel Control Unit (FCU) Throttle LeverCutoff Functional Check (Airplanes-5197 thru -6000, and Airplanes-5001 thru -5196 IncorporatingSB560XL-76-03) Task 76-10-00-620

E 05-12-04 410, 420

RevisedJan 4/99

A783012 Thrust Reversers - Inspect. Task78-31-00-210

E 05-12-04 410, 420

DeletedOct 1/06

C783012

RevisedJan 4/99

A783018 Thrust Reverser Electrical JunctionBox - Inspect. Task 78-31-00-211

F 05-12-05 312

DeletedOct 1/10

B783024

RevisedOct 1/10

B783030 Thrust Reverser System FunctionalCheck Task 78-90-30-720

E 05-12-04 AUX

RevisedApr 1/09

C783101 Thrust Reverser Lubrication (WC-393Non-Aerosol Spray LubricationMethod) Task 78-31-00-640

B 05-12-07 AUX

RevisedApr 1/09

C783102 Thrust Reverser Guide RodsLubrication (D-5100NS AerosolSpray Lubrication Method) Task78-31-00-641

B 05-12-07 AUX

RevisedJul 1/07

C783103 Lubrication of the Thrust ReverserPivot Points (C-5A AntiseizeCompound Lubrication Method) Task78-31-00-642

J 05-12-30 AUX

RevisedJan 3/05

C793002 Engine Oil Change and Oil Filter -Replace. Task 79-00-00-610

H 05-12-09 410, 420

RevisedJul 1/15

A801001 Starter-Generator - Inspect forsecurity of installation. Inspectterminal block and electricalconnections for cleanliness andevidence of damage from heating andarcing. Task 80-10-00-210

D 05-12-02 410, 420

B801004 Starter Disengage System - Performoperational test. Task 80-10-00-710

F 05-12-05 ENG

Added Jan7/02

A801101 Auxiliary Power Unit (APU)Starter-Generator Brush - Inspect.Task 80-11-00-620

AB 05-12-58 321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

COMPONENT TIME LIMITS

1. Component Time Limits

A. All components not listed here should be inspected as detailed elsewhere in this chapter and repaired,overhauled, or replaced as required. Items shown here should be overhauled or replaced duringthe regular maintenance periods falling due nearest to the specified limit. This is not applicable forChapter 4 items.

B. Items that are underlined are Chapter 4, Airworthiness Limitations requirements. Refer toChapter 4, Airworthiness Limitations for additional information.

C. The replacement life for each component listed in this section applies to the part throughout its life onthe original installation and on later installations. The life (number of hours or number of landings) mustbe recorded individually for these components and must remain with the component during removal.For example, if a component is removed for overhaul, it must be tagged with the life (number of hoursor number of landings) to the date of removal and this tag must remain with the component throughoutthe overhaul process. (Overhaul of a component does not zero time the life of the component.) Whenreceived from overhaul and installed on an airplane, the life of the component must be recorded toallow continued accumulation toward the life limit.

D. Components which have exceeded overhaul or replacement times due to a current change in theinspection program, may continue in service, if the component is serviceable, and the component isimmediately scheduled for overhaul or replacement component ordered. Possible delays resultingfrom component shortage or overhaul schedules shall not result in extending time past 60 days.

2. Schedule

A. Air Conditioning (Chapter 21).(1) Vapor Cycle Cooling System

(a) Compressor Drive Motor Brushes (Compressor Motors 1134104-1, -5) - Replace every 500compressor hours.

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and ComponentMaintenance Manual 21-00-06.

B. Communications (Chapter 23).(1) Cockpit Voice Recorder Underwater Locating Device (ULD) Battery - Replace every 6 years.

Refer to Task 23-90-70-960.

C. Equipment and Furnishings (Chapter 25).(1) Locator Beacon Battery Pack

(a) Artex 110-4 - Replace every 2 years. Refer to Task 25-90-60-960.(b) Artex 110-406 - Replace every 5 years. Refer to Task 25-90-60-960.(c) Artex C406-2 - Replace every 5 years. Refer to Task 25-90-60-960.(d) Artex C406-N - Replace every 5 years. Refer to Task 25-90-60-960..

D. Fire Protection (Chapter 26).(1) Fire Bottle Cartridges. Refer to Table 1.

(a) Engine Fire Bottle Cartridge. Refer to Task 26-90-30-960.(b) APU Fire Bottle Cartridge. Refer to Task 26-90-30-961.(c) Cockpit or Cabin Mounted Halon-type Fire Extinguishers - Replace, or empty, inspect for

damage and recharge every 6 years.(d) Cockpit and Cabin Mounted Halon-type Fire Extinguishers - Complete a hydrostatic test (if

bottle has been recharged) every 12 years. Refer to Task 26-90-20-841.

5-11-00 Page 1© TEXTRON AVIATION INC. Jul 1/2016

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Fire Bottle Cartridge Life

CARTRIDGE PART NUMBER SERVICE LIFE (YEARS) TOTAL LIFE (YEARS)

13083-5 6 6

AE13083-5 The combined shelf-life andthe service life cannot exceed

ten (10) years.

10

NOTE: Service life is the amount of time the explosive cartridge is installed in a fireextinguisher. Service life of any particular explosive cartridge can not be extended.

NOTE: Total life starts on the day the cartridge is made and must be replaced at a specifictime. A date (month/year) is stamped or marked on the plastic bag containing thecartridge or on the cartridge body. Total life cannot be extended and includesany mix of time the explosive cartridge is kept ”on the shelf” and/or installed in afire extinguisher.

(2) Portable Fire Extinguisher Bottle - Complete the NFPA required internal inspection every 6 years(refer to Task 26-90-20-842).

(3) Portable Fire Extinguisher Bottle - Complete the NFPA required hydrostatic test every 12 years(refer to Task 26-90-20-841).

(4) Engine and Auxiliary Power Unit Fire Extinguishing Bottles - Complete the required hydrostatictest every 5 years (refer to Task 26-21-01-780)

E. Flight Controls (Chapter 27).(1) Flaps

(a) Inboard and Outboard Flap Rollers (Part Number S3049-5F8) - Replace every 5000landings.

(2) Elevators(a) Elevator Trim Cables

1 Aft Elevator Trim Cable Assembly (Part Number 6660003-1) - Replace every 4800hours

NOTE: The trim cable assembly is made using an up, down and center cable(Part Number 6660002-35, -36, -67).

F. Indicating/Recording Systems (Chapter 31).(1) Flight Data Recorder Underwater Locating Device (ULD) Battery - Replace every 6 years. Refer

to Task 31-90-30-960.

G. Landing Gear (Chapter 32).(1) Landing Gear Extension/Retraction System

(a) Emergency Pneumatic Storage Bottle - Replace (Discard) every 24 years. Refer to Task32-30-09-281.

(b) Pneumatic Storage Bottle - Complete the required hydrostatic test every three years. Referto Task 32-30-09-280.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Main Landing Gear

NOTE: The attaching hardware related to this installation is to be replaced whenever theassociated components are replaced.

NOTE: The attaching hardware can be used again if a rental component is to be installedfor no more than 100 landings. The attaching hardware can also be used again ifthe original gear is to be installed again. If a replacement gear is installed, all of theattachment hardware must be replaced.
























CESSNA®MODEL 560XL

MAINTENANCE MANUAL





every 33,300 landings.(d) Nose Landing Gear Actuator (Part Number 9912491-2, -3, -4, -5, -6) - Replace every

33,300 landings.

H. Navigation (Chapter 34).(1) Securaplane Standby Battery - Replace every 4 years. Refer to Task 34-90-20-960.

I. Oxygen (Chapter 35).(1) Oxygen bottle (cylinder) hydrostatic test and discard.

NOTE: DOT Ratings are used to find the correct hydrostatic test and service life intervals.

NOTE: US DOT Exemption E 8162 was superseded by US DOT Special Permit SP 8162dated May 11, 2007. DOT-SP 8162 applies to all cylinders manufactured afterSeptember 30, 2007 and DOT-E 8162 cylinders hydrostatic tested after July 1,2006. Reference AVOX Service Information Letters SIL-35-114 and SIL-35-116.

NOTE: DOT-SP 8162 applies to DOT3FC1850 cylinders.

(a) Hydrostatic test, refer to Table 2 for the correct Hydrostatic Test Interval and related Task.

Table 2. Oxygen Bottle Hydrostatic Test Intervals

DOT RATING HYDROSTATIC TEST INTERVAL TASK NUMBER

DOT3AA 5 years (NOTE 1) 35-90-00-840

DOT-SP 8162 5 years 35-90-00-840

NOTE 1: The DOT3AA text requirement is 5 years. If the hydrostatic test is overdue, you can complete the testat the next inspection phase interval.

(b) Discard, refer to Table 3 for the correct Service Life Interval and related Task.

Table 3. Oxygen Bottle Service Life Intervals

DOT RATING SERVICE LIFE INTERVAL TASK NUMBER

DOT3AA N/A N/A

DOT-SP 8162 15 years 35-90-00-960


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Crew Oxygen Mask - Overhaul every 6 years. Refer to Task 35-90-10-840 Crew MasksRestoration (Overhaul).

NOTE: Under normal environmental conditions and use, the crew oxygen masks must beoverhauled every 6 years. If the crew oxygen masks are exposed to environmentsthat accelerate aging of elastomer components, periodic inspection may warrantshorter intervals between overhaul periods.

(3) Protective Breathing Equipment - Discard every 10 years. Refer to Task 35-30-00-960.

J. Fuselage (Chapter 53)(1) Trunnion Attach Fitting Assemblies



(2) Actuator Fitting Assemblies(a) Actuator Fitting on Airplanes 560-5001 thru 560-5500, (Part Number 6211191-2, -3) -

Replace every 25,500 landings.

NOTE: Actuator Fitting Part numbers 6211191-2, -3 are components of the6211190-41, -42 Actuator Fitting Assemblies.

(b) Actuator Fitting Assembly on Airplanes 560-5501 and On, (Part Number 6611591-9, -10)- Replace every 25,500 landings.

K. Wing (Chapter 57)(1) Trunnion Attach Fitting Assemblies






23,800 landings.

L. Powerplants (Chapter 71).(1) Forward and Aft Engine Mount Isolators - Replace at every second Engine Overhaul.

NOTE: The engine mount isolators do not have an hourly replacement requirement. Theyare replaced by the number of engine overhauls. You can purchase the exchangedor overhauled engine mount isolators, which are approved to be installed asreplacement engine mount isolators, through Citation Parts Distribution.

(a) Forward Engine Mount Isolators - LM-451-SA1 and LM-451-SA4 (Cessna Part Number9912480-1)

(b) Aft Engine Mount Isolators - LM-451-SA2 (Cessna Part Number 9912480-2)

M. Starting (Chapter 80).(1) Starter-Generator - OVERHAUL 1000 hours. Refer to Task 80-90-10-840.(2) APU Starter-Generator - OVERHAUL 1000 APU hours. Refer to Task 80-90-11-840.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

CONTINUOUS INSPECTION

1. Continuous Airworthiness Inspection Program

A. Purpose and Use.(1) As shown in Part 91.409, paragraph (e) of Title 14 of the Code of Federal Regulations, turbojet

airplanes must be inspected in accordance with an authorized inspection schedule. This sectioncontains the continuous inspection program for the Model 560XL recommended by CessnaAircraft Company.

(2) For airplanes registered in countries other than the United States, the procedures specified bythe Airworthiness Authority of that country should be followed.

2. Title 14 of the Code of Federal Regulations

A. General Operating and Flight Rules, Part 91.409.(1) No person may operate a large airplane, or a turbojet multi-engine airplane, or turbo -

propeller-powered multi-engine airplane, or turbine-powered rotorcraft unless the replacementtimes for life-limited parts specified in the aircraft specifications, type data sheets orother documents approved by the Administrator are complied with and the airplane, orturbine-powered rotorcraft including the airframe, engines, propellers, rotors, appliances,survival equipment and emergency equipment, is inspected in accordance with an inspectionprogram selected under the provisions of paragraph 91.409(f) of this section, except that, theowner or operator of a turbine-powered rotorcraft may elect to use the provisions of paragraph91.409(a), (b), (c) or (d) in lieu of an inspection option of paragraph (f).

(2) The registered owner or operator of each airplane or turbine powered rotorcraft described inparagraph 91.409(e) of this section must select, identify in the aircraft maintenance records anduse one of the following programs for the inspection of the aircraft:(a) A continuous airworthiness inspection program that is a part of a continuous airworthiness

maintenance program currently in use by a person holding an air carrier operatingcertificate issued under Part 121, 127, or 135 of this chapter and operating that makeand model aircraft under Part 121 of this chapter and maintaining it under paragraph135.411(a) (2) of this chapter.

(b) An approved aircraft inspection program approved under paragraph 135.419 of this chapterand currently in use by a person holding an operating certificate under Part 135 of thischapter.

(c) A current inspection program recommended by the manufacturer.(d) Any other inspection program established by the registered owner or operator of that

airplane or turbine-powered rotorcraft and approved by the Administrator under paragraph(g) of this section. However, the Administrator may require revision to this inspectionprogram in accordance with the provisions of Part 91.415.

(3) Each operator shall include in the selected program the name and address of the personresponsible for scheduling the inspections required by the program and make a copy of thatprogram available to the person performing inspections on the aircraft and, upon request, tothe Administrator.

(4) Each operator of an airplane or turbine-powered rotorcraft desiring to establish or change anapproved inspection program under paragraph (f)(4) of this section must submit the programfor approval to the local FAA Flight Standards District Office having jurisdiction over the area inwhich the aircraft is based. The program must include the following information:(a) Instructions and procedures for the conduct of inspections for the particular make and

model airplane including necessary tests and checks. The instructions and proceduresmust set forth in detail the parts and areas of the airframe, engines, propellers, rotors andappliances, including emergency equipment required to be inspected.

(b) A schedule for performing the inspections that must be performed under the programexpressed in terms of the time in service, calendar time, number of system operations,or any combination of these.

(c) When an operator changes from one inspection program, under paragraph (f) of thissection, to another, the time in service, calendar times, or cycles of operation accumulatedunder the previous program must be applied in determining inspection due times underthe new program.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

3. Construction

A. Following is the recommended continuous inspection and maintenance schedule for Model 560XLAirplanes.

B. The program is divided into five primary phases (Phases 1 through 5) which are the main repetitivephases that make up the basic requirements of the inspection program. The remaining phases includeall of the remaining inspection items.

NOTE: Phase B is also provided and is required to be accomplished at 150-hour intervals whenPhases 1 through 4 are combined at 300-hour intervals (Method 3 of accomplishingPhases 1 through 4).

C. The inspection program is divided into phases to better enable the continuous type inspection tobe accomplished. Recommended continuous type inspection may be accomplished by one of threemethods.

D. The remaining sections in the 5-12-XX series contain signoff sheets which are listings of inspectionitems in zone order. The last two digits (XX) of the chapter/section/subject correspond to the inspectionphase.

E. For a complete inspection program when the continuous inspection program is selected, additionalinspections shall be complied with as follows:(1) Continuous - All phases shall be performed. Tasks are defined within the individual chapters.(2) Component Time Limits - Refer to 5-11-00. Components that must have maintenance done at

a specified time (does not include on condition items).(3) Unscheduled Maintenance - Refer to 5-50-00. This includes the following:

• Hard or Overweight Landing Check• Overspeed Check• Severe Turbulence and/or Maneuver Checks• Inadvertent In-Flight Thrust Reverser Deployment• Lightning Strike Check• Foreign Object Damage Check• Towing with Large Fuel Unbalance or High Drag/Side Loads Due to Ground Handling

Check• Airplane Operation Through Deep Standing Water• Nose Landing Gear Tow Limits Check

4. Continuous Inspection Program Procedure

A. The five primary phases (Phases 1 through 5) are the core of the continuous inspection program. Theremaining phases, which have the higher time inspection requirements, are not included in the Phases1 through 5 continuous inspection cycle. There are three plans (Method 1, 2 and 3) which put togetherthe different methods to do Phases 1 through 5 in a continuous inspection program. Each plan givesdifferent inspection intervals to align with the requirements of the individual operators. Refer to Threeoptional methods to complete Phases 1 through 4 for the continuous inspection program chart thatgives which phases are due at a specific hourly interval for each plan.

B. The five primary phases (Phases 1 through 5) constitute the core of the continuous inspectionprogram.(1) Phases 1 through 4, which each have an interval of 300 hours, are designed to be accomplished

in a continuous, repetitive 300-hour cycle by three different optional methods as detailed in ItemG.

(2) Phase 5, which has an interval of 1200 hours, is designed to be accomplished in a continuous,repetitive 1200-hour cycle.

C. The remaining phases are to be accomplished when due or at any time earlier to coincide with aconvenient inspection or maintenance downtime.

D. The calendar time limits (such as 36 calendar months in Phase 5) must be taken into considerationfor airplanes accumulating less than the specified hours in the calendar period.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

E. Component Time Limits (5-11-00) lists all components which are to be replaced or overhauled ona scheduled basis. Those items which are underlined are also listed in Chapter 4, AirworthinessLimitations. Replacement or overhaul of items listed is required to be accomplished when due orearlier to coincide with a convenient inspection or maintenance downtime.

F. An operator may elect to perform the recommended inspections on a schedule other than thatspecified. Any inspection schedule requiring the various inspection items detailed in this chapterto be performed at a frequency equal to that specified here or more frequently is acceptable. Anyinspection item performed at a time period in excess of that specified herein must be approved bythe appropriate regulating agency.

G. Three optional methods to complete Phases 1 through 4

NOTE: Operators changing from one method to another of performing Phases 1 through 4, mustensure that time from the previous inspection to the next inspection of an item does notexceed intervals indicated in this manual.

METHOD 1: Phase 1 through Phase 4 inspections are based on 300-hour cycles, with one of thephase inspections accomplished every 75 hours of airplane operation. Applicable additional phasesare integrated at their due times with the first four phases. At the completion of Phase 4, Phase 1 willbecome due 75 hours later and the cycle is repeated.

75-HOUR 150-HOUR 225-HOUR 300-HOUR

PHASE 1 X

PHASE 2 X

PHASE 3 X

PHASE 4 X

METHOD 2: Phase 1 and Phase 2 are combined and accomplished at alternate 150-hour intervals,with Phase 3 and Phase 4 being performed at the next 150-hour interval. Applicable additional phasesare integrated at their due times with the first four phases. At the completion of Phase 3 and Phase4, Phase 1 and Phase 2 will become due 150 hours later and the cycle is repeated.


PHASE 1 X

PHASE 2 X

PHASE 3 X

PHASE 4 X

METHOD 3: Phase 1 through Phase 4 are all combined and accomplished at 300-hour intervals.Applicable additional phases are integrated at their due times with the first four phases. Those thatcannot be so integrated must be performed early or separately.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL


PHASE B X

PHASE 1 X

PHASE 2 X

PHASE 3 X

PHASE 4 X

NOTE: With all of the phases combined into 300-hour intervals, an inspection is required to beaccomplished on certain items every 150 hours. These inspections are listed in Phase B.The 150-hour inspections are listed in two of the phases. Duplicated items need only beaccomplished one time when combining phases.

H. Phase 5 is to be accomplished all at once, each 1200 hours concurrently with accomplishment at theend of the fourth cycle of Phases 1 through 4.

I. Hour Interval Items.(1) Upon completion of Phase 1 through Phase 4, a continued program will repeat the cycle. When

you reach the 1200-hour interval, Phase 5 will be performed.(2) Special inspections (Phases 6 and on) having hour interval will be performed with a phase

corresponding to that particular hour interval.

J. Time Limit Items.(1) Components and/or systems having time limits of 12 calendar months, 24 calendar months,

36 calendar months, 48 calendar months, 60 calendar months, etc., may be performed at thespecific time limit or with a phase inspection corresponding to interval.

5. Inspection Time Limitations

NOTE: Any inspection time limitation found in Chapter 5 that is also required in Chapter 4 shall not beextended. Any inspection required by the Code of Federal Regulations (CFR) and ReducedVertical Separation Minimums (RVSM) shall not be extended.

A. Phases 1, 2, 3, 4 and 5 due points can be extended for maintenance scheduling purposes only asprovided below:(1) Phases 1, 2, 3 and 4 can be extended up to a maximum of 30 flight hours or two calendar months

beyond the due point.(2) Phase 5, 49, 51, and 60 can be extended up to a maximum of 100 flight hours or two calendar

months beyond the due point.(3) The Phase B, when used, can be extended up to a maximum of 30 flight hours or two calendar

months beyond the due point.(4) Phase 59 can be extended up to a maximum of 50 flight hours or one calendar month beyond

the due point.

B. All remaining phase due points can be extended for maintenance scheduling purposes only up to amaximum of 10 flight hours from the due point for hourly driven inspections and 1 calendar month forcalendar driven inspections.

C. Any portion of the allowable extension used need not be deducted from the subsequent due point.

D. Any inspection program based upon the intervals of the items in this chapter or more frequent intervalsis acceptable.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

6. Program Startup

NOTE: This procedure for program startup applies only to airplanes that have been previously usingan inspection program other than Cessna's recommended Continuous Inspection Program.

A. To start this continuous inspection program, the following steps must be accomplished for airplanesother than those newly manufactured.(1) Conduct a complete airplane inspection by performing Phases 1 through 5.(2) Start the program at Check Number 1. (Refer to Continuous Inspection Program Procedure)(3) Continue performing inspections in the normal manner.

7. Logbook Forms, Pilot Information

A. Airplane Flight Log, Section 1.(1) Provides a convenient place to maintain individual and cumulative flight records, total hours on

the airplane and each engine, total landings for the airplane and the cycles of each engine.(2) The original of the Flight Log form is placed in Section 1 of the FAA Approved Airplane Flight

and Maintenance Logbook and kept as part of the permanent airplane log.

B. Form Completion.(1) The basic information at the top of this form should be completed. Enter the number of the page

as it sequentially falls in the logbook section beginning with 1. The line entitled "AccumulatedTotals Brought Forward" is the record information which is being carried forward from theprevious page. This is a journey log and one line represents one flight. Under the followingcolumns should be recorded:

1. The date of each flight.

2a. City where flight originated.

2b. City of flight destination.

3. The number of persons aboard, including crew.

4. Distance of flight in nautical miles.

5. The flight duration in hours and tenths from flight hour meter.

6. Accumulated total airplane time in hours and tenths.

7. Accumulated total time for engine 1 in hours and tenths.

8. Accumulated total time for engine 2 in hours and tenths.

9. Number of landings this flight.

10. Accumulated total airplane landings.

11. Accumulated engine 1 cycles.


13. The discrepancy sheet number column provides a reference to the airplanediscrepancy form which details the airplane discrepancies on particular flight.If there are no discrepancies, NONE should be entered in this column. Thisprovides the pilot with a convenient method of determining whether previousairplane discrepancies have been corrected.

14. The last name of the pilot and copilot for each flight should be recorded in thelast column.

15. The line "Accumulated Totals" should be filled in when the form is completelyfilled or at the end of the CESCOM reporting period.

(2) The totals of these lines should be carried forward to the line entitled "Accumulated TotalsBrought Forward" on the next airplane flight log form used.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(3) The original (white sheet) should be placed in the Airplane Flight and Maintenance Logbook inSection 1.

(4) The first copy (pink sheet) should be mailed to the address at the top of the form and is used byCESCOM to report airplane utilization.

(5) The second copy (yellow sheet) provides an extra customer copy and should be filed at theairplane base.

Table 1. MODEL 560XL Logbook includes airplane and engine logs in the following:

SECTION 1 Flight Time Information SECTION 6 Left Engine Maintenance

SECTION 2 Pilot Squawk on Last Flight SECTION 7 Left Engine Service Bulletin

SECTION 3 General Airplane Maintenance SECTION 8 Right Engine Maintenance

SECTION 4 Service Bulletin SECTION 9 Right Engine Service Bulletin

SECTION 5 Engine Change SECTION 10 Service Condition Reports

SECTION 11 Component Master InventoryCross-Reference List

Table 2. New pages for the airplane logbook are listed below:

Airplane SECTION 1 Airplane Flight Log

Airplane SECTION 2 Airplane Discrepancies

Airplane SECTION 3 Maintenance Transaction Report


Airplane SECTION 5 Engine Change Record

Left Engine SECTION 6 Maintenance Transaction Report

Left Engine SECTION 7 Maintenance Transaction Report

Right Engine SECTION 8 Maintenance Transaction Report

Right Engine SECTION 9 Maintenance Transaction Report

Airplane SECTION 10 Service Condition Report

SECTION 11 Component Master Inventory Cross-Reference List

C. Mechanic Information:(1) Mechanics will fill out the airplane and engine maintenance records and use "Maintenance

Transaction Report" for additional pages in the airplane logbook in Sections 3, 4, 6, 7, 8 and 9.(2) Place copies of the inspection program selected (sample letter), inspection record of phase

due and completed in the front of the airplane log, for pilot’s and mechanic’s; information oninspection coming due.

8. Maintenance Transaction Report

A. Fill Out Maintenance Transaction Report as Follows.(1) Maintenance Log - Airplane or engine entry.(2) Date - Put the month, day and year the maintenance is performed.(3) Airplane Serial Number and Airplane Registration Number.(4) Total Airplane Hours.(5) Complete When Applicable.(6) Write in the three-letter identifier for the city in which the maintenance transaction is performed.

(a) Item Name - The component for which the transaction is being performed.(b) Position - Left or Right, Inboard or Outboard.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(c) Part Number.(d) Serial Number of Installed Part.(e) Removal Reason - Check the box which corresponds to the reason for the component

removal.(f) Status of Installed Part - Check the status of the part installed. Page 3 (Yellow) should go

to Airplane base files.(g) Time Between Overhaul (TBO) - Check one of the boxes under (check one); next, place

the TBO change in the blank and check one of the TBO controls. If the (OK as is) box ischecked, nothing else need be done in this box.

(h) Time Since Overhaul (TSO) - If an overhaul component is being installed, place its presentTSO in the block and check the type of control.

(i) Section and Page Numbers.(j) Type of Maintenance.(k) For Information and other Log Entries:(l) Enter pages in logbook. Put Page 1 (white) in logbook. Put Page 2 (pink) in CESCOM.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 1

Date: _______________

Registration Number: _______________

Serial Number: _______________

Total Time: _______________

1. Description

A. Phase 1 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, intervalinspection items contained in the forward nose section, cockpit area, instrument panel, controlpedestal and cabin area. Items from other areas are included to meet their required time interval.

B. Inspection items are listed in order of the zone in which the inspection is to be performed. A descriptivestatement of the inspection requirement and the Item Code Number for cross reference to section5-10-01 is provided. In many instances, tasks define more specifically the scope and extent of eachrequired inspection. These tasks are printed in the individual chapters of this manual.

C. The right portion of each page provides room for the mechanic's and inspector's initials and remarks.These pages may be reproduced as a checklist for use when performing this inspection phase.

2. General Inspection Criteria

A. During accomplishment of each of the specific inspection tasks within this inspection document,additional general inspections of the surrounding areas should be performed while access isavailable. These general inspections are intended to detect obvious conditions which may warrantfurther action.

B. If a component or system is disturbed (due to maintenance being performed) after completion of aninitially required task, then that specific task must be reconfirmed after completion of any maintenancebefore returning the system or component to service.

ITEM CODENUMBER

TASK ZONE MECH INSP REMARKS

B237002 Cockpit Voice Recorder System (Fairchild A200S) -Complete an operational test. Task 23-70-00-710

AUX

B237004 Cockpit Voice Recorder System (Fairchild FA2100)- Complete an operational test. Task 23-70-00-711

AUX

B243003 Overvoltage System - Perform Functional Test.Task 24-41-02-710

AUX

A324011 Brake Master Cylinders (Airplanes -5001 thru-5500) - Inspect for leaks and security. Inspecthoses for chafing and evidence of damage. Task32-42-02-210

241, 242

B335001 Emergency Lighting System Operational CheckTask 33-50-00-710

BAT

A335002 Emergency Exit Lights - Inspect for security ofinstallation. Task 33-50-02-210

164, 166,251, 252,261, 262

C521000 Door Locks - Lubricate lock tumblers. 211, 212,323, 331,810


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A521001 Cabin Door Inflatable Seal, Secondary Seal- Inspect for security of installation, wear,deterioration and evidence of damage. Task52-10-04-210

810

B527001 Door Warning System - Perform operational check.Task 52-70-00-710

AUX

A530002 Moisture Drain Holes - Inspect airplaneunpressurized area drain holes for obstruction andevidence of corrosion. Task 53-10-05-210

211, 212,411, 412,511, 512,611, 612

A531015 Radome Surface Mounted Lightning Diverter Strips- Inspect for missing segments, corrosion, damageand electrical continuity to airplane structure. Task53-10-10-211

110

B531017 Radome - Check electrical bond. Task 53-10-10-760 110

A561003 Windshield Humpseal Detailed Inspection Task56-11-00-210

241, 242

A562001 Cabin Windows - Inspect windows for scratches,cracks, crazing and deformities. Task 56-20-00-210

251, 252,261, 262

*** End of Inspection Phase 1 Inspection Items ***


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 2

Date: _______________



Total Time: _______________

1. Description

A. Phase 2 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, intervalinspection items contained in the wings, landing gear and tailcone. Items from other areas are includedto meet their required time interval.






ITEM CODENUMBER


B271001 Aileron Trim Tab Functional Test (Free Play) Task27-10-00-220

532

C271001 Aileron Trim Tab Actuator - Lubricate. Task12-21-01-640

532

A272001 Rudder and Rudder Trim Tab - Inspect. Task27-20-00-223

340

C272002 Rudder Trim Tab Actuator - Lubricate. Task12-21-01-640

340

C273002 Elevator Trim Tab Actuators - Lubricate. Task12-21-01-640

351, 352

B301002 Pneumatic Deice System - Perform operational test.Task 30-12-00-710

ENG

A301003 Deice Boots, Empennage - Inspect for securityof installation and evidence of damage. Task30-12-01-210

351, 352

B320001 Landing Gear Extension and Retraction - Performfunctional test. Task 32-01-00-720

AUX


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A321001 Main Gear - Inspect. Task 32-10-00-210 720, 730

D321001 Main Landing Gear Breather Vent Discard Task32-10-00-960

720, 730

A322001 Nose Gear - Inspect. Task 32-20-00-210 710

A322002 Shimmy Damper - Inspect for security, evidence ofdamage and proper service. Task 32-20-01-610

710

C322003 Nose Landing Gear - Lubricate. Task 12-21-02-640 710

C322005 Main Landing Gear Lubrication - Perform. Task12-21-02-642

720, 730

A323001 Uplock Assembly - Inspect. Task 32-30-05-210 710, 720,730

A324003 Main Gear Wheel Brakes - Check brake wear. Task32-42-01-220

720, 730

A528001 Main Landing Gear Door - Inspect hinge forcorrosion and doors for evidence of damage. Task32-10-00-211

720, 730

A528002 Nose Landing Gear Door - Inspect doors forevidence of damage and signs of tire rub. Task32-20-00-211

710

A551001 Horizontal Stabilizer External Inspection - Inspect.Task 55-10-01-210

351, 352

A551002 Horizontal and Vertical Stabilizer Aft Edge - Visuallyinspect for separation of the bond between the skinand doubler. Task 55-00-00-210

351, 352,340

A553001 Vertical Stabilizer External Examination - Inspect.Task 55-30-01-210

340

A575002 Flaps - Check drain holes for obstruction. Task57-50-04-211

512, 522,612, 622

A761101 Fuel Control Unit (FCU) Throttle Lever CutoffFunctional Test (Airplanes-5001 thru -5196 NotIncorporating SB560XL-76-03) Task 76-10-00-620

410, 420

A801001 Starter-Generator - Inspect for security ofinstallation. Inspect terminal block and electricalconnections for cleanliness and evidence of damagefrom heating and arcing. Task 80-10-00-210

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 3

Date: _______________



Total Time: _______________

1. Description

A. Phase 3 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, intervalinspection items contained in the tailcone area. Items from other areas are included to meet theirrequired time interval.


C. Item Code A215201 was deleted from this document in Revision 33.

D. The right portion of each page provides room for the mechanic's and inspector's initials and remarks.These pages may be reproduced as a checklist for use when performing this inspection phase.


A. During accomplishment of each of the specific inspection tasks within this phase, additional generalinspections of the surrounding areas should be performed while access is available. These generalinspections are intended to detect obvious conditions which may warrant further action.


ITEM CODENUMBER


C275001 Flap Rollers Lubrication - Perform Task12-21-01-643

512, 522,612, 622



241, 242

*** End of Phase 3 Inspection Items ***


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 4

Date: _______________



Total Time: _______________

1. Description

A. Phase 4 consists of 150-hour and 300-hour or 24 calendar months, whichever occurs first, intervalinspection items contained in the power plant. Items from other areas are included to meet theirrequired time interval.






ITEM CODENUMBER


B215001 Emergency Pressurization System OperationalCheck Task 21-51-00-712

ENG


710


720, 730

B324003 Main Gear Wheel Brakes - Check parking brake foroperation. Task 32-44-00-711

ENG


710

A711001 Nacelle and Cowling - Inspect the upper andlower cowls, inlet, aft cowling, inboard cowling, oilfiller door and access panels for failed fasteners,security of installation and evidence of damage.Task 71-90-00-212

410, 420

A720003 Engine - Perform general inspection. Task71-00-00-210

410, 420


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER



410, 420

A761102 Fuel Control Unit (FCU) Throttle Lever CutoffFunctional Check (Airplanes -5197 thru -6000,and Airplanes -5001 thru -5196 IncorporatingSB560XL-76-03) Task 76-10-00-620

410, 420

A783012 Thrust Reversers - Inspect. Task 78-31-00-210 410, 420

B783030 Thrust Reverser System Functional Check Task78-90-30-720

AUX


410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE B

Date: _______________



Total Time: _______________

1. Description

A. Phase B consists of 150-hour inspection items which must be performed when Phases 1 thru 4 arecombined at 300-hour intervals (Method 3).






ITEM CODENUMBER



710


720, 730



710


241, 242

5-12-0B Page 1© TEXTRON AVIATION INC. Jul 1/2015

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER



410, 420


410, 420

*** End of Inspection Phase B Inspection Items ***

5-12-0B Page 2© TEXTRON AVIATION INC. Jul 1/2015

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 5

Date: _______________



Total Time: _______________

1. Description

A. Phase 5 consists of items to be inspected every 1200 hours or 36 calendar months, whichever occursfirst.






ITEM CODENUMBER


A110001 Required Interior and Exterior Placards and Decals- Examine for security of installation and legibility.Task 11-00-00-210

All Zones

A212002 Cabin Air Distribution Check Valves DetailedInspection Task 21-22-00-210

161, 162

B213000 Pressurization System Functional Check Task21-30-00-721

ENG

B213002 Cabin Altitude Pressure Switch Functional TestTask 21-31-05-720

245

B215000 Environmental System - Perform operational check.Task 21-51-00-710

ENG

B216001 Nose Avionics Cooling Fan - Perform operationalcheck. Task 21-25-00-710

AUX

A216001 Nose Avionics Cooling Fan - Inspect. Task21-25-00-210

110

B216002 Instrument Panel Cooling - Perform operationalcheck. Task 21-24-00-710

AUX


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A216002 Cockpit Zone Temperature Assembly - Inspect.Task 21-61-00-710

246

A216003 Cabin Zone Temperature Assembly - Inspect. Task21-61-00-711

261

A217002 Aspirator (Water Separator Nozzle) - Inspect nozzlefor heat or other damage. Task 21-51-00-210

312

A221001 Aileron Servo Mount and Actuator - Inspect. Task22-11-01-210

314

A221002 Rudder Servo Mount and Actuator - Inspect. Task22-11-01-211

321

A221003 Elevator Servo Mount and Actuator - Inspect. Task22-11-01-211

321

B221004 Autopilot Disengagement and Warning System -Perform operational test. Task 22-11-03-710

AUX

A231001 High Frequency Antenna and Tensioning Unit -Inspect. Task 23-11-00-210

312, 340

A236001 Static Discharging System Functional Check Task23-90-60-720

331, 332,532, 540,632, 640

A242001 Nose Area Electrical Components - Inspect. Task24-00-00-210

110, 211,212, 221,222

A245002 Side Console Equipment Panel - Inspect. Task24-50-02-211

245, 246

A245003 Aft Power Junction Box - Inspect. Task24-50-03-210

311, 312

A245005 Interior Junction Box Components - Inspect. Task24-50-05-210

261

A251001 Crew and Cabin Seats - Inspect. Task 25-11-01-210 241, 242,251, 252,261, 262

A251002 Pilot and Copilot Seat Track Stops - Inspectfor damage and security of installation. Task25-11-01-211

241, 242

B262010 Fire Extinguishing System - Perform functional test.Task 26-21-00-720

AUX

A271001 Aileron and Aileron Trim Tab Security of Installation- Examine. Task 27-10-00-211

244, 247,248, 532

B271002 Aileron and Trim Tab - Check Travel. Task27-10-00-221

532, 632

A271004 Aileron Outboard Wing Control Cable FunctionalTest Task 27-10-00-212

512, 522,532, 612,622, 632


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


B272003 Rudder - Check rudder and rudder trim tab travel.Task 27-20-00-221

340

A272004 Rudder Pedals - Inspect. Task 27-20-00-224 241, 242

A273001 Elevator and Elevator Trim Tab External VisualInspection. Task 27-31-00-211

351, 352

B273003 Elevator and Elevator Trim Tab - Check travel. Task27-31-00-221

351, 352

B273004 Elevator Trim Tab - Check elevator trim tab freeplay. Task 27-31-00-220

351, 352

A273007 Control Column - Examine. Task 27-31-02-210 141, 142,241, 242

A273009 Elevator Linkage - Inspect. Task 27-31-00-212 340

B274001 Takeoff Warning System Sensors - Operationalcheck. Task 27-40-00-712

AUX

B274002 Two Position Horizontal Stabilizer - Operationalcheck. Task 27-40-00-710

AUX

C274002 Horizontal Stabilizer Actuator Reservoir - Oilleakage acceptance criteria and oil level check.Task 12-21-01-641

340

A275001 Flap Drive System - Inspect. Task 27-51-00-210 142, 153,163, 166

B275003 Flaps - Check flap travel. Task 27-51-00-220 512, 522,612, 622

B275004 Flap Approach Warning Switch - Performoperational check. Task 27-51-00-710

AUX

A276001 Speed Brake System Detailed Inspection Task27-61-00-210

512, 522,612, 622

A277002 Control Lock Assembly - Inspect for security ofinstallation, wear and corrosion. Task 27-71-00-210

151

B277003 Control (Gust) Lock System Operational CheckTask 27-71-00-710

235

A281001 Fuel Storage System Detailed Inspection Task28-10-00-210

511, 512,521, 522,531, 532,611, 612,621, 622,631, 632

B282001 Fuel Boost Pump and Scavenge Ejector Pump -Perform operational test. Task 28-20-00-710

AUX

B284001 Low Fuel Warning System Functional Test Task28-42-00-710

AUX

A291001 Hydraulic Panel Assembly and Components -Inspect. Task 29-11-06-210

313


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


D291002 Hydraulic System Filters Discard Task 29-11-04-901 313

B301001 Bleed Air Anti-Ice Systems Operational Check(Airplanes -5001 thru -6000) Task 30-11-00-710

ENG

A301004 Deice Control Valves - Inspect for corrosion,security of installation. Task 30-12-02-210

311, 321

A301005 Deice Pressure Switches - Inspect for corrosion,security of installation and damaged electricalcomponents. Task 30-12-02-211

322

B304001 Nose Compartment Overtemperature SwitchFunctional Test Task 30-40-00-710

AUX

A311001 Instrument Panel Area - Inspect. Task 31-10-00-210 235

B313004 Flight Data Recorder System Functional CheckTask 31-90-30-720

322

A323002 Emergency Extension System Cables - Inspect.Task 32-30-08-210

141, 151,161, 512,612, 710

A323003 Emergency Gear Release Rigging FunctionalCheck. Task 32-30-08-720

512, 612

A324005 Brake Reservoir Visual Inspection (Airplanes -5001thru -5500) Task 32-42-00-210

221

D324006 Brake Reservoir Air Filter Replacement (Airplanes-5001 thru -5500) Task 32-42-00-902

222

D324007 Reservoir Supply Line Filter Cleaning (Airplanes-5001 thru -5500) Task 32-42-00-131

221

D324008 Hydraulic Pack Assembly Filter Replacement(Airplanes -5001 thru -5500) Task 32-42-00-901

211

B324009 Antiskid System Functional Test (Airplanes -5001thru -5500) Task 32-42-00-710

AUX

B324010 Emergency Brake System - Perform operationaltest. Task 32-42-09-710

AUX

A324400 Brake Reservoir Visual Inspection (Airplanes -5501and On) Task 32-44-00-210

313

D324400 Vent Filter Element Replacement (Airplanes -5501and On) Task 32-44-00-960

313

B324401 Antiskid Brake System (Airplanes -5501 and On) -Complete a functional test. Task 32-44-00-710

AUX

D324401 Hydraulic Pump Assembly Filter Replacement(Airplanes -5501 and On) Task 32-44-00-961

313

A325001 Nose Steering Arm and Support Bracket, Bungeeand Bellcrank - Inspect for security, wear, corrosion,failed fasteners and evidence of damage. Task32-50-00-210

710

A325002 Nose Steering Cables - Inspect. Task 32-50-00-730 211, 241


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A332001 Indirect Cabin Fluorescent Lighting (Airplanes -5001thru -5349) - Inspect high voltage wiring aboveheadliner for security of installation and condition ofelectrical wire. Task 33-20-01-210

251, 252,261, 262

A335001 Emergency Lighting Battery Packs - Inspect. Task33-50-00-210

241, 261

B341005 Angle-of-Attack System - Perform Self-TestProcedure and the Landing Gear Extended andSquat Switch Logic Test. Task 34-14-01-720

AUX

A342001 Magnetic Compass Inspection (Airplanes -5001 thru-5500, and Airplanes -5501 thru -6000 IncorporatingSB560XL-34-61) - Examine for correct installation,a clean surface, and signs of damage. Make surethat the current compass card is installed. Task34-24-01-210

241

B342001 AHRS, Standby HIS-315 and Standby MagneticCompass Accuracy Check - Perform Task34-21-01-710

ENG

A351001 Oxygen Cylinder, Supply Pressure Regulator andShutoff Valve - Inspect for security of installation,corrosion, cleanliness of the area and evidence ofdamage. Verify valve is safetied in the ON position.Task 35-01-00-210

212

B351001 Passenger Oxygen System Functional Test Task35-01-00-710

AUX

A351002 Crew Oxygen Mask - Inspect masks and hoses fordeterioration, cleanliness and proper stowage. Task35-10-01-210

241, 242

D361001 Particulate Trap Restoration (Cleaning) NOTE: Thissupplies data to clean the Cabin Door and OutflowValve particulate traps. Task 36-15-00-170

161

B383001 Externally Serviceable Toilet Functional Check Task38-30-02-720

262

B383003 Drain Lines - Perform an operational check. Task38-30-00-710

151, 162

A521003 Cabin Door and Door frame - Inspect for cracks,loose or failed fasteners, damaged locking pins,worn or damaged receptacles and indications ofstructural damage. Task 52-10-00-211

251

A521004 Cabin Door Detailed Inspection Task 52-10-00-210 810

A522001 Emergency Exit Door Detailed Inspection Task52-20-00-210

820

A524001 Tailcone Access Door - Inspect for proper operationand evidence of damage. Task 52-40-00-210

312

A524002 Nose Compartment Doors - Inspect for security ofinstallation. Task 52-40-01-210

211, 212


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A530001 Pressurized Area Moisture Seals - Inspect. Task53-10-05-160

141, 151,161, 162

A531004 Aft Tailcone Components - Inspect. Task53-10-12-210

321, 322

A531005 Forward Tailcone Components - Inspect. Task53-10-12-211

311, 312

A531006 Fuselage Internal Components - Inspect. Task53-10-11-210

141, 142,151, 152,161, 162

A531009 Emergency Exit Door Frame - Inspect for cracks,loose or failed fasteners and any indication ofstructural damage. Task 53-10-11-212

820

A531011 Nose Area - Inspect all structures for security ofinstallation, cracks, corrosion. Task 53-90-00-216

110, 211,212, 221,222

A531012 Control Pedestal - Inspect. Task 53-20-02-210 243

A531013 Stinger Assembly - Inspect for security ofinstallation, corrosion and evidence of damage.Task 53-90-00-215

321, 322

A531016 Radome - Inspect. Task 53-10-10-210 110

A532002 Nose Gear Wheel Well - Inspect nose landing gearattach fittings, supporting structure and remainderof wheel well for cracks, failed fasteners, corrosionand evidence of damage. Task 53-00-00-210

710

A532003 Main Gear Wheel Well - Inspect main landing gearattach fittings, supporting structure and remainderof wheel well for cracks, failed fasteners, corrosionand evidence of damage. Task 57-10-00-210

720, 730

A533001 Fuselage Exterior Skin - Inspect for cracks, loose orfailed fasteners and evidence of structural damage.Task 53-30-01-211

141, 142,151, 152,161, 162,231, 232,241, 242,251, 252,261, 262

A541001 Nacelle Firewall - Inspect for damage, deterioratedfirewall sealant and corrosion. Task 54-50-01-210

411, 412

A541002 Pylon - Inspect for failed fasteners, evidence ofstructural damage and pylon skin cracks. Task54-50-01-211

411, 412

C551003 Horizontal Stabilizer Scissor Fitting Bolts Lubrication- Perform. Task 12-21-01-642

340

A551003 Horizontal Stabilizer Internal Examination - Inspect.Task 55-10-01-211

351, 352


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A553002 Vertical Spar Pivot Fitting Lower Flange andClip Inspection (This inspection is necessary forAirplanes that have not replaced the one-piece clipwith a two-piece assembly.) Task 55-30-01-211

340

A553003 Vertical Stabilizer Internal Examination - Inspect.Task 55-30-01-212

340

A555001 Horizontal Stabilizer - Inspect the elevator attachpoints and carry-thru for evidence of damage. Task55-00-00-211

351, 352

A555002 Vertical Stabilizer - Inspect the rudder and verticalstabilizer attach points for evidence of damage.Task 55-00-00-212

340

A561001 Cockpit Windshield and Side Windows DetailedInspection (Delamination) Task 56-11-00-212

241, 242

A561002 Windshield Retainer Screws Functional Test(Torque Inspection) Task 56-11-00-280

241, 242

A573001 Wings - Inspect external skin and access panels forcracks, failed fasteners and evidence of damage.Task 57-10-00-212

511, 512,521, 522,531, 532,540, 611,612, 621,622, 631,632, 641

A575003 Flaps and Flap Tracks - Inspect. Task 57-50-04-210 512, 522,612, 622

A575004 Flaps - Perform coin tap inspection. Task57-50-04-212

512, 522,612, 622

A711002 Upper Cowling Camloc Hole Detailed InspectionTask 71-11-00-220

410, 420

A711003 Forward and Aft Upper Cowling Edge DetailedInspection Task 71-11-00-221

410, 420

A783018 Thrust Reverser Electrical Junction Box - Inspect.Task 78-31-00-211

312

B801004 Starter Disengage System - Perform operationaltest. Task 80-10-00-710

ENG



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 7

Date:_______________



Total Time: _______________

1. Description

A. Phase 7 consists of items to be inspected every 300 hours.






ITEM CODENUMBER


C783101 Thrust Reverser Lubrication (WC-393 Non-AerosolSpray Lubrication Method) Task 78-31-00-640

AUX

C783102 Thrust Reverser Guide Rods Lubrication(D-5100NS Aerosol Spray Lubrication Method)Task 78-31-00-641

AUX



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 8

Date: _______________



Total Time: _______________

1. Description

A. Phase 8 consists of items to be inspected every six calendar months.






ITEM CODENUMBER


A262002 Portable Fire Extinguisher Bottle Detailed InspectionTask 26-22-00-750

242, 262

A281003 Fuel Filler Cap Lubrication Task 28-11-04-210 531, 631



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 9

Date: _______________



Total Time: _______________

1. Description

A. Phase 9 consists of items to be inspected every 900 hours, +50 or -50 hours, or 24 calendar months,whichever occurs first.






ITEM CODENUMBER


C793002 Engine Oil Change and Oil Filter - Replace. Task79-00-00-610

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 18

Date: _______________



Total Time: _______________

1. Description

A. Phase 18 consists of items to be inspected every year.






ITEM CODENUMBER


A215208 Vapor Cycle Cooling System 12-Month MaintenanceTask 21-52-00-212

321, 322

A245001 Cockpit Circuit Breaker Panels - Inspect. Task24-50-02-210

245, 246

A256002 First Aid Kit Detailed Inspection - Perform Task25-60-01-210

262

A256003 Life Preserver(s) - Inspect. Task 25-60-00-210 241, 242,251, 252,261, 262

D312001 Davtron Digital Clock Battery - Discard Task31-20-01-960

235

A320004 Landing Gear General Visual Inspection (CorrosionInspection) Task 32-00-00-210

710, 720,730

B342002 L3 Com Standby Battery Pack Functional Test(Capacity Check) Task 34-20-00-762

LAB

A351004 Passenger Mask - Inspect masks and hoses fordeterioration, cleanliness and proper stowage. Task35-20-02-210

251, 261


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A353001 Protective Breathing Equipment Detailed InspectionTask 35-30-00-220

251, 252,261, 262

A383002 Externally Serviceable Toilet - Inspect all toiletplumbing, including the tank, for signs of leakage ordamage. Task 38-30-02-210

262

A530014 Nose Landing Gear Wheel Well GeneralVisual Inspection (Corrosion Inspection). Task53-00-00-210

710

A530015 Tailcone Area General Visual Inspection Task53-90-00-218

313, 321,322

A531019 Inspect for corrosion in the lavatory, vanity andrefreshment center area. Task 53-10-11-211

161, 162

A551007 Horizontal Stabilizer Aft Spar Area GeneralVisual Inspection (Corrosion Inspection) Task55-10-01-212

351, 352

A553018 Vertical Stabilizer Aft Spar Assembly GeneralVisual Inspection (Corrosion Inspection) Task55-30-01-213

340

A571017 Aft Wing Spar Area General Visual Inspection(Corrosion Inspection) Task 57-10-00-211

512, 522,532, 612,622, 632

A571021 Main Landing Gear Wheel Well GeneralVisual Inspection (Corrosion Inspection) Task57-10-00-210

512, 612



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 20

Date: _______________



Total Time: _______________

1. Description

A. Phase 20 consists of items to be inspected every 24 calendar months as required by Title 14 of theCode of Federal Regulations 91.411, 91.413 and RVSM certification.






ITEM CODENUMBER


B341006 Air Data Systems (Airplanes -0001 thru -5356) -Perform calibration required by Title 14 of the Codeof Federal Regulations 91.411. Task 34-11-08-710

AUX

B341007 Perform RVSM Skin Waviness Inspection. Task34-11-01-220

141, 142

B341008 Air Data Systems (Airplanes -5357 thru -6000) -Perform calibration required by Title 14 of the Codeof Federal Regulations 91.411. Task 34-11-09-710

AUX

B345001 Transponder Functional Check (Required by 14CFR 91.413) Task 23-90-20-720

AUX


5-12-20 Page 1© TEXTRON AVIATION INC. Jan 1/2014

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 21

Date: _______________



Total Time: _______________

1. Description

A. Phase 21 consists of items to be inspected every two years.






ITEM CODENUMBER


A237001 Cockpit Voice Recorder and ULD - Inspect. Task23-70-00-210

312

B237003 Underwater Locator Beacon Installed on CockpitVoice Recorder - Perform pinger test using DuKanePL-1 tester. Task 23-90-70-720

312

A313001 Flight Data Recorder and Underwater LocatingDevice (ULD) - Inspect. Task 31-30-01-210

322

B313001 Underwater Locating Device (ULD) located on theFlight Data Recorder - Perform operational test.Task 31-30-01-720

322

A530016 Tailcone Under Floor Area and Tailcone Stinger GVITask 53-90-00-219

313, 321,322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 28

Date: _______________



Total Time: _______________

1. Description

A. Phase 28 consists of selected items to be inspected every 100 hours or 12 calendar months.



D. Item Code D243002 was deleted from this Inspection Phase in revision 38.




ITEM CODENUMBER


B245002 Ni-Cad Battery (Saft) Functional Check (CapacityCheck) The inspection interval can be adjustedafter the water loss per cell is established. Refer tothe Battery Service Table. Task 24-90-50-721

321, 322

B245003 Ni-Cad Battery (Marathon) Functional Check(Capacity Check) The inspection interval canbe adjusted after the water loss per cell isestablished. Refer to the Battery Service Table.Task 24-90-50-722

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 30

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B272002 Rudder Trim Tab Functional Test (Free Play) Task27-20-00-220

340

B342004 Securaplane Standby Battery Operational Check(Energy Level) Task 34-20-00-763

211

C783103 Lubrication of the Thrust Reverser Pivot Points(C-5A Antiseize Compound Lubrication Method)Task 78-31-00-642

AUX

D217001 Water Separator Restoration (Cleaning) Task12-19-02-160

312



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 49

Date: _______________



Total Time: _______________

1. Description

A. This phase consists of items to be inspected at the first 6 years or 2400 hours, whichever occurs first,and every 1200 hours or 36 calendar months, whichever occurs first, thereafter.






ITEM CODENUMBER


A533002 Fuselage External Surface Special DetailedInspection (Eddy Current) Task 53-30-01-250

141, 142,151, 152,161, 162,241, 242,251, 252,261, 262



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 51

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A221004 Aileron, Rudder, and Elevator Autopilot ServoCables - Examine. Task 22-11-01-220

314, 321,340

A271005 Aileron Trim Tab Control Cables - Examine. Task27-10-00-222

141, 153,163, 512,522,

A272006 Rudder Trim Tab Control Cables - Examine. Task27-20-00-226

141, 142,153, 163,166, 321,322

A272007 Rudder Bias Control Cables - Examine. Task27-20-00-227

322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 52

Date: _______________



Total Time: _______________

1. Description

A. Phase 52 consists of items to be inspected every 600 hours or 12 calendar months whichever occursfirst and every 200 hours or 3 calendar months whichever occurs first, thereafter.






ITEM CODENUMBER


B243300 Lead Acid Batteries - Check general conditionand security. Check terminals for overheating orburning. Perform battery checks and capacitytest as necessary. NOTE: The inspectionschedule may be adjusted after the useful batterylife is established, based on operations. Task24-33-00-760

313



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 53

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A490001 Auxiliary Power Unit - Inspect. Task 49-00-00-210 321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 58

Date: _______________



Total Time: _______________

1. Description

A. Phase 58 consists of items to be inspected every 500 operating hours of the Auxiliary Power Unit(APU) starter-generator. Phase 58 is to be performed prior to the APU starter-generator overhaul asrequired in Chapter 5-11-00.






ITEM CODENUMBER


A801101 Auxiliary Power Unit (APU) Starter-Generator Brush- Inspect. Task 80-11-00-620

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 59

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A361101 Precooler Heat Exchanger General VisualInspection Task 36-11-03-210

411, 412

A561104 Cockpit Openable Aft Side Window Hinge andLatch Inspection Task 56-11-00-213

241, 242

A720001 Engine Minor Inspection - Complete the scheduledmaintenance checks. Refer to the Model PW545Aor PW545B Pratt & Whitney Canada MaintenanceManual, Chapter 5, Section 05-20-00, ScheduledMaintenance Checks. Task 71-90-00-610

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 60

Date: _______________



Total Time: _______________

1. Description

A. Phase 60 consists of items to be inspected initially at 2400 hours and then every 1200 hours thereafter.






ITEM CODENUMBER


A271003 Aileron Fuselage and Inboard Wing Control Cables- Inspect. Task 27-10-00-210

141, 142,152, 161,162, 247,248

A272005 Rudder Control Cables - Inspect. Task 27-20-00-225 141, 151,161, 241,311, 321,322

A273008 Elevator Control Cables - Inspect. Task27-31-00-210

141, 142,151, 161,311, 321

A273010 Elevator Trim Tab Control Cables - Examine. Task27-31-00-222

141, 142,153, 163,165, 321



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 63

Date: _______________



Total Time: _______________

1. Description

A. Phase 63 consists of items to be inspected every 12 calendar months as required by 14 CFR 91.207.(No grace period.)






ITEM CODENUMBER


B256001 ELT 110-4 Emergency Locator Beacon System -Visually examine and complete an operational test.Test required by Title 14 of the Code of FederalRegulations 91.207. Task 25-61-03-710

BAT

A256004 Artex C406-2 Emergency Locator Transmitter -Complete a visual examination. Required by Title14 of the Code of Federal Regulations 91.207. Task25-61-04-210

BAT

B256004 Artex C406-2 Emergency Locator Transmitter -Complete an operational test. Required by Title 14of the Code of Federal Regulations 91.207. Task25-61-04-720

BAT

A256005 Artex C406-N Emergency Locator Transmitter -Complete a visual examination. Required by Title14 of the Code of Federal Regulations 91.207. Task25-61-05-210

BAT

B256005 Artex C406-N Emergency Locator Transmitter -Complete an operational test. Required by Title 14of the Code of Federal Regulations 91.207. Task25-61-05-720

BAT


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A256106 Artex 110-406 Emergency Locator Inspection Task25-61-06-210

BAT

B256106 Artex 110-406 Emergency Locator Functional TestTask 25-61-06-720

BAT



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 66

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


D217002 Ozone Converters Restoration (Cleaning) Task12-19-02-161

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 67

Date: _______________



Total Time: _______________

1. Description

A. Phase 67 consists of items to be inspected every 400 hours or 12 calendar months whichever occursfirst.






ITEM CODENUMBER


B561001 Windshield Surface Seal Treatment FunctionalCheck Task 56-11-00-720

241, 242



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 68

Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B238001 Standby Nav/Com Control Unit Operational Check(Airplanes -5001 thru -6000) Task 23-80-01-710

AUX



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 69

Date: _______________



Total Time: _______________

1. Description

A. Phase 69 consists of inspection item(s), which are completed every 6 calendar months (for airplanesthat operate in moderate or severe corrosion environments. Refer to Chapter 51, Corrosion SeverityMaps - Description and Operation).






ITEM CODENUMBER



710, 720,730


710

A551006 Horizontal Stabilizer Aft Spar Area GeneralVisual Inspection (Corrosion Inspection) Task55-10-01-212

351, 352


340


512, 522,532, 612,622, 632


512, 612



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 70

Date: _______________



Total Time: _______________

1. Description

A. Phase 70 consists of items to be inspected every 500 compressor hours on the vapor cycle coolingsystem.






ITEM CODENUMBER


A215207 Vapor Cycle Cooling System 500 Compressor-HourMaintenance Task 21-52-00-211

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE 71

Date: _______________



Total Time: _______________

1. Description

A. Phase 71 consists of items to be inspected at the first 6000 hours and every 1200 hours thereafter.






ITEM CODENUMBER


A553020 Vertical Stabilizer Internal Inspection (NOTE:This inspection is for the horizontal pivot fittingassembly.) Task 55-30-01-212

340



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MB

Date: _______________



Total Time: _______________

1. Description

A. Phase MB consists of items to be inspected at the first 3000 hours, then every 1500 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A712200 Aft Engine Beam Inspection (Chapter 4 Item)NOTE: This engine support structure inspection isfor Airplanes -5001 thru -5060. Task 71-22-00-210

311, 312,411, 412

*** End of Phase MB Inspection Items ***

5-12-MB Page 1© TEXTRON AVIATION INC. Oct 1/2011

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MD

Date: _______________



Total Time: _______________

1. Description

A. Phase MD consists of items to be inspected at the first 6000 hours or ten years whichever occurs firstand every 2400 hours or ten years, whichever occurs first thereafter. This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A531020 Forward Pressure Bulkhead - Visually inspectforward side for cracks, failed fasteners, corrosionand evidence of structural damage. Include theweb and supporting structure on the forward sideand the periphery angles on the aft side (Chapter 4Item). Task 53-10-11-251

221, 222

*** End of Phase MD Inspection Items ***

5-12-MD Page 1© TEXTRON AVIATION INC. Apr 1/2013

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE ME

Date: _______________



Total Time: _______________

1. Description

A. Phase ME consists of items to be inspected every 15,000 hours. This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A521008 Cabin Door Detailed Inspection (Chapter 4 Item)Task 52-10-00-210

810

A522004 Emergency Exit Door Detailed Inspection (Chapter4 Item) Task 52-20-00-210

820

A531010 Aft Pressure Bulkhead - Visually inspect forwardside for cracks, failed fasteners, corrosion andevidence of structural damage (Chapter 4 Item).Task 53-10-11-252

311, 312

A533004 Upper Skin Splice at BL 0.00 (Chapter 4 Item) Task53-30-01-251

251, 252,261, 262

A533006 Lower Skin Splice at Stringer 13 (Chapter 4 Item)Task 53-30-01-252

141, 142,151, 152,161, 162

A533008 Lower Skin from Right Stringer 13 to Left Stringer13 (Chapter 4 Item) Task 53-30-01-210

141, 142,151, 152,161, 162,321, 322

*** End of Phase ME Inspection Items ***

5-12-ME Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MF

Date: _______________



Total Time: _______________

1. Description

A. Phase MF consists of items to be inspected at the first 7500 hours, then every 1400 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571000 Lower Wing Main Spar Lower Skin Splice at WS22.50 (Chapter 4 item) Task 57-10-00-250

511, 512,611, 612

A571002 Lower Wing Main Spar Lower Skin Splice at WS22.50 (Chapter 4 item) Task 57-10-00-270

511, 512,611, 612

*** End of Phase MF Inspection Items ***

5-12-MF Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MG

Date: _______________



Total Time: _______________

1. Description

A. Phase MG consists of items to be inspected at the first 6500 hours, then every 3000 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553005 Vertical Stabilizer Rear Spar Cap at WL 146.00(Airplanes -5001 thru -5020) (Chapter 4 item) Task55-30-01-250

340

*** End of Phase MG Inspection Items ***

5-12-MG Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MH

Date: _______________



Total Time: _______________

1. Description

A. Phase MH consists of items to be inspected at the first 11,000 hours, then every 6000 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553006 Vertical Stabilizer Rear Spar Nested Angle at WL146.00 (Airplanes -5001 thru -5020) (Chapter 4item) Task 55-30-01-251

340

*** End of Phase MH Inspection Items ***

5-12-MH Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MI

Date: _______________



Total Time: _______________

1. Description

A. Phase MI consists of items to be inspected at the first 5000 hours, then every 2500 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553007 Vertical Stabilizer Rear Spar Strap at WL 146.00(Airplanes -5001 thru -5020) (Chapter 4 item) Task55-30-01-252

340

*** End of Phase MI Inspection Items ***

5-12-MI Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MJ

Date: _______________



Total Time: _______________

1. Description

A. Phase MJ consists of items to be inspected every 13,000 hours. This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A533010 Upper Skin from Right Stringer 13 to Left Stringer13 (Chapter 4 Item) Task 53-30-01-210

241, 242,251, 252,261, 262,311, 312,321, 322

A545000 Forward Engine Beam, Upper Angles, HorizontalCap Flange at BL 30.5 to BL 42.0 (Chapter 4 Item)Task 54-50-10-250

311, 312,411, 412

*** End of Phase MJ Inspection Items ***

5-12-MJ Page 1© TEXTRON AVIATION INC. Oct 1/2011

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MK

Date: _______________



Total Time: _______________

1. Description

A. Phase MK consists of items to be inspected at the first 11,500 hours, then every 9000 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553011 Vertical Stabilizer Forward Spar Strap at WL 150.00(Airplanes -5001 thru -5020) (Chapter 4 Item) Task55-30-01-253

321, 322

*** End of Phase MK Inspection Items ***

5-12-MK Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE ML

Date:_______________



Total Time: _______________

1. Description

A. Phase ML consists of items to be inspected at the first 11,500 hours, then every 3300 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571004 Lower Wing Main Spar Skin Splice Flange at WS11.50 (Chapter 4 item) Task 57-10-00-251

511, 512,611, 612

A571006 Lower Wing Main Spar and Skin Splice at WS 11.50(Chapter 4 item) Task 57-10-00-271

511, 512,611, 612

*** End of Phase ML Inspection Items ***

5-12-ML Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MM

Date:_______________



Total Time: _______________

1. Description

A. Phase MM consists of items to be inspected at the first 11,000 hours, then every 4200 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571008 Lower Wing Main Spar at WS 114.57 (Chapter 4item) Task 57-10-00-252

521, 522,621, 622

*** End of Phase MM Inspection Items ***

5-12-MM Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MN

Date:_______________



Total Time: _______________

1. Description

A. Phase MN consists of items to be inspected at the first 9000 hours, then every 3400 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER



521, 522,621, 622

*** End of Phase MN Inspection Items ***

5-12-MN Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MO

Date:_______________



Total Time: _______________

1. Description

A. Phase MO consists of items to be inspected at the first 12,500 hours, then every 6100 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER



521, 522,621, 622

*** End of Phase MO Inspection Items ***

5-12-MO Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MP

Date: _______________



Total Time: _______________

1. Description

A. Phase MP consists of items to be inspected every 300 hours. This inspection is a Chapter 4requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A215201 Vapor Cycle Cooling System Hour Meter CheckTask 21-52-00-210

332

*** End of Phase MP Inspection Items ***

5-12-MP Page 1© TEXTRON AVIATION INC. Jul 1/2012

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION PHASE MQ

Date: _______________



Total Time: _______________

1. Description

A. Phase MQ consists of items to be inspected at the first 10,000 hours and every 5000 hours thereafter.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553013 Vertical Stabilizer Forward Spar Strap at WL188.00 (Airplanes -5001 thru -5020) (Chapter 4requirement) Task 55-30-01-254

340

*** End of Phase MQ Inspection Items ***

5-12-MQ Page 1© TEXTRON AVIATION INC. Apr 1/2013

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

DISCRETIONARY MAINTENANCE

1. Scope

A. This section provides reference to discretionary maintenance tasks that may be applicable and/oreffective for individual operators.

NOTE: During the MSG-3 Maintenance Review Board Process, not all tasks recommended inSupplier reference documents are determined applicable and/or effective for all operators.As a result, some tasks given in the Supplier Information reference documents are notincluded in the Cescom/Camp Systems scheduled maintenance set-up. However, if anoperator desires discretionary maintenance tracking for any inspection task listed in Table1, or associated Supplier Information documents, contact Cescom/Camp Systems atwww.campsystems.com, to have your reports customized.

5-19-00 Page 1© TEXTRON AVIATION INC. Oct 1/2017

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Discretionary Maintenance

DISCRETIONARY MAINTENANCE

Maintenance Manual TaskNumber

Discretionary Maintenance Reference

15 Day High Exposure Areas -Airplane Zone 1 Wash

(NOTE 1)

(NOTE 2)

(NOTE 3)

12-26-00-6001

(NOTE 4)

45 Day Medium Exposure Areas -Airplane Zone 2 Wash

(NOTE 1)

(NOTE 2)

(NOTE 3)

12-26-00-6002

(NOTE 4)

90 Day Low Exposure Areas -Airplane Zone 3 Wash

(NOTE 1)

(NOTE 2)

(NOTE 3)

12-26-00-6003

(NOTE 4)

Cessna Standard PracticesManual, Chapter 20, ExteriorCleaning/Washing/Rinse -ServicingCessna Standard PracticesManual Chapter 51, Corrosion -Description and OperationCessna Standard PracticesManual, Chapter 51, CorrosionSeverity Maps - Description andOperation

NOTE 1: Aircraft washing is a key component of any CPCP. Washing removes corrosive agents from the surfaceof the airplane.

NOTE 2: These wash intervals are a baseline aircraft wash schedule. If an aircraft flies into any SevereCorrosion Areas during its operation route, it may be necessary to increase the frequency of thewash schedule.

NOTE 3: Cessna strongly recommends washing or rinsing the airplane as soon as possible, no later than threedays, after any operation that exposes the airplane to Runway De-Icing (RDI) fluids. Any delay canresult in the greater likelihood of corrosion.

NOTE 4: Operators can refer to the Exterior Cleaning procedures in the Cessna Standard Practices Manual,Chapter 20, Exterior Cleaning/Washing/Rinse - Servicing. Description and Operation of Corrosioncan also be found in the Cessna Standard Practices Manual Chapter 51, Corrosion - Description andOperation. Corrosion Severity Maps can be found in the Cessna Standard Practices Manual, Chapter51, Corrosion Severity Maps - Description and Operation.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

UNSCHEDULED MAINTENANCE CHECKS

1. General

NOTE: This section applies to the MSG-3 inspection program as well as the Non-MSG-3 InspectionProgram.

A. During operation, the airplane can have forces put on it that make it necessary to completeunscheduled maintenance.(1) Hard/overweight landings.(2) Overspeed (Above 8000 ft) - A condition in which the airplane is operated at airspeeds that are

more than those permitted by the Approved Airplane Flight Manual at altitudes that are morethan 8000 feet.

(3) Overspeed (Below 8000 ft) - A condition in which the airplane is operated at airspeeds that aremore than those permitted by the Approved Airplane Flight Manual at altitudes that are less than8000 feet. Overspeed conditions at this altitude also increase the chance for birdstrike damageto the airplane.

(4) Flap System Overspeed - A condition in which the flaps are extended at airspeeds that are morethan those permitted by the Approved Airplane Flight Manual.

(5) Landing Gear Assembly Overspeed - A condition in which the landing gear is extended atairspeeds that are more than those permitted by the Approved Airplane Flight Manual.

(6) Dangerous air turbulence or dangerous maneuvers.(7) Accidental in-flight thrust reverser deployment.(8) Lightning strike.(9) Foreign object damage.(10) Airplane towed with a large fuel unbalance or high drag/side loads because of ground handling.(11) Airplane operation through deep standing water.(12) Nose landing gear tow limits.

B. When any of these conditions is supplied in a report by the flight crew, complete a visual inspectionof the airframe and specific inspections of components and areas where an effect is possible.

C. The inspections are completed to find and make an analysis of the depth of damage in local areaswhere damage can be seen, and to the structure and components adjacent to the area of damage.

D. When there is a lightning strike, a full inspection of the airplane exterior is completed to find possibledamage.

E. If it is thought that foreign object damage occurred, do a visual inspection of the airplane before theairplane is returned to service.

F. If there has been fluid spilled in the interior cabin or tailcone, complete the Interior Cabin/TailconeFluid Spill procedures below.

G. If the airplane has been exposed to high-wind conditions while parked, complete the Exposure to HighWinds While the Aircraft is Parked Check, below.

2. Unscheduled Maintenance Checks Defined

A. Hard/Overweight Landings.(1) A hard landing is a landing that is made by an airplane with a sink rate that is more than the

permitted sink rate.(2) Related to a hard landing is an overweight landing, which is landing the airplane at any gross

weight which is more than the placard landing weights.

NOTE: If the hard/overweight landing is mixed with high drag/side loads, additional checks arerequired.

B. Overspeed.(1) Any time an airplane has done one or both of the conditions that follow:

(a) Airplane overspeed that is more than the placard speed limits of the flaps and/or landinggear.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(b) Airplane overspeed that is more than the design speeds.

C. Dangerous Air Turbulence or Dangerous Maneuvers.(1) Conditions that can dangerously shake an airplane. Dangerous maneuvers are any maneuvers

that are more than those permitted by the Approved Airplane Flight Manual.

D. Lightning Strike.(1) If flown through an electrically charged area of the atmosphere, where electrical release is

transferred from cloud-to-cloud and from cloud-to-earth, the airplane can become a part of thisflow. During a lightning strike, the current goes in the airplane at one point and goes out atanother, usually at opposite sides of the airplane. It is in these areas, wing tips, and nose andtail sections, where damage is most possible to occur. Burns and/or erosion of small surfaceareas of the skin and structure can be found during an inspection. Usually the damage is easilyseen, but damage that is hard to see, can occur. The function of the lightning strike inspectionis to find any damage that can occur to the airplane, before it is returned to service.

E. Foreign Object Damage.(1) Damage to the airplane engine can be caused by the ingestion of slush, a bird strike, or by any

other foreign object, while the airplane is operated on the ground or in normal flight. Damagecan also be caused by tools, bolts, nuts, washers, rivets, rags, or pieces of safety wire left inthe engine inlet duct during maintenance operations. Dents, nicks or scratches in the engineinlet are to be thought of as an indication of foreign object ingestion. The function of the foreignobject damage inspection is to find any damage before to the airplane is repaired or returned toservice.

(2) Safety precautions must be done to prevent the touch of foreign objects to the airplane duringtowing, and at all times when airplane is not in service. To prevent corrosion in the compressorstages and damage to the fan disc and blades, the engine inlet and tailpipe must have the correctcovers. When the wind will turn the engines, the covers must be installed as soon as possibleafter engine shutdown.

(3) The level of aerodynamic smoothness (how smooth the surface), with specific focus on theengine inlet cowling area, helps the performance function of the airplane. It is most importantthat a very clean level be kept.

(4) Contour and distortion of the aerodynamic surface can occur during normal operation or byincorrect movement during maintenance operations. Surfaces that are very curved, such asthe engine inlet lip and inlet ducting, are areas where distortions can have a large effect on theairplane performance. Doors and access panels can easily get distortion by incorrect movement.Be careful when you touch these items.

F. Airplane Towed with a Large Fuel Unbalance or High Drag/Side Loads Because of Ground Handling.(1) A fuel unbalance condition is when one wing has a larger quantity of fuel than the other. This can

be because of a fuel system incorrect operation, incorrect refuel procedure, etc. It is best notto move an airplane in this condition. If it must be done, be careful and complete an inspectionbefore the airplane is returned to service.

(2) High drag/side load condition is when the airplane skids or leaves the prepared surface into anunprepared surface, or lands before the prepared surface, or lands and has a blown tire(s) orgoes into a skid on a runway where the safety of the airplane is not sure. This is for takeoffs,landings, or unusual taxi conditions.

G. Turns Past the Nose Landing Gear Limits When Towed.(1) Turns that are more than the limits of the nose landing gear when the airplane is towed with

either a towbarless vehicle or towbar can cause damage to the nose landing gear. The turnlimits for the tow method that follow are:

NOTE: The nose wheel can be turned more than the black limit marks when the torquelinks are disconnected and kept apart from each other and the tire. This will preventdamage to the nose gear centering mechanism or steering stops.

(a) When the airplane is towed with the control lock disengaged, the turn limit is 90 degrees.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(b) When the airplane is towed with the control lock engaged, the turn limit is 60 degrees.

NOTE: Cessna Aircraft Company does not recommend that the airplane be towedwith the Lektro tow vehicle when the torque links are engaged.

3. Hard or Overweight Landing Check

A. Landing Gear (Chapter 32).(1) The main landing gear upper barrel-to-trunnion attachment (bolts and braze) - Examine for

correct installation and indications of structural damage.(2) Main landing gear actuator attachments and support structure - Examine for correct installation,

loose or unserviceable fasteners, and indications of structural damage.(3) Nose landing gear trunnion at supports and attach structure - Examine for correct installation,

unserviceable fasteners, and any indications of structural damage.(4) Nose landing gear actuator attachments and support structure - Examine for correct installation,

unserviceable fasteners, and any indications of structural damage.

B. Wings (Chapter 57).(1) Lower wing surface in the main landing gear area - Examine for skin buckles, unserviceable

fasteners, correct installation of landing gear rib and trunnion fittings, rear spar web, and fuelleaks.

(2) Wing-to-stub wing fittings - Examine for correct installation and any indications of structuredamage.

(3) Trailing edge assembly - Examine for any deformation that has an effect on normal flap operation.(4) Leading edge - Examine the skin attach rivets along the leading edge of the wing inboard of the

landing gear for loose rivets.

4. Overspeed Check (Above 8000 ft)

A. Landing Gear (Chapter 32).(1) Trunnion and supports - Examine for cracks, correct installation, and indications of structural

damage.(2) Doors and Attachments - Examine for unserviceable fasteners, cracks, buckles, and indications

of structural damage.(3) Examine to make sure components are free to move and do an operational check.

B. Fuselage (Chapter 53).(1) Nose section - Examine for buckles, dents, unserviceable fasteners and any indications of

structural damage.(2) All hinged access doors - Examine the hinges, hinge attach points, latches and attachments and

skins for deformation and indications of structural damage.

C. Nacelles and Pylons (Chapter 54).(1) Skins - Examine for buckles, cracks unserviceable fasteners, and indications of structural

damage.(2) Fillets and fairings - Examine for buckles, dents cracks, and loose or unserviceable fasteners.

D. Stabilizers (Chapter 55).(1) Stabilizers - Examine the skins, hinges, and attachments, surfaces that can move, mass balance

weights and attach structure for cracks, dents, buckles, unserviceable fasteners and indicationsof structural damage.

E. Wings (Chapter 57).(1) Flaps - Examine for skin buckles, cracks, unserviceable fasteners, attachments, and structure

for damage.(2) Complete a check of the flaps for freedom of movement operation.

5. Overspeed Check (Below 8000 ft)

A. Landing gear (Chapter 32).(1) Doors - Examine for dents, tears, punctures, blood, feathers or other indications of structural

damage.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

B. Fuselage (Chapter 53).(1) Radome - Examine for dents, tears, punctures, blood, feathers or other indications of structural

damage.(2) Skins - Examine the forward areas (including belly and upper skins) for dents, tears, punctures,

blood, feathers or other indications of structural damage.

C. Nacelles/Pylons (Chapter 54).(1) Skins - Examine for dents, tears, punctures, blood, feathers or other indications of structural

damage.

D. Stabilizers (Chapter 55).(1) Leading edge skins - Examine for dents, tears, punctures, blood, feathers or other indications

of structural damage.

E. Windows (Chapter 56).(1) Windshields - Examine for scratches, blood, feathers or other indications of structural damage.

F. Wings (Chapter 57).(1) Leading edge skins - Examine for dents, tears, punctures, blood, feathers or other indications

of structural damage.

G. Power Plant (Chapter 71).(1) Cowling - Examine for dents, tears, punctures, blood, feathers or other indications of structural

damage.(2) Air Inlet Sections - Examine for dents, tears, punctures, blood, feathers or other indications of

structural damage.(3) Examine the engine in accordance with the applicable Pratt & Whitney Turbofan Engine

Maintenance Manual. Refer to the Introduction, Supplier Publication List.

6. Flap System Overspeed Checks

A. Flaps with the landing gear in the UP position. (Chapter 27)(1) Examine for skin buckles, cracks, unserviceable fasteners, attachments and structure for

damage.(2) Complete a check of the flaps for freedom of movement and operation.

7. Landing Gear Assembly Overspeed Checks

A. Landing Gear with the flaps in the UP position. (Chapter 32)(1) Trunnion and supports - Examine for cracks, correct installation, and indications of structural

damage.(2) Doors and Attachments - Examine for unserviceable fasteners, cracks, buckles, and indications

of structural damage.(3) Make sure that the doors are aligned correctly.(4) Complete a check of the landing gear for freedom of movement and operation.

8. Severe Turbulence and/or Maneuver Checks

A. Fuselage (Chapter 53).(1) Forward and Center Fuselage - Do an inspection of the airplane skin surface for buckles, wrinkles

and deformations. Do a check for unserviceable or missing fasteners. Do an inspection of theareas around the wing attachments, the cabin door, and the emergency exit door for structuraldamage.

(2) Tailcone - Do an inspection of the airplane skin surface for buckles, wrinkles, and deformations.Check for unserviceable or missing fasteners. Do an inspection of the areas around the baggagedoor and the engine beams for structural damage.

B. Stabilizer (Chapter 55).(1) Horizontal tail hinge fittings, actuator fittings, and stabilizer center section - Examine for correct

installation, unserviceable fasteners, and any indications of structural damage.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Vertical tail - Examine for indications of structural damage, skin buckles, and correct installationat the primary attachments in the tailcone, unserviceable fasteners and damage to hinges andactuator fittings.

(3) Elevator and rudder balance weight support structure - Examine for correct installation,unserviceable fasteners, and indications of structural damage.

C. Wing (Chapter 57).(1) Wing to body fittings and support structure - Examine for correct installation, unserviceable

fasteners and indications of structural damage.(2) Trailing Edge - Examine for any deformation that will effect normal operation of flap and aileron.(3) Leading Edge - Examine the skin attach rivets along the leading edge of the wing inboard of the

landing gear for loose rivets.

9. Inadvertent In-Flight Thrust Reverser Deployment

A. Fuselage (Chapter 53).(1) Examine the tailcone skins, stringers, and frames aft of the aft pressure bulkhead for wrinkles,

cracks, unserviceable or loose fasteners or bonds, or other damage. Examine the strakes andtheir installation for damage.

B. Nacelles (Chapter 54).(1) Examine the nacelles, pylons, engine beams and related attach fittings, and thrust reversers for

buckles, cracks, unserviceable fasteners, and indications of structural damage.

C. Stabilizer (Chapter 55).(1) Horizontal stabilizer and elevator hinges and hinge fittings, actuator hinge fittings connections,

and idlers - Examine for correct installation, unserviceable fasteners, and any indications ofstructural damage. Examine the forward spar area of the stabilizer at the stabilizer actuatorattachment and the stabilizer aft spar at the pivot for damage and unserviceable fasteners.

(2) Vertical stabilizer and rudder - Examine the stabilizer for indications of structural damage, skinbuckles, and correct installation at the primary attachments in the tailcone. Complete a checkfor cracks or unserviceable fasteners at the attach points. On the rudder, complete a check fordamage to the hinges, hinge fittings, actuators, and actuator fittings.

10. Lightning Strike Check

A. As the checks are done that follow, complete the Lightning Strike/Static Discharge Incident ReportingForm. Mail the completed form to Cessna Citation Customer Service, P.O. Box 7706, Wichita, KS67277 Attn: Citation Hot Line.

B. Communications (Chapter 23).(1) Antennas - Examine all of the antennas for indications of burns or erosion. If damage is found,

complete a functional check of the applicable system.

C. Navigation (Chapter 34).(1) Radar reflector, feed horn, motor box assembly, and mount structure - Examine for damage. If

damage is found, complete a bench check of the system. If pits or burns in the surface of themount structure only are found, complete a functional check of the radar system.

(2) Glideslope antenna - Examine for burns and pits. If damage is found, complete a functionalcheck of the glideslope system.

(3) Standby compass - The standby compass shall be thought of as serviceable if the correctedheading is within +10 or -10 degrees of the heading indication given by the remote compasssystem. If the standby compass is not within tolerance, remove, repair or replace, as necessary.

D. Fuselage (Chapter 53).(1) Radome - Examine for indications of burns or erosion.(2) Skin - Examine the surface of the fuselage skin for indications of damage.(3) Stinger - Examine the static discharge wicks for damage.

E. Stabilizers (Chapter 55).(1) Rudder - Examine the static discharge wicks for damage.(2) Elevator - Examine the static discharge wicks for damage.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

F. Wings (Chapter 57).(1) Skins - Examine for indications of burns and erosion.(2) Wing Tips - Examine for indications of burns and pits. Examine the static discharge wicks for

damage.(3) Flaps, ailerons, and speed brakes - Examine for burns and pits. Examine the static discharge

wicks for damage.

G. Engine (Chapter 72).(1) Engine - Refer to the engine maintenance manual for lightning strike inspection.

11. Foreign Object Damage Check

A. Landing Gear (Chapter 32).(1) Doors - Examine for dents, cracks, and indication of structural damage. Also, make sure the

door is not incorrectly aligned.

B. Fuselage (Chapter 53).(1) Radome - Examine for dents, cracks, punctures, scratches, etc.(2) Skin - Examine the forward and belly areas for dents, punctures, cracks, and any indications of

damage.

C. Nacelles/Pylons (Chapter 54).(1) Skins - Examine for dents, punctures, unserviceable fasteners, cracks, and indications of

structural damage.

D. Stabilizers (Chapter 55).(1) Leading edge skins - Examine for dents, cracks, scratches, and any indications of structural

damage.

E. Windows (Chapter 56).(1) Windshield - Examine for chips, scratches, and cracks.

F. Wings (Chapter 57).(1) Leading edge skins - Examine for dents, cracks, punctures, and indications of possible structural

damage.

G. Power Plant (Chapter 71).(1) Cowling - Examine for dents, cuts, tears, scratches, blood, and feathers.(2) Air inlet section - Examine for dents, cracks, scratches, punctures, blood, and feathers.(3) Fan - Examine for bent, broken, or cracked blades. Make sure the blades do not have nicks or

rubs.(4) Refer to the engine manufacturer’s maintenance manual for additional inspection procedures

that are necessary after a bird strike or ingestion.

12. Towing with Large Fuel Unbalance or High Drag/Side Loads Due to Ground Handling Check

A. Landing Gear (Chapter 32).(1) Main landing gear and doors - Examine for unserviceable fasteners, buckles, correct installation,

cracks, and indications of structural damage.(2) Nose landing gear and doors - Examine for unserviceable fasteners, cracks, correct installation,

buckles, and indications of structural damage.

13. Airplane Operation Through Deep Standing Water

A. Visually examine the elevator trim tabs for delamination or peeling along the trailing edge.

14. Nose Landing Gear Tow Limits Check

A. Complete the checks that follow, if the airplane's nose landing gear is turned past the limit with thecontrol lock disengaged.(1) Nose wheel steering gear attach bolts on top of the upper barrel - Examine for correct installation,

loose or unserviceable fasteners, or indications of damage.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Nose wheel steering gear stops on top of the trunnion - Examine for correct installation, looseor unserviceable fasteners, or indication of damage to the structure.

(3) Steering bungee, bell crank, steering cable brackets and steering cables - Examine for correctinstallation, loose or unserviceable fasteners, or indication of damage to the structure.

B. Complete the checks that follow, if the airplane is turned past the limit with the control lock engaged.(1) Nose wheel steering gear attach bolts on top of the upper barrel - Examine for correct installation,

loose or unserviceable fasteners, or indications of damage.(2) Nose wheel steering gear stops on top of the trunnion - Examine for correct installation, loose

or unserviceable fasteners, or indication of damage to the structure.(3) Steering bungee, bell crank, steering cable brackets and steering cables - Examine for correct

installation, loose or unserviceable fasteners, or indication of damage to the structure.(4) Rudder cables and cable brackets, rudder pass-thru sector, and rudder control lock system -

Examine for correct installation, loose or unserviceable fasteners, or indication of damage to thestructure.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

15. Exposure to High Winds While the Aircraft is Parked Check

A. If the airplane has been exposed to high-wind conditions while parked, complete the checks thatfollow:(1) Examine the landing gear doors for condition or damage from foreign object debris.(2) Examine all transparent surfaces for condition and cleanliness, including cockpit windows/

windshields, passenger windows and external lights.(3) Examine all static ports and pitot tubes for damage or debris.(4) Examine the AOA Stator Vane for condition and deformation.(5) Examine the stabilizers for condition, deformation or other damage.(6) Examine the fuselage and wings for condition, deformation or other damage.(7) Examine the engines (turbine blades, exhaust nozzle, fixed blades of turbine outset) for absence

of foreign matter and condition.(8) Examine all flight control surfaces (pitch, yaw and roll) for condition, deformation or other

damage.

16. Interior Cabin/Tailcone Fluid Spill

A. Fluid spills should be cleaned up as soon as practical.

B. Clean all contaminated areas. Refer to Chapter 20, Interior Finish - Cleaning/Painting.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

MSG-3 INSPECTIONS

1. General

A. General inspection criteria.(1) When each of the specified inspections in this chapter are done and while access is available,

you must do a general visual inspection of the adjacent areas. These general visual inspectionsare done to find conditions where more maintenance is necessary.

(2) When you have access to an area, you must examine the wire bundles for damage and correctinstallation. Make sure that the wire bundles are not attached to hydraulic tubes or lines.

(3) The inspection items given are for specified components and systems. It is necessary that themaintenance technicians fully examine all of the components and systems to make sure thatthey are safe and operate correctly.

(4) If a component or system is moved or changed (because of maintenance done) after anoperational or functional test is completed, then it is necessary to do the test again before thesystem or component is returned to service. Refer to the applicable chapter in this MaintenanceManual for removal/installation, and operational or functional tests of components and/orsystems.

(5) For the lubrication of items or components, refer to Chapter 12, Replenishing - Description andOperation for the correct lubricant and the points to lubricate.

(6) Refer to Chapter 6, Airplane Zoning - Description and Operation for the airplane zones.(7) Do a preflight inspection after the applicable inspection is done to make sure that the servicing

is done correctly. Refer to the Approved Airplane Flight Manual.(8) To help you keep records, intervals that start with the letter M are used for the necessary

inspection items in Chapter 4, Airworthiness Limitations. The interval for each of these items isspecified by Chapter 4 and must be done at or before the recorded interval. You cannot extendChapter 4 inspection items more than the given interval.

2. Inspection and Document Cross-Reference for Inspection Time Limits:

NOTE: A calendar month starts on the first day of the month. All inspections for that interval becomedue by the last day of that month.

NOTE: The manufacturer supplies the inspections necessary for the engine, APU, vapor cycle coolingsystem, wheels, and brakes. To make sure that you do the correct inspections necessary,as given by the manufacturer, refer to the inspections at the intervals in the manufacturer'smanuals that follow.

A. The Citation Model 560XL (CE-560XL) powerplant (PW545A, PW545B, and PW545C) maintenanceis defined by the Pratt & Whitney Engine Maintenance Manuals (PW545A part number 30J1272,PW545B part number 30J2242, and PW545C part number 30J2302). The Engine MaintenanceManual is necessary to maintain the continued airworthiness of the Citation Model 560XL(CE-560XL) propulsion engines. The Engine Maintenance Manual includes details on all themaintenance/inspection requirements for the engine and its sub-systems as delivered with theengine. The Pratt & Whitney Engine Maintenance Manual is the FAA accepted document for detailedmaintenance instructions per Type Certificate Data Sheet E00059EN. The Engine MaintenanceManual including Chapter 5 of the Engine Maintenance Manual is not part of the MaintenanceReview Board (MRB) or subject to approval by the MRB.(1) The Citation Model 560XL (CE-560XL) engine program is intended as a stand-alone engine

program with on-wing engine maintenance/inspection intervals defined by the MaintenanceReview Board Report (MRBR). The operator should use the Pratt & Whitney EngineMaintenance Manual for detailed shop visit information.

B. The Citation Model 560XL (CE-560XL) auxiliary power unit (APU) (RE100XL) maintenanceintervals are contained in the Model 560XL Maintenance Review Board Report. The CitationModel 560XL (CE-560XL) auxiliary power unit (APU) (RE100XL) maintenance procedures aredefined by the Honeywell/AlliedSignal RE100(XL) Maintenance Manual (part number 49-25-85).The Honeywell/AlliedSignal RE100(XL) Maintenance Manual is necessary to maintain thecontinued airworthiness of the Citation Model 560XL (CE-560XL) APU. The Honeywell/AlliedSignalRE100(XL) Maintenance Manual includes details on all the maintenance/inspection requirements


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

for the APU. The Honeywell/AlliedSignal RE100(XL) Maintenance Manual is the FAA accepteddocument for detailed maintenance instructions per Type Certificate Data Sheet E00059EN. TheHoneywell/AlliedSignal RE100(XL) Maintenance Manual is part of the Maintenance Review Board(MRB) and is subject to approval by the MRB.(1) The operator should use the Honeywell/AlliedSignal RE100(XL) Maintenance Manual for

detailed shop visit information.

C. The Citation Model 560XL (CE-560XL) vapor cycle cooling system maintenance is defined by theEnviro Systems, Inc. General Operating, Servicing, and Maintenance Manual for Airborne R-134AAir Conditioning System (part number MAN-R-134A). The Enviro Systems, Inc. General Operating,Servicing, and Maintenance Manual for Airborne R-134A Air Conditioning System is necessaryto maintain the continued airworthiness of the Citation Model 560XL (CE-560XL) vapor cyclecooling system. The Enviro Systems, Inc. General Operating, Servicing, and Maintenance Manualfor Airborne R-134A Air Conditioning System includes details on all the maintenance/inspectionrequirements for the vapor cycle cooling system. The Enviro Systems, Inc. General Operating,Servicing, and Maintenance Manual for Airborne R-134A Air Conditioning System is the FAAaccepted document for detailed maintenance instructions per Type Certificate Data Sheet E00059EN.The Enviro Systems, Inc. General Operating, Servicing, and Maintenance Manual for AirborneR-134A Air Conditioning System is not part of the Maintenance Review Board (MRB) or subject toapproval by the MRB.(1) The operator should use the Enviro Systems, Inc. General Operating, Servicing, and

Maintenance Manual for Airborne R-134A Air Conditioning System for detailed shop visitinformation.

D. The Citation Model 560XL (CE-560XL) wheels maintenance is defined by the Goodrich ComponentMaintenance Manual with Illustrated Parts List - Main Wheel Assembly (part number 32-45-48).The Goodrich Component Maintenance Manual with Illustrated Parts List - Main Wheel Assemblyis necessary to maintain the continued airworthiness of the Citation Model 560XL (CE-560XL)wheels. The Goodrich Component Maintenance Manual with Illustrated Parts List - Main WheelAssembly includes details on all the maintenance/inspection requirements for the wheels. TheGoodrich Component Maintenance Manual with Illustrated Parts List - Main Wheel Assembly isthe FAA accepted document for detailed maintenance instructions per Type Certificate Data SheetE00059EN. The Goodrich Component Maintenance Manual with Illustrated Parts List - Main WheelAssembly is not part of the Maintenance Review Board (MRB) or subject to approval by the MRB.(1) The operator should use the Goodrich Component Maintenance Manual with Illustrated Parts

List - Main Wheel Assembly for detailed shop visit information.

E. The Citation Model 560XL (CE-560XL) brakes maintenance is defined by the Goodrich ComponentMaintenance Manual with Illustrated Parts List Cessna 560XL Main Landing Gear Brake Assembly(part number 32-46-49). The Goodrich Component Maintenance Manual with Illustrated PartsList Cessna 560XL Main Landing Gear Brake Assembly is necessary to maintain the continuedairworthiness of the Citation Model 560XL (CE-560XL) brakes. The Goodrich ComponentMaintenance Manual with Illustrated Parts List Cessna 560XL Main Landing Gear Brake Assemblyincludes details on all the maintenance/inspection requirements for the brakes. The GoodrichComponent Maintenance Manual with Illustrated Parts List Cessna 560XL Main Landing Gear BrakeAssembly is the FAA accepted document for detailed maintenance instructions per Type CertificateData Sheet E00059EN. The Goodrich Component Maintenance Manual with Illustrated Parts ListCessna 560XL Main Landing Gear Brake Assembly is not part of the Maintenance Review Board(MRB) or subject to approval by the MRB.(1) The operator should use the Goodrich Component Maintenance Manual with Illustrated Parts

List Cessna 560XL Main Landing Gear Brake Assembly for detailed shop visit information.

F. Chapter 4 Inspections(1) All Chapter 4 inspection items that are also given in Chapter 5 are recorded as individual

inspections in Chapter 5. At the request of the FAA and Part 135 operators, Chapter 4 itemsare recorded again in sections 5-92-M*.

(2) The actual intervals for these inspection items are the same as those recorded in Chapter 4 atthe time of publication.

(3) Inspection items in the documents that start with the letter M have no grace period.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(4) Because the Chapter 4 inspection items have their own individual documents, operators andmaintenance technicians can complete and report these inspections individually without havingto complete them with other documents.

Inspection Interval InspectionDocument

MSG-3 interval 1A/1C item(s), which are completed every 600 hours or 12calendar months whichever occurs first.

- 5-92-01

MSG-3 interval 1C item(s), which are completed every 12 calendar months. - 5-92-02


- 5-92-03



- 5-92-05

MSG-3 interval 3A/3C item(s), which are completed every 1800 hours or 36calendar months, whichever occurs first.

- 5-92-06



- 5-92-08

MSG-3 interval 4A/4C, 2A/4C thereafter item(s), which are completed at thefirst 2400 hours or 48 calendar months whichever occurs first, then every 1200hours or 48 calendar months whichever occurs first thereafter.

- 5-92-09


MSG-3 interval 4C, 2C thereafter item(s), which are completed at the first 48calendar months, then every 24 calendar months thereafter.

- 5-92-11

MSG-3 interval 5A item(s), which are completed every 3000 hours. - 5-92-12




MSG-3 interval 400 hours/1C item(s), which are completed every 400 hours or1C (12 calendar months), whichever occurs first.

- 5-92-16

MSG-3 interval 500 APU hours/2C item(s), which are completed every 500APU hours or 24 calendar months whichever occurs first.

- 5-92-17

MSG-3 interval 1000 hours/2C item(s), which are completed every 1000 hoursor 24 calendar months whichever occurs first. Hours are based on APUoperating hours.

- 5-92-18


- 5-92-19

Item(s), which are recommended every 14 days for operators who routinelyoperate or base their airplane in areas subject to saltwater or other corrosioneffects. (Not Currently Used)

- 5-92-22

Inspection item(s), which are completed every 100 hours or 12 calendarmonths, whichever occurs first

- 5-92-23

Inspection item(s), which are completed every 150 hours. - 5-92-24


CESSNA®MODEL 560XL

MAINTENANCE MANUAL



Inspection item(s), which are completed every 500 APU hours. - 5-92-26


Inspection item(s), which are completed every 800 hours in accordancewith (IAW) the manufacturer's instructions. Hours are based on compressoroperating hours. (Not Currently Used)

- 5-92-28

Inspection item(s), which are completed every 1000 hours in accordance with(IAW) the manufacturer's instructions. (Not Currently Used)

- 5-92-29

Inspection item(s), which are completed every 1000 hours in accordance with(IAW) the manufacturer's instructions. Hours are based on APU operatinghours.

- 5-92-30

Inspection item(s), which are completed at the first 1200 hours or 24 calendarmonths whichever occurs first, then every 200 hours or 12 calendar monthswhichever occurs first thereafter in accordance with (IAW) the manufacturer'sinstructions. (Not Currently Used)

- 5-92-31


- 5-92-32


- 5-92-33

Inspection item(s), which are completed every 6 calendar months in accordancewith (IAW) the manufacturer's instructions.

- 5-92-34

Inspection item(s), which are completed every 12 calendar months inaccordance with (IAW) the manufacturer's instructions.

- 5-92-35

Inspection item(s), which are completed every 24 calendar months inaccordance with (IAW) the manufacturer's instructions.

- 5-92-36

Inspection item(s), which are completed every 3 years in accordance with(IAW) the manufacturer's instructions. (Not Currently Used)

- 5-92-37

Inspection item(s), which are completed every 5 years in accordance with(IAW) the manufacturer's instructions.

- 5-92-38


- 5-92-39

Inspection item(s), which are completed at the first 2400 hours or 72 calendarmonths whichever occurs first, then every 1200 hours or 36 calendar monthswhichever occurs first thereafter.

- 5-92-40

Inspection item(s), which are completed every 12 years in accordance with(IAW) the manufacturer's instructions.

- 5-92-41


- 5-92-42

Inspection item(s), which are completed in accordance with (IAW) themanufacturer's instructions.

- 5-92-43

Required 14 CFR 91.207 item(s), which are completed every 12 calendarmonths. (These items do not have a grace period.)

- 5-92-44


CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Required 14 CFR 91.411, 91.413 and RVSM certification item(s), which arecompleted every 24 calendar months. (These items do not have a graceperiod.)

- 5-92-45

Inspection item(s), which are completed at every removal/installation of thenose wheel. (Not Currently Used)

- 5-92-46

Inspection item(s), which are completed at the first 600 hours or 12 calendarmonths whichever occurs first, then every 200 hours or 3 calendar monthswhichever occurs first thereafter.

- 5-92-47


Inspection item(s), which are completed at the first 10 years, then every 5years thereafter. (Not Currently Used)

- 5-92-49

Inspection item(s), which are completed every 6 calendar months (for airplanesthat operate in moderate or severe corrosion environments. Refer to Chapter51, Corrosion Severity Maps - Description and Operation).

- 5-92-50

Inspection item(s), which are completed every 500 compressor hours on thevapor cycle cooling system.

- 5-92-51

Inspection item(s), which are completed at the first 6000 hours, then every1200 hours thereafter.

- 5-92-52

Inspection item(s), which are completed every 500 hours. This inspection isa Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded. (Not Currently Used)

- 5-92-MA

Inspection item(s), which are completed at the first 3000 hours, then every1500 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.

- 5-92-MB

Inspection item(s), which are completed at the first 180 hours, then every 180hours or 24 calendar months whichever occurs first thereafter. This inspectionis a Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded. (Not Currently Used)

- 5-92-MC

Inspection item(s), which are completed at the first 6000 hours or 10 yearswhichever occurs first, then every 2400 hours or 10 years whichever occursfirst thereafter. This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.

- 5-92-MD

Inspection items which are completed every 15,000 hours. This inspectionis a Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.

- 5-92-ME

Inspection items which are completed at the first 7500 hours, then every 1400hours thereafter. This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.

- 5-92-MF


- 5-92-MG

Inspection items which are completed at the first 11,000 hours, then every 6000hours thereafter. This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.

- 5-92-MH


CESSNA®MODEL 560XL

MAINTENANCE MANUAL



- 5-92-MI

Inspection items which are completed every 13,000 hours. This inspectionis a Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.

- 5-92-MJ


- 5-92-MK


- 5-92-ML


- 5-92-MM


- 5-92-MN


- 5-92-MO

Inspection items which are completed every 300 hours. This inspection isa Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.

- 5-92-MP

Inspection items which are completed every 170 hours. This inspection isa Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.

- 5-92-MQ

Inspection item(s), which are completed at the first 10,000 hours and every5000 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded

- 5-92-MR

3. Inspection Time Limitations

NOTE: Do not extend the interval for any inspection found in Chapter 5 that is also required byChapter 4.

A. You can extend all inspection intervals for maintenance scheduling purposes only as given below:(1) The extension of all MSG-3 intervals up to a maximum of one (1) calendar month, or 20 flight

hours is permitted from the inspection due point.(a) Inspections that use a calendar and flight hour intervals can extend the due point one (1)

calendar month, or 20 flight hours, whichever occurs first.(b) Inspection items that use calendar intervals only, can extend the due point one (1) calendar

month only.(c) Inspection items that use flight hour intervals only, can extend the due point 20 flight hours

only.(2) All inspection due times that remain can be extended for maintenance scheduling purposes only

up to a maximum of one (1) calendar month, or 20 flight hours beyond the due time. This doesnot apply to Chapter 4, Airworthiness Limitations Inspection Documents beginning with the letterM or N, and interval items required by 14 CFR 91.411, 14 CFR 91.413, or 14 CFR 91.207.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(3) An inspection that is a calendar month inspection is due at the end of the month that theinspection is due, and not the day of the month that the inspection was last completed.(a) Inspection items that use a calendar and flight hour intervals can extend the due point one

(1) calendar month, or 20 flight hours, whichever occurs first.(b) Inspection items that use calendar intervals only, can extend the due point one (1) calendar

month only.(c) Inspection items that use flight hour intervals only, can extend the due point 20 flight hours

only.

B. Do not add the part of the month or hours used in an allowable extension to the subsequent inspectiondue time.

C. Any inspection program based upon the intervals of the items in this chapter or more frequent intervalsis acceptable.

4. Task Identification

A. Inspection items include tasks that have more data than can be given in Inspection Time Limits. Tasksare identified with an ATA Chapter-Section-Subject-Function number. Each task has a unique number.The Chapter-Section-Subsection number shows the location of the procedure in the MaintenanceManual, while the last three digits are assigned to correspond to the tasks specific functions.

B. The example shows a sample task number. Starting with the word Task, the numbers that follow givethe chapter, section, and subsection (subject) where the inspection task text is found. The two-digitfunction number shows the general class of the task. Refer to function number identification in Table1. The last digit gives the sequence number. If the same chapter-section-subsection and functionnumber is used for a different task, the sequence number increments by one.

C. CD-ROM users can link from a highlighted task number to the task text. Task numbers are foundin the Inspection Time Limits table or at any place throughout this manual where a task number isreferenced.

D. The task functions that are used in this manual are given in Table 1.

NOTE: The third digit of the function number is assigned sequentially, starting with zero. This willmake sure that there is a unique nine-digit task number.

E. Supplemental Type Certificate (STC) Installations.(1) Inspection requirements for STC installations are not included in this manual. When an STC

installation is incorporated on the airplane, those parts of the airplane affected by the installationmust be examined in accordance with the inspection program and published by the owner ofthe STC. Since STC installations may change systems interface, operating characteristics andcomponent loads or stresses on adjacent structures, Cessna supplied inspection criteria are notvalid for these airplanes.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Function Number Identification

10 CLEANING

11 Chemical

12 Abrasive

13 Ultrasonic

14 Mechanical

15 Stripping

16 Miscellaneous Cleaning

17 Flushing

20 INSPECTION, CHECK

21 General Visual

22 Detailed Dimensional

23 Penetrant

24 Magnetic

25 Eddy Current

26 X-Ray

27 Ultrasonic

28 Specific, Special

29 Borescope

60 SERVICING, PRESERVING, LUBRICATION

61 Servicing

64 Lubricating

65 Fueling, Defueling

67 Disinfect, Sanitize

68 Drain Fluid

70 TESTING, CHECKING

71 Operational

72 Functional

73 System

74 Bite

75 Special

76 Electrical

78 Pressure

79 Leak

80 MISCELLANEOUS

81 Fault Isolation


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Function Number Identification (continued)

82 Adjusting, aligning, calibration, rigging

84 Restore

87 Bleeding

90 CHANGE, REMOVE, INSTALL

96 Replace

5. Definitions

A. Lubrication or Servicing Task(1) Any act of lubrication or servicing for the purpose of maintaining inherent design capabilities.

B. Visual Check(1) A visual check is an observation to determine that an item is fulfilling its intended purpose. The


C. General Visual (Surveillance) Inspection(1) A visual examination of an interior or exterior area, installation or assembly to detect obvious

damage, failure, or irregularity. This level of inspection is made under normally available lightingconditions such as daylight, hangar lighting, flashlight, or drop-light and may require removalor opening of access panels or doors. Stands, ladders, or platforms may be required to gainproximity to the area being checked.

D. Detailed Inspection(1) An intensive visual examination of a specific structural area, system, installation or assembly to

detect damage, failure, or irregularity. Available lighting is normally supplemented with a directsource of good lighting at an intensity deemed appropriate by the inspector. Inspection aidssuch as mirrors, magnifying lenses, etc. may be used. Surface cleaning and elaborate accessprocedures may be required.

E. Special Detailed Inspection(1) An intensive examination of a specific item(s), installation or assembly to detect damage,

failure, or irregularity. The examination is likely to make extensive use of specialized inspectiontechniques and/or equipment. Intricate cleaning and substantial access or disassemblyprocedure may be required.

F. Operational Check(1) An operational check is a task to determine that an item is fulfilling its intended purpose. The


G. Functional Check(1) A functional check is a quantitative check to determine if one or more functions of an item perform

within specified limits.

H. Restoration Task(1) That work necessary to return the item to a specific standard. Since restoration may vary from

cleaning or replacement of single parts up to a complete overhaul, the scope of each assignedrestoration task has to be specified.

I. Discard Task(1) The removal from service of an item at a specified life limit. Discard tasks are normally applied

to so-called single parts such as cartridges, canisters, cylinders, engine disks, and safe-lifestructural members.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

MSG-3 INSPECTION TIME LIMITS

1. Inspection Items

REVISIONSTATUS

ITEM CODENUMBER


D121400 Shimmy Damper Servicing Task12-90-20-610

1A/1C 05-92-01 710

C122100 Flap System Lubrication Task12-90-20-640

1A/1C 05-92-01 512, 522,612, 622

C122101 Landing Gear System LubricationTask 12-90-20-641

1A/1C 05-92-01 710, 720,730

DeletedApr 1/08

D211000

A212004 Cabin Air Distribution CheckValves Detailed Inspection Task21-22-00-210

4A/4C 05-92-08 161, 162

DeletedApr 1/08

B213001

B213003 Cabin Altitude Pressure SwitchFunctional Check Task 21-31-05-720

4A/4C 05-92-08 245

Added Apr1/08

B215002 Pressurization System FunctionalCheck Task 21-30-00-720

2A/2C 05-92-03 ENG

DeletedApr 1/08

A215204

DeletedApr 1/08

A215205

Added Jul1/12

A215206 Vapor Cycle Cooling System HourMeter Check. Task 21-52-00-210

MP 05-92-MP 332

Added Jan1/14

A215209 Vapor Cycle Cooling System 500Compressor-Hour Maintenance Task21-52-00-211

Every 500Vapor Cy-cle Cool-ing Com-pressorHours

05-92-51 321, 322

Added Jan1/14

A215210 Vapor Cycle Cooling System12-Month Maintenance Task21-52-00-212

1C 05-92-02 321, 322

D217000 Water Separator Restoration(Cleaning) Task 12-19-02-160

2A/2C 05-92-03 312

D217003 Ozone Converters Restoration(Cleaning) Task 12-19-02-161

5A 05-92-12 321, 322

B236000 Static Discharging System FunctionalCheck Task 23-90-60-720

4C, 2Cthereafter

05-92-11 331, 332,532, 540,632, 640

DeletedApr 1/08

D237000


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/08

B237005 Cockpit Voice Recorder System(Fairchild A200S) Operational Checkor Cockpit Voice Recorder SystemOperational Check (Fairchild FA2100or L3 Communications FA2100) Task23-90-70-710

2C 05-92-04 AUX

RevisedApr 1/08

B237006 Cockpit Voice Recorder UnderwaterLocating Device (ULD) FunctionalCheck Task 23-90-70-720

24 cal-endarmonths(IAW themanu-facturer'sinstruc-tions)

05-92-36 AUX

RevisedApr 1/16

B238000 Standby Nav/Com Control UnitOperational Check (Airplanes -5001thru -6000) Task 23-80-01-710

Every 500hours

05-92-48 AUX

RevisedApr 1/09

B238002 Transponder Functional Check(Airplanes -5001 thru -6000)(Required by 14 CFR 91.413) Task23-90-20-720

24calendarmonths

05-92-45 AUX

RevisedApr 1/16

B243001 Lead-Acid Battery FunctionalCheck (Capacity Check) NOTE:The inspection schedule may beadjusted after the useful battery lifeis established, based on operations.Task 24-90-50-720

600hours/12calendarmonths,thenevery 200hours/3calendarmonthsthereafter

05-92-47 313

RevisedApr 1/08

B243002 Saft Ni-Cad Battery Restoration(Deep Cycle) Task 24-90-50-840


05-92-35 313

RevisedJan 1/14

B245000 Ni-Cad Battery (Saft) FunctionalCheck (Capacity Check) Theinspection interval can be adjustedafter the water loss per cell isestablished. Refer to the BatteryService Table. Task 24-90-50-721

100 hoursor 12calendarmonths

05-92-23 321, 322

RevisedJan 1/14

B245001 Ni-Cad Battery (Marathon) FunctionalCheck (Capacity Check) Theinspection interval can be adjustedafter the water loss per cell isestablished. Refer to the BatteryService Table. Task 24-90-50-722

100 hoursor 12calendarmonths

05-92-23 321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/08

A251003 Crew Seats Detailed Inspection Task25-90-10-220

4A/4C 05-92-08 241, 242

RevisedApr 1/08

A252000 Passenger Seats Detailed InspectionTask 25-90-20-220

4C 05-92-10 261, 262

A256006 Life Raft Detailed Inspection Task25-90-60-221

1C 05-92-02 261, 262

RevisedJul 1/08

B256006 Emergency Locator TransmitterSystem Functional Check (Artex ELT110-4) (Required by 14 CFR 91.207)Task 25-90-60-710

12calendarmonths

05-92-44 BAT

A256007 Life Vest Detailed Inspection Task25-90-60-222

1C 05-92-02 241, 242,251, 252,261, 262

A256008 Smoke Goggle Assembly DetailedInspection Task 25-90-60-223

1C 05-92-02 241, 242

A256009 Water Barrier Assembly DetailedInspection Task 25-90-60-224

1C 05-92-02 313

A256010 First Aid Kit Detailed Inspection Task25-60-01-210

1C 05-92-02 262

RevisedJul 1/08

A256012 Emergency Locator TransmitterSystem Detailed Inspection (ArtexELT 110-4) (Required by 14 CFR91.207) Task 25-90-60-225

12calendarmonths

05-92-44 BAT

Added Jul1/08

A256104 Artex C406-2 Emergency LocatorInspection (Required by 14 CFR91.207) Task 25-61-04-210

12calendarmonths

05-92-44 BAT

Added Jul1/08

B256104 Artex C406-2 Emergency LocatorFunctional Test (Required by 14 CFR91.207) Task 25-61-04-720

12calendarmonths

05-92-44 BAT

Added Jul1/08

A256105 Artex C406-N Emergency LocatorInspection (Required by 14 CFR91.207) Task 25-61-05-210

12calendarmonths

05-92-44 BAT

Added Jul1/08

B256105 Artex C406-N Emergency LocatorFunctional Test (Required by 14 CFR91.207) Task 25-61-05-720

12calendarmonths

05-92-44 BAT

Added Apr1/17

A256106 Artex 110-406 Emergency LocatorInspection Task 25-61-06-210

12calendarmonths

05-92-44 BAT

Added Apr1/17

B256106 Artex 110-406 Emergency LocatorFunctional Test Task 25-61-06-720

12calendarmonths

05-92-44 BAT

DeletedApr 1/08

B261001

DeletedJul 1/15

A262003


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


DeletedApr 1/16

B262004

DeletedApr 1/16

B262005

DeletedApr 1/16

B262008

Added Apr1/08

B262009 Baggage Compartment SmokeDetection System Operational CheckTask 26-90-10-711

4A/4C 05-92-08 311, 312

RevisedApr 1/08

B262011 Engine Fire Extinguishing SystemFunctional Check Task 26-90-20-720

4A/4C 05-92-08 AUX,241, 242,321

B262012 Portable Fire Extinguisher FunctionalCheck (Weight Check) Task26-90-20-721

1C 05-92-02 242, 262

AddedSep13/17

B262014 Optional Aft Vanity Fire ExtinguisherBottle Functional Check (WeightCheck) Task 26-90-20-723

5 Years 05-92-38 261, 262

B262013 APU Fire Extinguishing SystemFunctional Check Task 26-90-20-722

4A/4C 05-92-08 AUX

B263000 Fuel Shutoff Valve Operational CheckTask 26-90-30-710

1C 05-92-02 241, 242,313, 314

C271002 Aileron Trim Tab Actuator LubricationTask 27-90-10-640

1A/1C 05-92-01 532, 632

C271002 Aileron Trim Tab Actuator LubricationTask 27-90-10-640

1A/1C 05-92-01 532, 632

B271003 Aileron and Aileron Trim Tab ControlSystem Functional Check Task27-90-10-721

4A/4C,2A/4Cthereafter

05-92-09 532, 632

B271004 Aileron Outboard Wing Control CableFunctional Check Task 27-10-00-212

2A/4C 05-92-05 512, 522,532, 612,622, 632

B271005 Aileron Trim Tab Functional Check(Free Play) Task 27-10-00-220

1A/1C 05-92-01 532

B272000 Rudder Trim Tab Functional Check(Free Play) Task 27-20-00-220

1A/1C 05-92-01 340

C272003 Rudder Trim System Lubrication Task27-90-20-640

1A/1C 05-92-01 340

B272004 Rudder and Rudder Trim ControlSystem Functional Check Task27-90-20-721


05-92-09 340

C273003 Elevator Trim Tab Actuator LubricationTask 27-90-30-640

1A/1C 05-92-01 351, 352


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


B273005 Elevator and the Elevator Trim TabSystem Functional Check Task27-90-30-720


05-92-09 351, 352

B274003 Two-Position Horizontal StabilizerFunctional Check Task 27-90-40-720

4A/4C 05-92-08 AUX

Added Oct1/11

B274004 Horizontal Stablizer Scissor FittingBolts and Aft Pivot Bolts LubricationTask 12-21-01-642

2A/2C 05-92-03 340

B275005 Flap System Functional Check Task27-90-50-720

4A/4C 05-92-08 AUX

A276100 Speed Brake System DetailedInspection Task 27-61-00-210

4A/4C 05-92-08 512, 522,612, 622

A277100 Control (Gust) Lock SystemOperational Check Task 27-71-00-710

4A/4C 05-92-08 151

A281000 Fuel Storage System DetailedInspection Task 28-10-00-210

4C 05-92-10 511, 512,521, 522,531, 532,611, 612,621, 622,631, 632

A281100 Fuel Filler Cap Lubrication Task28-11-04-210

1C 05-92-02 531, 631

B284000 Low Fuel Warning System FunctionalCheck Task 28-42-00-710

4C 05-92-10 AUX

D291100 Hydraulic System Filters Discard Task29-11-04-901

6C 05-92-13 313

B301003 Horizontal Stabilizer Deice SystemFunctional Check Task 30-90-10-720

1A/1C 05-92-01 351, 352

RevisedJul 1/08

B301100 Bleed Air Anti-Ice SystemsOperational Check (Airplanes-5001 thru -6000) Task 30-11-00-710

4A/4C 05-92-08 ENG

Added Jul1/08

B301102 Bleed Air Anti-Ice SystemsOperational Check (Airplanes-6001 and On) Task 30-11-00-711

4A/4C 05-92-08 ENG

B304000 Nose Compartment OvertemperatureSwitch Functional Check Task30-40-00-710

4C 05-92-10 AUX

Added Jul1/16

D312002 Davtron Digital Clock Battery -Discard Task 31-20-01-960

1C 05-92-02 LAB

B313002 Flight Data Recorder SystemFunctional Check Task 31-90-30-720

4C 05-92-10 322

DeletedApr 1/08

A313002


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/08

B313003 Flight Data Recorder UnderwaterLocating Device (ULD) FunctionalCheck Task 31-90-30-721


05-92-36 312

Added Apr1/13


Inspec-tionitem(s),whichare com-pletedevery 6calendarmonths(for air-planesthat op-erate inmoderateor severecorrosionenviron-ments.Refer toChapter51, Cor-rosionSeverityMaps -Descrip-tion andOpera-tion).

05-92-50 710, 720,730

Added Apr1/13


1C 05-92-02 710, 720,730

DeletedJul 1/15

B320900

B321000 Landing Gear System FunctionalCheck Task 32-90-10-720

4A/4C 05-92-08 AUX

RevisedOct 1/11

A324000 External Zonal Inspection of the Noseand Main Landing Gear Wheel WellsTask 32-90-40-210

4C 05-92-10 710, 720,730

B324001 Emergency Brake System DetailedInspection Task 32-90-40-221

4A/4C 05-92-08 AUX

A324004 Landing Gear Brakes DetailedInspection Task 32-90-40-220

1A/1C 05-92-01 720, 730


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


A324006 Landing Gear Wheels SpecialDetailed Inspection (NDI). Refer to theGoodrich Component MaintenanceManual 32-45-48, Main LandingGear Wheel Assembly, Part Number3-1571 and Goodrich ComponentMaintenance Manual 32-47-42, NoseLanding Gear Wheel Assembly, PartNumber 3-1418. Task 32-90-40-280

IAW themanufac-turer's in-structions

05-92-43 710, 720,730

D324010 Brake System Filters Discard Task32-90-40-960

6C 05-92-13 211

B324011 Emergency Brake SystemOperational Check Task 32-42-09-710

4A/4C 05-92-08 AUX

DeletedApr 1/08

B324012

B335000 Emergency Lighting SystemOperational Check Task 33-50-00-710

1C 05-92-02 BAT

B335002 Emergency Battery Pack(s)Functional Check (Capacity Check)Task 33-90-50-720

2C 05-92-04 BAT

RevisedApr 1/09

B341100 Pitot-Static System Functional Check(Airplanes -5001 thru -6000) Required14 CFR 91.411, 91.413 and RVSMcertification Task 34-90-10-210

24calendarmonths

05-92-45 AUX

RevisedApr 1/09

B341200 Pitot-Static System Functional Test(Airplanes -6001 and On) Required14 CFR 91.411, 91.413 and RVSMcertification Task 34-90-12-210

24calendarmonths

05-92-45 AUX

RevisedApr 1/08

B342005 L3 Com Standby Battery PackFunctional Check (Capacity Check)Task 34-20-00-762


05-92-35 211

RevisedApr 1/08

B342006 L3 Com Standby Battery PackOperational Check (Periodic Check)Task 34-90-20-710


05-92-34 211


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/08

B342007 Securaplane Standby BatteryOperational Check (Energy Level)Task 34-20-00-763


05-92-34 211

Added Apr1/09

B345307 Transponder System FunctionalCheck (Airplanes -6001 and On)(Required by 14 CFR 91.413) Task34-53-07-720

24calendarmonths

05-92-45 AUX

DeletedOct 1/11

B350000

DeletedOct 1/11

B350001

B350100 Passenger Oxygen SystemFunctional Check Task 35-01-00-710

4C 05-92-10 AUX

DeletedApr 1/09

D351001

A351005 Crew Masks and StowageBoxes Detailed Inspection Task35-90-10-220

3C 05-92-07 241, 242

B352000 Passenger Oxygen SystemOperational Check Task 35-90-20-710

2C 05-92-04 241, 242,251, 252,AUX

A352000 Dropout Boxes and MaskAssembly Detailed InspectionTask 35-90-20-220

4C 05-92-10 251, 261

Added Apr1/10

A353003 Protective Breathing EquipmentDetailed Inspection Task35-30-00-220

1C 05-92-02 251, 252,261, 262

D361000 Cabin Door Particulate TrapRestoration (Cleaning) Task36-15-00-170

4A/4C 05-92-08 261

RevisedApr 1/10

A361102 Precooler Heat Exchanger GeneralVisual Inspection Task 36-11-03-210

1A/1C 05-92-01 411, 412

RevisedJul 1/08

B383000 Externally Serviceable ToiletFunctional Check Task 38-30-02-720

3A/3C 05-92-06 262

D493000 APU Fuel Filter Element Discard Task49-90-30-960

1000APUhrs/2C

05-92-18 321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


A494000 APU Igniter Plug Detailed InspectionTask 49-90-40-220

1000APUhours(IAW themanu-facturer'sinstruc-tions)

05-92-30 321, 322

RevisedApr 1/08

A497000 APU Magnetic Chip Collector DetailedInspection Task 49-90-70-220

500 APUhrs / 2C

05-92-17 321, 322

D499000 APU Oil Filter Element Discard Task49-90-90-960

1000APUhrs/2C

05-92-18 321, 322

D499001 APU Oil Discard Task 49-90-90-961 1000APUhrs/2C

05-92-18 321, 322

C521001 Aircraft Locks Lubrication Task52-90-00-640

1C 05-92-02 211, 212,323, 331,810

A521005 Cabin Door Seals General VisualInspection Task 52-90-10-210

1C 05-92-02 810

A521006 Cabin Door Detailed Inspection Task52-10-00-210

4A/4C 05-92-08 810

Added Apr1/09

A521007 Cabin Door Detailed Inspection(Chapter 4 requirement) Task52-10-00-210

Inspectevery15,000hours(Chapter4 require-ment)

05-92-ME 810

A522002 Emergency Exit Door DetailedInspection Task 52-20-00-210

2C 05-92-04 820

Added Apr1/09

A522003 Emergency Exit Door DetailedInspection (Chapter 4 requirement)Task 52-20-00-210


05-92-ME 820

A523001 Baggage Door Detailed InspectionTask 52-90-30-220

4A/4C 05-92-08 311

DeletedApr 1/17

A530003


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedOct 1/11

A530004 External Zonal Inspection of theFuselage Task 53-90-00-211

8C 05-92-14 110, 141,142, 153,154, 163,164, 165,166, 211,212, 221,222, 241,242, 251,252, 261,262, 311,312, 313,314, 321,322, 810,820

RevisedOct 1/11

A530005 Internal Zonal Inspection of the CabinSection Task 53-90-00-212

8C 05-92-14 151, 152,161, 162,251, 252,261, 262,810, 820

Added Oct1/11

A530006 Internal Zonal Inspection of theCockpit Below Floorline Task53-90-00-213

8C 05-92-14 141, 142,244

Added Oct1/11

A530007 Internal Zonal Inspection of theCockpit Above Floorline Task53-90-00-214

8C 05-92-14 235, 241,242, 244,245, 246,247, 248

Added Oct1/11

A530008 Internal Zonal Inspection of the TailSection Task 53-90-00-215

8C 05-92-14 311, 312,321, 322

Added Oct1/11

A530009 Internal Zonal Inspection of the NoseSection Task 53-90-00-216

8C 05-92-14 110, 211,212, 221,222, 710

Added Oct1/11

A530010 Internal Zonal Inspection of the APUin the Tail Section Task 53-90-00-217

2C 05-92-04 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/13


Inspec-tionitem(s),whichare com-pletedevery 6calendarmonths(for air-planesthat op-erate inmoderateor severecorrosionenviron-ments.Refer toChapter51, Cor-rosionSeverityMaps -Descrip-tion andOpera-tion)

05-92-50 710

Added Apr1/13


1C 05-92-02 710

Added Jan1/15

A530017 Tailcone Area General VisualInspection Task 53-90-00-218

1C 05-92-02 313, 321,322

Added Jan1/15

A530018 Tailcone Under Floor Area andTailcone Stringer General VisualInspection Task 53-90-00-219

2C 05-92-04 313, 321,322

Added Oct1/11

A531001 Internal Zonal Inspection of theEmpennage Task 53-90-10-210

8C 05-92-14 340, 351,352

Added Oct1/11

A531002 External Zonal Inspection of theEmpennage Task 53-90-10-211

8C 05-92-14 340, 351,352

RevisedOct 1/07

A531014 Aft Pressure Bulkhead Inspection(Chapter 4 Requirement) Task53-10-11-252


05-92-ME 311, 312


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/13

A531021 Forward Pressure BulkheadInspection (Chapter 4 Requirement)Task 53-10-11-251

Inspectat thefirst 6000hours/tenyearswhiche-ver oc-curs first,then ev-ery 2400hours/tenyearswhiche-ver oc-curs firstthereafter(Chapter4 require-ment)

05-92-MD 221, 222

RevisedApr 1/08

A533003 Fuselage External Surface SpecialDetailed Inspection (Eddy Current)Task 53-30-01-250

2400hoursor 72calendarmonths,thenevery1200hoursor 36calendarmonthsthereafter

05-92-40 141, 142,151, 152,161, 162,241, 242,251, 252,261, 262

Added Apr1/09

A533005 Upper Skin Splice at BL 0.00 (Chapter4 requirement) Task 53-30-01-251


05-92-ME 251, 252,261, 262

Added Apr1/09

A533007 Lower Skin Splice at Stringer 13(Chapter 4 requirement) Task53-30-01-252


05-92-ME 141, 142,151, 152,161, 162

Added Apr1/09

A533009 Lower Skin from Right Stringer13 to Left Stringer 13 (Chapter 4requirement) Task 53-30-01-210


05-92-ME 141, 142,151, 152,161, 162,321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/09

A533011 Upper Skin from Right Stringer13 to Left Stringer 13 (Chapter 4requirement) Task 53-30-01-210


05-92-MJ 241, 242,251, 252,261, 262,311, 312,321, 322

RevisedOct 1/11

A535000 Internal Zonal Inspection of theFuselage Fairing Task 53-90-50-210

8C 05-92-14 151, 152,153, 154,161, 162,163, 164,165, 166,313, 314

Added Oct1/11

A545000 Forward Engine Beam, Upper Angles,Horizontal Cap Flange at BL 30.5 toBL 42.0 Special Detailed Inspection(Eddy Current) Task 54-50-10-250


05-92-MJ 311, 312,411, 412

Added Apr1/13

A551004 Horizontal Stabilizer Aft Spar AreaGeneral Visual Inspection (CorrosionInspection). Task 55-10-01-212


05-92-50 351, 352

Added Apr1/13

A551005 Horizontal Stabilizer Aft Spar AreaGeneral Visual Inspection (CorrosionInspection). Task 55-10-01-212

1C 05-92-02 351, 352


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedApr 1/13

A553004 Vertical Spar Pivot Fitting LowerFlange and Clip Inspection (Thisinspection is necessary for Airplanesthat have not replaced the one-piececlip with a two-piece assembly.) Task55-30-01-211

2A/4C 05-92-05 340

RevisedOct 1/10

A553008 Vertical Stabilizer Rear Spar Capat WL 146.00 (Airplanes -5001 thru-5020) (Chapter 4 requirement) Task55-30-01-250

MG 05-92-MG 340

RevisedOct 1/10

A553009 Vertical Stabilizer Rear Spar NestedAngle at WL 146.00 (Airplanes -5001thru -5020) (Chapter 4 requirement)Task 55-30-01-251

MH 05-92-MH 340

RevisedOct 1/10

A553010 Vertical Stabilizer Rear Spar Strapat WL 146.00 (Airplanes -5001 thru-5020) (Chapter 4 requirement) Task55-30-01-252

MI 05-92-MI 340

RevisedOct 1/10


Inspect atthe first11,500hours,then ev-ery 9000hoursthereafter(Chapter4 require-ment)

05-92-MK 321, 322

Added Apr1/13



05-92-MR 340


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/13



05-92-50 340

Added Apr1/13


1C 05-92-02 340

Added Apr1/16

A553019 Vertical Stabilizer Internal InspectionTask 55-30-01-212

First 6000hours,thenevery1200hoursthereafter

05-92-52 340

DeletedOct 1/07

B561002

A561100 Windshield Humpseal DetailedInspection Task 56-11-00-210

400hrs/1C

05-92-16 241, 242

RevisedApr 1/08

B561100 Windshield Surface Seal TreatmentFunctional Check Task 56-11-00-720

400hrs/1C

05-92-16 241, 242

RevisedApr 1/09

A561101 Cockpit Windshield and Side WindowsDetailed Inspection (Delamination)Task 56-11-00-212

4A/2C 05-92-19 241, 242

RevisedApr 1/09

A561102 Windshield Retainer ScrewsFunctional Check (Torque Inspection)Task 56-11-00-280

4A/2C 05-92-19 241, 242


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/13

A561103 Cockpit Openable Aft Side WindowHinge and Latch Inspection Task56-11-00-213

1C 05-92-02 241, 242

RevisedOct 1/11

A570000 External Zonal Inspection of theWings Task 57-90-00-210

12C 05-92-15 511, 512,521, 522,531, 532,540, 611,612, 621,622, 631,632, 641,720, 730

RevisedApr 1/09

A571001 Lower Wing Main Spar Lower SkinSplice at WS 22.50 (Chapter 4requirement) Task 57-10-00-250

Inspectat thefirst 7500hours,then ev-ery 1400hoursthereafter(Chapter4 require-ment)

05-92-MF 511, 512,611, 612

RevisedApr 1/09

A571003 Lower Wing Main Spar Lower SkinSplice at WS 22.50 (Chapter 4requirement) Task 57-10-00-270


05-92-MF 511, 512,611, 612

Added Apr1/09

A571005 Lower Wing Main Spar Skin SpliceFlange at WS 11.50 (Chapter 4requirement) Task 57-10-00-251


05-92-ML 511, 512,611, 612


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/09

A571007 Lower Wing Main Spar and SkinSplice at WS 11.50 (Chapter 4requirement) Task 57-10-00-271


05-92-ML 511, 512,611, 612

Added Apr1/09

A571009 Lower Wing Main Spar at WS114.57 (Chapter 4 requirement) Task57-10-00-252


05-92-MM 521, 522,621, 622

Added Apr1/09



05-92-MN 521, 522,621, 622

Added Apr1/09



05-92-MO 521, 522,621, 622


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/13



05-92-50 512, 522,532, 612,622, 632

Added Apr1/13


1C 05-92-02 512, 522,532, 612,622, 632


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


Added Apr1/13



05-92-50 512, 612

Added Apr1/13


1C 05-92-02 512, 612

RevisedOct 1/11

A710000 Internal Zonal Inspection ofthe Engines and Pylons Task71-90-00-210

2C 05-92-04 410, 411,412, 420

Added Oct1/11

A710001 External Zonal Inspection ofthe Engines and Pylons Task71-90-00-211

2C 05-92-04 410, 411,412, 420

A711100 Upper Cowling Camloc Hole DetailedInspection Task 71-11-00-220

4C 05-92-10 410, 420

A711101 Forward and Aft Upper CowlingEdge Detailed Inspection Task71-11-00-221

4C 05-92-10 410, 420


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

REVISIONSTATUS

ITEM CODENUMBER


RevisedOct 1/11

A712201 Aft Engine Beam Inspection (Chapter4 Requirement) NOTE: This enginesupport structure inspection is forAirplanes -5001 thru -5060. Task71-22-00-210


05-92-MB 311, 312,411, 412

A761103 Fuel Control Unit (FCU) Throttle LeverCutoff Functional Check (Airplanes-5001 thru -5196 Not IncorporatingSB560XL-76-03) Task 76-10-00-620

150 hrs 05-92-24 410, 420

RevisedOct 1/10

A761104 Fuel Control Unit (FCU) Throttle LeverCutoff Functional Check (Airplanes-5197 thru -6000, and Airplanes-5001 thru -5196 IncorporatingSB560XL-76-03) Task 76-10-00-620

300 hrs 05-92-25 410, 420

Added Jul1/12

A761600 Time Limited Dispatch OperationalCheck (Airplanes -6001 and On) Task76-16-00-710

MQ 05-92-MQ 235

RevisedApr 1/09

C783001 Thrust Reverser Lubrication (WC-393Non-Aerosol Spray LubricationMethod) Task 78-31-00-640

300 hrs 05-92-25 410, 420

RevisedApr 1/09

C783002 Thrust Reverser Guide RodsLubrication (D-5100NS AerosolSpray Lubrication Method) Task78-31-00-641

300 hrs 05-92-25 410, 420

C783003 Lubrication of the Thrust ReverserPivot Points (C-5A AntiseizeCompound Lubrication Method) Task78-31-00-642

600 hrs 05-92-27 410, 420

B783025 Thrust Reverser System FunctionalCheck Task 78-90-30-720

2A/2C 05-92-03 AUX

A783100 Thrust Reverser System DetailedInspection Task 78-31-00-210

2A/2C 05-92-03 410, 420

DeletedOct 1/07

D801000

DeletedOct 1/07

D801100

RevisedOct 1/07

A801103 APU Starter Generator DetailedInspection Task 80-90-11-220

500 APUhours

05-92-26 321, 322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

MSG-3 COMPONENT TIME LIMITS

1. Component Time Limits

A. All components not recorded here must be examined as given in other sections of this chapter andrepaired, overhauled, or replaced as necessary. The items in the list that follows must be overhauledor replaced during the regular maintenance periods done nearest to the specified limit.

B. Items that are underlined are Chapter 4, Airworthiness Limitations requirements. Refer toChapter 4, Airworthiness Limitations for additional information.

C. The replacement life for each component recorded in this section applies to the part throughout its lifeon the original installation and on later installations. The life (number of hours or number of landings)must be recorded individually for these components and must stay with the component during removal.For example, if a component is removed for overhaul, it must be tagged with the life (number of hoursor number of landings) to the date of removal and this tag must stay with the component throughoutthe overhaul process. (Overhaul of a component does not zero time the life of the component.) Whenthe component is received from overhaul and installed on an airplane, its life must be recorded toallow continued accumulation toward the life-limit.

D. Components which have gone through overhaul or replacement times because of a current change inthe inspection program can continue in service. The component must be serviceable and immediatelyscheduled for overhaul, or you must send an order for a replacement component. Do not extend thetime more than 60 days due to overhaul schedules or components that are not available.

2. Schedule

A. Air Conditioning (Chapter 21).(1) Vapor Cycle Cooling System

(a) Compressor Drive Motor Brushes (Compressor Motors 1134104-1, -5) - Replace every 500compressor hours.

NOTE: Refer to the Enviro Systems Inc. Operating, Servicing and ComponentMaintenance Manual 21-00-06.

B. Communications (Chapter 23).(1) Cockpit Voice Recorder Underwater Locating Device (ULD) Battery - Discard every 6 years.

Refer to Task 23-90-70-960.

C. Equipment/Furnishings (Chapter 25).(1) Artex 110-4 Emergency Locator Transmitter Battery- Discard every 2 years. Refer to Task 25-

90-60-960.(2) Artex 110-406 Emergency Locator Transmitter Battery- Discard every 5 years. Refer to Task

25-90-60-960.(3) Artex C406-2 Emergency Locator Transmitter Battery- Discard every 5 years. Refer to Task

25-90-60-960.(4) Artex C406-N Emergency Locator Transmitter Battery - Discard every 5 years. Refer to Task

25-90-60-960.

D. Fire Protection (Chapter 26).(1) Fire Bottle Cartridges. Refer to Table 1.

(a) Engine Fire Bottle Cartridge. Refer to Task 26-90-30-960.(b) APU Fire Bottle Cartridge. Refer to Task 26-90-30-961.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

Table 1. Fire Bottle Cartridge Life

CARTRIDGE PART NUMBER SERVICE LIFE (YEARS) TOTAL LIFE (YEARS)

13083-5 6 6

AE13083-5 The combined shelf-life andthe service life cannot exceed

ten (10) years.

10

NOTE: Service life is the amount of time the explosive cartridge is installed in a fireextinguisher. Service life of any particular explosive cartridge can not be extended.

NOTE: Total life starts on the day the cartridge is made and must be replaced at a specifictime. A date (month/year) is stamped or marked on the plastic bag containing thecartridge or on the cartridge body. Total life cannot be extended and includesany mix of time the explosive cartridge is kept ”on the shelf” and/or installed in afire extinguisher.

(2) Portable Fire Extinguisher Bottle - Complete the NFPA required internal inspection every 6 years(refer to Task 26-90-20-842).

(3) Portable Fire Extinguisher Bottle - Complete the NFPA required hydrostatic test every 12 years(refer to Task 26-90-20-841).

(4) Engine Fire Extinguisher Bottle - Complete the required hydrostatic test every 60 calendarmonths (refer to Task 26-90-20-840)

(5) APU Fire Extinguisher Bottle - Complete the required hydrostatic test every 60 calendar months(refer to Task 26-90-20-843)

E. Flight Controls (Chapter 27).(1) Flaps

(a) Inboard and Outboard Flap Rollers (Part Number S3049-5F8) - Replace every 5000landings.

(2) Elevators(a) Elevator Trim Cables

1 Aft Elevator Trim Cable Assembly (Part Number 6660003-1) - Replace every 4800hours

NOTE: The trim cable assembly is made using an up, down and center cable(Part Number 6660002-35, -36, -67).

F. Indicating/Recording Systems (Chapter 31).(1) Flight Data Recorder Underwater Locating Device (ULD) Battery - Discard every 6 years. Refer

to Task 31-90-30-960.

G. Landing Gear (Chapter 32).(1) Landing Gear Extension/Retraction System

(a) Emergency Pneumatic Storage Bottle - Replace (Discard) every 24 years. Refer to Task32-30-09-281.

(b) Pneumatic Storage Bottle - Complete a hydrostatic test every 3 years, in accordance with(IAW) the manufacturers instructions. Refer to Task 32-30-09-280.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Main Landing Gear



(a) Main Landing Gear Breather Vent - Discard every 600 hours or 12 calendar months,whichever occurs first. Refer to Task 32-10-00-960.

(b) Trunnion Subassembly1 Left Trunnion Subassembly (Part Number 6641640-5) - Replace every 7600 landings.2 Right Trunnion Subassembly (Part Number 6641640-6) - Replace every 7600






33,300 landings.(c) Trailing Link Assembly









(d) Oleo Assembly1 Oleo Assembly (Part Number 6641615-3, -4), except the part that follows - Replace



(e) Actuator Assembly1 Left Actuator Assembly (Part Number 9912537-1, -3, -5) - Replace every 70,200


landings.(f) Trailing Link Spacer

1 Trailing Link Spacer (Part Number 6641618-9, -12) - Replace every 6200 landings.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

2 Trailing Link Spacer (Part Number 6641533-1, -2) - Replace every 33,300 landings.(3) Nose Landing Gear





landings.

H. Navigation (Chapter 34).(1) Securaplane Standby Battery - Discard every 4 years. Refer to Task 34-90-20-960.

I. Oxygen (Chapter 35).(1) Oxygen bottle (cylinder) hydrostatic test and discard.

NOTE: DOT Ratings are used to find the correct hydrostatic test and service life intervals.

NOTE: US DOT Exemption E 8162 was replaced by US DOT Special Permit SP 8162dated May 11, 2007. DOT-SP 8162 applies to all cylinders manufactured afterSeptember 30, 2007 and DOT-E 8162 cylinders hydrostatic tested after July 1,2006. Reference AVOX Service Information Letters SIL-35-114 and SIL-35-116.

NOTE: DOT-SP 8162 applies to DOT3FC1850 cylinders.

(a) Hydrostatic test, refer to Table 2 for the correct Hydrostatic Test Interval and related Task.

Table 2. Oxygen Bottle Hydrostatic Test Intervals

DOT RATING HYDROSTATIC TEST INTERVAL TASK NUMBER

DOT3AA 5 years (NOTE 1) 35-90-00-840

DOT-SP 8162 5 years 35-90-00-840

NOTE 1: The DOT3AA text requirement is 5 years. If the hydrostatic test is overdue, you can complete the testat the next calendar-based interval.

(b) Discard, refer to Table 3 for the correct Service LIfe Interval and related Task.

Table 3. Oxygen Bottle Service Life Intervals

DOT RATING SERVICE LIFE INTERVAL TASK NUMBER

DOT3AA N/A N/A

DOT-SP 8162 15 years 35-90-00-960


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(2) Oxygen mask (EROS) - Overhaul every 6 Years. Refer to Task 35-90-10-840 Crew MasksRestoration (Overhaul).

NOTE: Under normal environmental conditions and use, the crew oxygen masks must beoverhauled every 6 years. If the crew oxygen masks are exposed to environmentsthat accelerate aging of elastomer components, periodic inspection may warrantshorter intervals between overhaul periods.

(3) Protective Breathing Equipment - Discard every 10 years. Refer to Task 35-30-00-960.

J. Fuselage (Chapter 53)(1) Trunnion Attach Fitting Assemblies




-3) - Replace every 25,500 landings.

NOTE: Actuator Fitting Part numbers 6211191-2, -3 are components of the6211190-41, -42 Actuator Fitting Assemblies.

(b) Actuator Fitting Assembly on Airplanes 560-5501 and On, (Part Number 6611591-9, -10)- Replace every 25,500 landings.

K. Wing (Chapter 57)(1) Trunnion Attach Fitting Assemblies






23,800 landings.

L. Powerplants (Chapter 71).(1) Forward and Aft Engine Mount Isolators - Replace at every second Engine Overhaul.

NOTE: The engine mount isolators do not have an hourly replacement requirement. Theyare replaced by the number of engine overhauls. You can purchase the exchangedor overhauled engine mount isolators, which are approved to be installed asreplacement engine mount isolators, through Citation Parts Distribution.

(a) Forward Engine Mount Isolators - LM-451-SA1 and LM-451-SA4 (Cessna Part Number9912480-1)

(b) Aft Engine Mount Isolators - LM-451-SA2 (Cessna Part Number 9912480-2)

M. Starting (Chapter 80).(1) Engine Starter-Generator Restoration - Overhaul every 1000 hours. Refer to Task 80-90-10-840.(2) APU Starter-Generator Restoration - Overhaul every 1000 APU hours. Refer to Task 80-90-11-

840.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

MSG-3 CONTINUOUS INSPECTION PROGRAM

1. Purpose and Use

A. As given in Part 91.409, paragraph (e) of Title 14 of the Code of Federal Regulations, Turbo JetAirplanes must have inspections that have an approved inspection schedule. This section gives thecontinuous inspection programs for the Model 560XL, recommended by Cessna Aircraft Company.

2. Title 14 of the Code of Federal Regulations

A. General Operating and Flight Rules, Part 91.409.(1) No person can operate a large airplane, or a turbojet multi-engine airplane, or turbo-propeller-

powered multi-engine airplane or turbine-powered rotorcraft unless the specified replacementtimes for the life-limited parts in the aircraft specifications, type data sheets or other documentsapproved by the Administrator are obeyed and the airplane, or turbine-powered rotorcraftwhich includes the airframe, engines, propellers, rotors, appliances, survival equipment andemergency equipment, is examined with an inspection program set in accordance with theprovisions of Part 91.409 paragraph (f). However, the owner or operator of a turbine-poweredrotorcraft can use the provisions of paragraph 91.409(a), (b), (c) or (d) as an alternativeinspection option of paragraph (f).

(2) The registered owner or operator of each airplane or turbine powered rotorcraft given in 91.409paragraph (e) must have the selection and identify in the aircraft maintenance records and useone of the programs that follow for the inspection of the airplane:(a) A continuous airworthiness inspection program that is a part of a continuous airworthiness

maintenance program currently in use by a person that has an air carrier operatingcertificate issued in accordance with Part 121, 127, or 135 of this chapter and operatesthat make and model aircraft in accordance with Part 121 of this chapter and does themaintenance in accordance with paragraph 135.411(a)(2) of this chapter.

(b) An aircraft inspection program approved in accordance with paragraph 135.419 of thischapter and currently in use by a person that has a certificate in accordance with Part 135of this chapter.

(c) A current inspection program recommended by the manufacturer.(d) Any other inspection program established by the registered owner or operator of that

airplane or turbine-powered rotorcraft and approved by the Administrator in accordancewith paragraph (g) of this section. However, the Administrator can require revision to thisinspection program in accordance with the provisions of Part 91.415.

(3) Each operator must include in the selected program, the name and address of the responsibleperson who schedules the inspections required by the program and make a copy of that programavailable to the person that completes the inspections on the aircraft and, upon request, to theAdministrator.

(4) Each operator of an airplane or turbine-powered rotorcraft desiring to establish or change anapproved inspection program in accordance with paragraph (f)(4) of this section must submitthe program for approval to the local FAA Flight Standards district office that has jurisdictionover the area in which the aircraft is based. The program must include the information thatfollows:(a) Instructions and procedures for the conduct of inspections for the particular make and

model airplane including necessary tests and checks. The instructions and proceduresmust set forth in detail the parts and areas of the airframe, engines, propellers, rotors andappliances, including emergency equipment, required to be inspected.

(b) A schedule to complete the inspections that must be done in accordance with the programexpressed in terms of the time in service, calendar time, number of system operations, orany combination of these.

(c) When an operator changes from one inspection program, in accordance with paragraph(f) of this section, to another, the time in service, calendar times, or cycles of operationaccumulated in accordance with the previous program must be applied in determininginspection due times in accordance with the new program.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

3. Construction

A. The published MSG-3 program is the basis for the MSG-3 Continuous Inspection Program for theModel 560XL and is recommended by Cessna Aircraft Company.

B. A continuous maintenance inspection program schedule applicable for your airplane must be selectedas early as possible. The inspection program timing begins from the Date of Airworthiness.

C. Operators can choose to complete their own inspection method not given in the manual. However,these inspection programs must be tracked by the operator.

D. The majority of the Model 560XL Maintenance Steering Group-3 (MSG-3) Continuous InspectionPrograms use MSG-3 analysis to set the intervals. Most inspections repeat either as a result of anumber of calendar year(s) or a number of hours that can be divided by 600.

E. Intervals for some inspections can be determined by the manufacturer of the component that isexamined. The applicable manufacturers manual gives the information necessary to determinethose intervals. Refer to the Introduction, Supplier Publication List.

F. The inspection program is divided into inspections to help the continuous type inspections to becompleted.

4. Maintenance Manual - Compact Disc - Read Only Memory (CD-ROM)

A. The maintenance manual on CD-ROM contains a search feature. With this, any item code can befound, quickly and entirely. Along with the item code, task information about the inspection and zoneis given. A task number is supplied with the items which give special inspection instructions. When atask number is clicked on, the link will show the task information from the appropriate section of themanual.

B. The end of each task is clearly shown with the message, “End of Task”.

5. Logbook Forms, Pilot Information

A. Airplane Flight Log, Section 1.(1) This gives an easy place to keep individual and collected flight records, total hours on the airplane

and each engine, total landings for the airplane, and the cycles of each engine.(2) The original of the Flight Log form is put in Section 1 of the Approved Airplane Flight and

Maintenance Logbook and kept as part of the permanent airplane log.

B. Form Completion.(1) The basic information at the top of this form must be completed. Enter the number of the page

as it is put in the logbook section which begins with 1. The line "Accumulated Totals BroughtForward" is the collected recorded information which is carried forward from the previous page.This is a journey log and one line shows one flight. In the rows that follow, you record:

1. The date of each flight.

2a. City where flight originated.

2b. City of flight destination.

3. The number of persons aboard, including crew.

4. Distance of flight in nautical miles.

5. The flight duration in hours and tenths of an hour from flight hourmeter.

6. Accumulated total airplane time in hours and tenths of an hour.

7. Accumulated total time for engine 1 in hours and tenths of an hour.

8. Accumulated total time for engine 2 in hours and tenths of an hour.

9. Number of landings for this flight.


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

10. Accumulated total airplane landings.



13. The discrepancy sheet number column gives a reference to the airplane discrepancy form whichhas the airplane discrepancies on a particular flight. If there are no discrepancies, "NONE"must be entered in this column. This gives the pilot an easy method to find if the airplanediscrepancies from other flights were corrected.

14. The last name of the pilot and copilot for each flight must be recorded in the last column.

15. The line "Accumulated Totals" must be filled in after the form is completely filled or at the endof the CESCOM reporting period.

(2) The totals of these lines are put on the line "Accumulated Totals Brought Forward" on the nextairplane flight log form used.

(3) The original (white sheet) must be put in the Airplane Flight and Maintenance Logbook in Section1.

(4) The first copy (pink sheet) must be mailed to the address at the top of the form and is used byCESCOM to make a report about airplane use.

(5) The second copy (yellow sheet) provides an extra customer copy and should be filed at theairplane base.

Table 1. Model 560XL Logbook includes the airplane and engine logs that follow:

SECTION 1 Flight Time Information SECTION 6 Left Engine Maintenance andService Bulletin

SECTION 2 Pilot Squawk on Last Flight SECTION 8 Right Engine Maintenance andService Bulletin

SECTION 3 General Airplane Maintenance SECTION 10 Service Condition Reports

SECTION 4 Service Bulletin SECTION 11 Component Master InventoryCross-Reference List

SECTION 5 Engine Change

Table 2. New pages for the airplane logbook are given below:

Airplane SECTION 1 Airplane Flight Log

Airplane SECTION 2 Airplane Discrepancies



Airplane SECTION 5 Engine Change Record

Left Engine SECTION 6 Engine Logbook

Right Engine SECTION 8 Engine Logbook

Airplane SECTION 10 Service Condition Report

SECTION 11 Component Master Inventory Cross-Reference List

C. Mechanic's Information:(1) Mechanics will fill out the airplane and engine maintenance records and use a "Maintenance

Transaction Report" for more pages in the airplane logbook in Sections 3, 4, 6, and 8.(2) Put copies of the documents that follow in the front of the airplane logbook.

(a) Inspection program selection (sample letter)


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

(b) Inspection records(c) Subsequent inspections

6. Maintenance Transaction Report

A. Information contained in this report is given as follows:(1) Maintenance Log - Airplane or engine entry.(2) Date - Put the month, day, and year when the maintenance is completed.(3) Airplane Serial Number and Airplane Registration Number.(4) Total Airplane Hours.(5) Complete When Applicable.(6) Write in the three-letters designation for the city where the maintenance transaction is completed.

(a) Item Name - The component for which the transaction is done.(b) Position - Left or right, inboard or outboard.(c) Part Number.(d) Serial Number of the installed part.(e) Removal Reason - Put a mark in the box which agrees with the reason for the component

removal.(f) Status of Installed Part - Put a mark for the status of the part installed.(g) Time Between Overhaul (TBO) - Put a mark in one of the boxes under (check one). Next,

put the TBO change in the blank and mark one of the TBO controls. If the (OK as is) boxhas a mark, nothing else needs to be done in this box.

(h) Time Since Overhaul (TSO) - If an overhaul component is installed, put its TSO in the blockand mark the type of control.

(i) Section and Page Numbers.(j) Type of Maintenance.(k) Information and Other Log Entries(l) Enter pages in the logbook as needed:

1 Page 1, White in the logbook2 Page 2, Pink in CESCOM3 Page 3, Yellow to the Airplane Base Files


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT 1

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-01 gives a list of MSG-3 interval 1A/1C items, which are completed every600 hours or 12 calendar months, whichever occurs first.






ITEM CODENUMBER


A324004 Landing Gear Brakes Detailed Inspection Task32-90-40-220

720, 730

A361102 Precooler Heat Exchanger General VisualInspection Task 36-11-03-210

411, 412

B271005 Aileron Trim Tab Functional Check (Free Play) Task27-10-00-220

532

B272000 Rudder Trim Tab Functional Check (Free Play) Task27-20-00-220

340

B301003 Horizontal Stabilizer Deice System FunctionalCheck Task 30-90-10-720

351, 352

C122100 Flap System Lubrication Task 12-90-20-640 512, 522,612, 622

C122101 Landing Gear System Lubrication Task12-90-20-641

710, 720,730

C271002 Aileron Trim Tab Actuator Lubrication Task27-90-10-640

532, 632

C272003 Rudder Trim System Lubrication Task 27-90-20-640 340


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


C273003 Elevator Trim Tab Actuator Lubrication Task27-90-30-640

351, 352

D121400 Shimmy Damper Servicing Task 12-90-20-610 710

*** End of Inspection Document 1 Inspection Items***


CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-02 gives a list of MSG-3 interval 1C item(s), which are completed every12 calendar months.


C. The right portion of each page provides room for the mechanic''s and inspector''s initials and remarks.These pages may be reproduced as a checklist for use when performing this inspection phase.




ITEM CODENUMBER


A215210 Vapor Cycle Cooling System 12-Month MaintenanceTask 21-52-00-212

321, 322

A256006 Life Raft Detailed Inspection Task 25-90-60-221 261, 262

A256007 Life Vest Detailed Inspection Task 25-90-60-222 241, 242,251, 252,261, 262

A256008 Smoke Goggle Assembly Detailed Inspection Task25-90-60-223

241, 242

A256009 Water Barrier Assembly Detailed Inspection Task25-90-60-224

313

A256010 First Aid Kit Detailed Inspection Task 25-60-01-210 262

B262012 Portable Fire Extinguisher Functional Check(Weight Check) Task 26-90-20-721

242, 262

B263000 Fuel Shutoff Valve Operational Check Task26-90-30-710

241, 242,313, 314

B263001 Hydraulic Shutoff Valve Operational Check Task26-90-30-711

241, 242,313, 314

A281100 Fuel Filler Cap Lubrication Task 28-11-04-210 531, 631


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


D312002 Davtron Digital Clock Battery - Discard Task31-20-01-960

LAB


710, 720,730

B335000 Emergency Lighting System Operational CheckTask 33-50-00-710

BAT

A353003 Protective Breathing Equipment Detailed InspectionTask 35-30-00-220

251, 252,261, 262

C521001 Aircraft Locks Lubrication Task 52-90-00-640 211, 212,323, 331,810

A521005 Cabin Door Seals General Visual Inspection Task52-90-10-210

810


710

A530017 Tailcone Area General Visual Inspection Task53-90-00-218

313, 321,322

A551005 Horizontal Stabilizer Aft Spar Area GeneralVisual Inspection (Corrosion Inspection). Task55-10-01-212

351, 352


340

A561103 Cockpit Openable Aft Side Window Hinge andLatch Inspection Task 56-11-00-213

241, 242


512, 522,532, 612,622, 632


512, 612



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-03 gives a list of MSG-3 interval 2A/2C item(s), which are completed every1200 hours or 24 calendar months, whichever occurs first.






ITEM CODENUMBER


A783100 Thrust Reverser System Detailed Inspection Task78-31-00-210

410, 420

B215002 Pressurization System Functional Check Task21-30-00-720

ENG

B274004 Horizontal Stablizer Scissor Fitting Bolts and AftPivot Bolts Lubrication Task 12-21-01-642

340

B783025 Thrust Reverser System Functional Check Task78-90-30-720

AUX

D217000 Water Separator Restoration (Cleaning) Task12-19-02-160

312



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B237005 Cockpit Voice Recorder System (Fairchild A200S)Operational Check or Cockpit Voice RecorderSystem Operational Check (Fairchild FA2100 or L3Communications FA2100) Task 23-90-70-710

AUX

B335002 Emergency Battery Pack(s) Functional Check(Capacity Check) Task 33-90-50-720

BAT

B352000 Passenger Oxygen System Operational CheckTask 35-90-20-710

241, 242,251, 252,AUX

A522002 Emergency Exit Door Detailed Inspection Task52-20-00-210

820

A530010 Internal Zonal Inspection of the APU in the TailSection Task 53-90-00-217

322

A530018 Tailcone Under Floor Area and Tailcone StringerGeneral Visual Inspection Task 53-90-00-219

313, 321,322


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A710000 Internal Zonal Inspection of the Engines and PylonsTask 71-90-00-210

410, 411,412, 420

A710001 External Zonal Inspection of the Engines andPylons Task 71-90-00-211

410, 411,412, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A553004 Vertical Spar Pivot Fitting Lower Flange andClip Inspection (This inspection is necessary forAirplanes that have not replaced the one-piece clipwith a two-piece assembly.) Task 55-30-01-211

340

B271004 Aileron Outboard Wing Control Cable FunctionalCheck Task 27-10-00-212

512, 522,532, 612,622, 632



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B383000 Externally Serviceable Toilet Functional Check Task38-30-02-720

262



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A351005 Crew Masks and Stowage Boxes DetailedInspection Task 35-90-10-220

241, 242



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A212004 Cabin Air Distribution Check Valves DetailedInspection Task 21-22-00-210

161, 162

A251003 Crew Seats Detailed Inspection Task 25-90-10-220 241, 242

A276100 Speed Brake System Detailed Inspection Task27-61-00-210

512, 522,612, 622

A277100 Control (Gust) Lock System Operational CheckTask 27-71-00-710

151

A521006 Cabin Door Detailed Inspection Task 52-10-00-210 810

A523001 Baggage Door Detailed Inspection Task52-90-30-220

311

B213003 Cabin Altitude Pressure Switch Functional CheckTask 21-31-05-720

245

B262009 Baggage Compartment Smoke Detection SystemOperational Check Task 26-90-10-711

311, 312

B262011 Engine Fire Extinguishing System Functional CheckTask 26-90-20-720

AUX,241, 242,321


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


B262013 APU Fire Extinguishing System Functional CheckTask 26-90-20-722

AUX

B274003 Two-Position Horizontal Stabilizer Functional CheckTask 27-90-40-720

AUX

B275005 Flap System Functional Check Task 27-90-50-720 AUX

B301100 Bleed Air Anti-Ice Systems Operational Check(Airplanes -5001 thru -6000) Task 30-11-00-710

ENG

B301102 Bleed Air Anti-Ice Systems Operational Check(Airplanes -6001 and On) Task 30-11-00-711

ENG

B321000 Landing Gear System Functional Check Task32-90-10-720

AUX

B324001 Emergency Brake System Detailed Inspection Task32-90-40-221

AUX

B324011 Emergency Brake System Operational Check Task32-42-09-710

AUX

D361000 Cabin Door Particulate Trap Restoration (Cleaning)Task 36-15-00-170

261



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-09 gives a list of item(s), which are completed at the first 4A (2400 hours)or 4C (48 calendar months) whichever occurs first, and then every 2A (1200 hours) or 4C (48 calendarmonths), whichever occurs first, thereafter.






ITEM CODENUMBER


B271003 Aileron and Aileron Trim Tab Control SystemFunctional Check Task 27-90-10-721

532, 632

B272004 Rudder and Rudder Trim Control System FunctionalCheck Task 27-90-20-721

340

B273005 Elevator and the Elevator Trim Tab SystemFunctional Check Task 27-90-30-720

351, 352



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A252000 Passenger Seats Detailed Inspection Task25-90-20-220

261, 262

A281000 Fuel Storage System Detailed Inspection Task28-10-00-210

511, 512,521, 522,531, 532,611, 612,621, 622,631, 632

B284000 Low Fuel Warning System Functional Check Task28-42-00-710

AUX

B304000 Nose Compartment Overtemperature SwitchFunctional Check Task 30-40-00-710

AUX

B313002 Flight Data Recorder System Functional CheckTask 31-90-30-720

322

A324000 External Zonal Inspection of the Nose and MainLanding Gear Wheel Wells Task 32-90-40-210

710, 720,730

B350100 Passenger Oxygen System Functional Check Task35-01-00-710

AUX


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A352000 Dropout Boxes and Mask Assembly DetailedInspection Task 35-90-20-220

251, 261

A711100 Upper Cowling Camloc Hole Detailed InspectionTask 71-11-00-220

410, 420

A711101 Forward and Aft Upper Cowling Edge DetailedInspection Task 71-11-00-221

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-11 gives a list of item(s), which are completed at the first 4C (48 calendarmonths), and then every 2C (24 calendar months), thereafter.






ITEM CODENUMBER


B236000 Static Discharging System Functional Check Task23-90-60-720

331, 332,532, 540,632, 640



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-12 gives a list of MSG-3 interval 5A item(s), which are completed every3000 hours.






ITEM CODENUMBER


D217003 Ozone Converters Restoration (Cleaning) Task12-19-02-161

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description



C. Item Code A262003 was deleted in Revision 39 of this document.

D. The right portion of each page provides room for the mechanic''s and inspector''s initials and remarks.These pages may be reproduced as a checklist for use when performing this inspection phase.




ITEM CODENUMBER


D291100 Hydraulic System Filters Discard Task 29-11-04-901 313

D324010 Brake System Filters Discard Task 32-90-40-960 211



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A530004 External Zonal Inspection of the Fuselage Task53-90-00-211

110, 141,142, 153,154, 163,164, 165,166, 211,212, 221,222, 241,242, 251,252, 261,262, 311,312, 313,314, 321,322, 810,820

A530005 Internal Zonal Inspection of the Cabin Section Task53-90-00-212

151, 152,161, 162,251, 252,261, 262,810, 820

A530006 Internal Zonal Inspection of the Cockpit BelowFloorline Task 53-90-00-213

141, 142,244


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A530007 Internal Zonal Inspection of the Cockpit AboveFloorline Task 53-90-00-214

235, 241,242, 244,245, 246,247, 248

A530008 Internal Zonal Inspection of the Tail Section Task53-90-00-215

311, 312,321, 322

A530009 Internal Zonal Inspection of the Nose Section Task53-90-00-216

110, 211,212, 221,222, 710

A531001 Internal Zonal Inspection of the Empennage Task53-90-10-210

340, 351,352

A531002 External Zonal Inspection of the Empennage Task53-90-10-211

340, 351,352

A535000 Internal Zonal Inspection of the Fuselage FairingTask 53-90-50-210

151, 152,153, 154,161, 162,163, 164,165, 166,313, 314



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A570000 External Zonal Inspection of the Wings Task57-90-00-210

511, 512,521, 522,531, 532,540, 611,612, 621,622, 631,632, 641,720, 730



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-16 gives a list of MSG-3 interval item(s), which are completed every 400hours or 1C (12 calendar months), whichever occurs first.






ITEM CODENUMBER



241, 242

B561100 Windshield Surface Seal Treatment FunctionalCheck Task 56-11-00-720

241, 242



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-17 gives a list of MSG-3 interval item(s), which are completed every 500APU hours or 2C (24 calendar months), whichever occurs first.






ITEM CODENUMBER


A497000 APU Magnetic Chip Collector Detailed InspectionTask 49-90-70-220

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-18 gives a list of MSG-3 interval item(s), which are completed every 1000APU hours or 2C (24 calendar months), whichever occurs first.






ITEM CODENUMBER


D493000 APU Fuel Filter Element Discard Task 49-90-30-960 321, 322

D499000 APU Oil Filter Element Discard Task 49-90-90-960 321, 322

D499001 APU Oil Discard Task 49-90-90-961 321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date:_______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A561101 Cockpit Windshield and Side Windows DetailedInspection (Delamination) Task 56-11-00-212

241, 242

A561102 Windshield Retainer Screws Functional Check(Torque Inspection) Task 56-11-00-280

241, 242



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-23 gives a list of Inspection item(s), which are completed every 100 hoursor 12 calendar months, whichever occurs first.






ITEM CODENUMBER


B245000 Ni-Cad Battery (Saft) Functional Check (CapacityCheck) The inspection interval can be adjustedafter the water loss per cell is established. Refer tothe Battery Service Table. Task 24-90-50-721

321, 322

B245001 Ni-Cad Battery (Marathon) Functional Check(Capacity Check) The inspection interval canbe adjusted after the water loss per cell isestablished. Refer to the Battery Service Table.Task 24-90-50-722

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date:_______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-24 gives a list of item(s), which are completed every 150 hours.



D. Inspection item(s) were removed from this Inspection Document. For more details, refer to theIntroduction, Inspection Program Change Summary.




ITEM CODENUMBER


A761103 Fuel Control Unit (FCU) Throttle Lever CutoffFunctional Check (Airplanes -5001 thru -5196 NotIncorporating SB560XL-76-03) Task 76-10-00-620

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


A761104 Fuel Control Unit (FCU) Throttle Lever CutoffFunctional Check (Airplanes -5197 thru -6000,and Airplanes -5001 thru -5196 IncorporatingSB560XL-76-03) Task 76-10-00-620

410, 420

C783001 Thrust Reverser Lubrication (WC-393 Non-AerosolSpray Lubrication Method) Task 78-31-00-640

410, 420

C783002 Thrust Reverser Guide Rods Lubrication(D-5100NS Aerosol Spray Lubrication Method)Task 78-31-00-641

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-26 gives a list of item(s), which are completed every 500 APU hours.






ITEM CODENUMBER


A801103 APU Starter Generator Detailed Inspection Task80-90-11-220

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


C783003 Lubrication of the Thrust Reverser Pivot Points(C-5A Antiseize Compound Lubrication Method)Task 78-31-00-642

410, 420



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-30 gives a list of Inspection item(s), which are completed every 1000 APUhours in accordance with (IAW) the manufacturer's instructions.






ITEM CODENUMBER


A494000 APU Igniter Plug Detailed Inspection Task49-90-40-220

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-34 gives a list of Inspection item(s), which are completed every 6 calendarmonths in accordance with (IAW) the manufacturer's instructions.






ITEM CODENUMBER


B342006 L3 Com Standby Battery Pack Operational Check(Periodic Check) Task 34-90-20-710

211

B342007 Securaplane Standby Battery Operational Check(Energy Level) Task 34-20-00-763

211



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B243002 Saft Ni-Cad Battery Restoration (Deep Cycle) Task24-90-50-840

313

B342005 L3 Com Standby Battery Pack Functional Check(Capacity Check) Task 34-20-00-762

211



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description







ITEM CODENUMBER


B237006 Cockpit Voice Recorder Underwater LocatingDevice (ULD) Functional Check Task 23-90-70-720

AUX

B313003 Flight Data Recorder Underwater Locating Device(ULD) Functional Check Task 31-90-30-721

312



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-38 gives a list of Inspection item(s), which are completed every 5 years inaccordance with (IAW) the manufacturer's instructions.






ITEM CODENUMBER


B262014 Optional Aft Vanity Fire Extinguisher BottleFunctional Check (Weight Check)Task26-90-20-723

261, 262



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-40 gives a list of Inspection item(s), which are completed at the first 2400hours or 72 calendar months whichever occurs first, then every 1200 hours or 36 calendar monthswhichever occurs first thereafter.






ITEM CODENUMBER


A533003 Fuselage External Surface Special DetailedInspection (Eddy Current) Task 53-30-01-250

141, 142,151, 152,161, 162,241, 242,251, 252,261, 262



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-43 gives a list of Inspection item(s), which are completed in accordancewith (IAW) the manufacturer's instructions.






ITEM CODENUMBER


A324006 Landing Gear Wheels Special Detailed Inspection(NDI). Refer to the Goodrich ComponentMaintenance Manual 32-45-48, Main LandingGear Wheel Assembly, Part Number 3-1571and Goodrich Component Maintenance Manual32-47-42, Nose Landing Gear Wheel Assembly,Part Number 3-1418. Task 32-90-40-280

710, 720,730



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-44 gives a list of required 14 CFR 91.207 item(s), which are completedevery 12 calendar months. These items do not have a grace period.






ITEM CODENUMBER


B256006 Emergency Locator Transmitter System FunctionalCheck (Artex ELT 110-4) (Required by 14 CFR91.207) Task 25-90-60-710

BAT

A256012 Emergency Locator Transmitter System DetailedInspection (Artex ELT 110-4) (Required by 14 CFR91.207) Task 25-90-60-225

BAT

A256104 Artex C406-2 Emergency Locator Inspection(Required by 14 CFR 91.207) Task 25-61-04-210

BAT

B256104 Artex C406-2 Emergency Locator Functional Test(Required by 14 CFR 91.207) Task 25-61-04-720

BAT

A256105 Artex C406-N Emergency Locator Inspection(Required by 14 CFR 91.207) Task 25-61-05-210

BAT

B256105 Artex C406-N Emergency Locator Functional Test(Required by 14 CFR 91.207) Task 25-61-05-720

BAT


CESSNA®MODEL 560XL

MAINTENANCE MANUAL

ITEM CODENUMBER


A256106 Artex 110-406 Emergency Locator Inspection Task25-61-06-210

BAT

B256106 Artex 110-406 Emergency Locator Functional TestTask 25-61-06-720

BAT



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-45 gives a list of required 14 CFR 91.411, 91.413 and RVSM certificationitem(s), which are completed every 24 calendar months. These items do not have a grace period.






ITEM CODENUMBER


B238002 Transponder Functional Check (Airplanes -5001thru -6000) (Required by 14 CFR 91.413) Task23-90-20-720

AUX

B341100 Pitot-Static System Functional Check (Airplanes-5001 thru -6000) Required 14 CFR 91.411, 91.413and RVSM certification Task 34-90-10-210

AUX

B341200 Pitot-Static System Functional Test (Airplanes-6001 and On) Required 14 CFR 91.411, 91.413and RVSM certification Task 34-90-12-210

AUX

B345307 Transponder System Functional Check (Airplanes-6001 and On) (Required by 14 CFR 91.413) Task34-53-07-720

AUX



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-47 gives a list of Inspection item(s) which are completed at the first 600hours or 12 calendar months whichever occurs first, then each 200 hours or 3 calendar months,whichever occurs first thereafter.






ITEM CODENUMBER


B243001 Lead-Acid Battery Functional Check (CapacityCheck) NOTE: The inspection schedule may beadjusted after the useful battery life is established,based on operations. Task 24-90-50-720

313



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-48 gives a list of Inspection item(s) which are completed every 500 hours.






ITEM CODENUMBER


B238000 Standby Nav/Com Control Unit Operational Check(Airplanes -5001 thru -6000) Task 23-80-01-710

AUX



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-50 gives a list of inspection item(s), which are completed every 6 calendarmonths (for airplanes that operate in moderate or severe corrosion environments. Refer to Chapter51, Corrosion Severity Maps - Description and Operation).






ITEM CODENUMBER



710, 720,730


710

A551004 Horizontal Stabilizer Aft Spar Area GeneralVisual Inspection (Corrosion Inspection). Task55-10-01-212

351, 352


340


512, 522,532, 612,622, 632


512, 612



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-51 gives a list of Inspection item(s), which are completed every 500compressor hours on the vapor cycle cooling system.






ITEM CODENUMBER


A215209 Vapor Cycle Cooling System 500 Compressor-HourMaintenance Task 21-52-00-211

321, 322



CESSNA®MODEL 560XL

MAINTENANCE MANUAL


Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-52 gives a list of Inspection item(s), which are completed at the first 6000hours, then every 1200 hours thereafter.






ITEM CODENUMBER


A553019 Vertical Stabilizer Internal Inspection Task55-30-01-212

340



CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MB

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MB gives a list of Inspection item(s), which are completed at the first 3000hours, then every 1500 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A712201 Aft Engine Beam Inspection (Chapter 4Requirement) NOTE: This engine support structureinspection is for Airplanes -5001 thru -5060. Task71-22-00-210

311, 312,411, 412

*** End of Inspection Document MB InspectionItems ***

5-92-MB Page 1© TEXTRON AVIATION INC. Oct 1/2011

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MD

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MD gives a list of Inspection item(s), which are completed at the first 6000hours or ten years whichever occurs first, then every 2400 hours or ten years whichever occurs firstthereafter. This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOTbe exceeded.






ITEM CODENUMBER


A531021 Forward Pressure Bulkhead Inspection (Chapter 4Requirement) Task 53-10-11-251

221, 222

*** End of Inspection Document MD InspectionItems ***

5-92-MD Page 1© TEXTRON AVIATION INC. Apr 1/2013

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT ME

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-ME gives a list of Inspection item(s), which are completed every 15,000hours. This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.






ITEM CODENUMBER


A521007 Cabin Door Detailed Inspection (Chapter 4requirement) Task 52-10-00-210

810

A522003 Emergency Exit Door Detailed Inspection (Chapter4 requirement) Task 52-20-00-210

820

A531014 Aft Pressure Bulkhead Inspection (Chapter 4Requirement) Task 53-10-11-252

311, 312

A533005 Upper Skin Splice at BL 0.00 (Chapter 4requirement) Task 53-30-01-251

251, 252,261, 262

A533007 Lower Skin Splice at Stringer 13 (Chapter 4requirement) Task 53-30-01-252

141, 142,151, 152,161, 162

A533009 Lower Skin from Right Stringer 13 to Left Stringer13 (Chapter 4 requirement) Task 53-30-01-210

141, 142,151, 152,161, 162,321, 322

*** End of Inspection Document ME InspectionItems ***

5-92-ME Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MF

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MF gives a list of Inspection item(s), which are completed at the first 7500hours, then every 1400 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571001 Lower Wing Main Spar Lower Skin Splice at WS22.50 (Chapter 4 requirement) Task 57-10-00-250

511, 512,611, 612

A571003 Lower Wing Main Spar Lower Skin Splice at WS22.50 (Chapter 4 requirement) Task 57-10-00-270

511, 512,611, 612

*** End of Inspection Document MF InspectionItems ***

5-92-MF Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MG

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MG gives a list of Inspection item(s), which are completed at the first 6500hours, then every 3000 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553008 Vertical Stabilizer Rear Spar Cap at WL146.00 (Airplanes -5001 thru -5020) (Chapter 4requirement) Task 55-30-01-250

340

*** End of Inspection Document MG InspectionItems ***

5-92-MG Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MH

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MH gives a list of Inspection item(s), which are completed at the first 11,000hours, then every 6000 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553009 Vertical Stabilizer Rear Spar Nested Angle at WL146.00 (Airplanes -5001 thru -5020) (Chapter 4requirement) Task 55-30-01-251

340

*** End of Inspection Document MH InspectionItems ***

5-92-MH Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MI

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MI gives a list of Inspection item(s), which are completed at the first 5000hours, then every 2500 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A553010 Vertical Stabilizer Rear Spar Strap at WL146.00 (Airplanes -5001 thru -5020) (Chapter 4requirement) Task 55-30-01-252

340

*** End of Inspection Document MI Inspection Items***

5-92-MI Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MJ

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MJ gives a list of Inspection item(s), which are completed every 13,000hours. This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT beexceeded.






ITEM CODENUMBER


A533011 Upper Skin from Right Stringer 13 to Left Stringer13 (Chapter 4 requirement) Task 53-30-01-210

241, 242,251, 252,261, 262,311, 312,321, 322

A545000 Forward Engine Beam, Upper Angles, HorizontalCap Flange at BL 30.5 to BL 42.0 Special DetailedInspection (Eddy Current) Task 54-50-10-250

311, 312,411, 412

*** End of Inspection Document MJ InspectionItems ***

5-92-MJ Page 1© TEXTRON AVIATION INC. Oct 1/2011

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MK

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MK gives a list of Inspection item(s), which are completed at the first 11,500hours, then every 9000 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER



321, 322

*** End of Inspection Document MK InspectionItems ***

5-92-MK Page 1© TEXTRON AVIATION INC. Oct 1/2010

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT ML

Date:_______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-ML gives a list of Inspection item(s), which are completed at the first 11,500hours, then every 3300 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571005 Lower Wing Main Spar Skin Splice Flange at WS11.50 (Chapter 4 requirement) Task 57-10-00-251

511, 512,611, 612

A571007 Lower Wing Main Spar and Skin Splice at WS 11.50(Chapter 4 requirement) Task 57-10-00-271

511, 512,611, 612

*** End of Inspection Document ML InspectionItems ***

5-92-ML Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MM

Date:_______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MM gives a list of Inspection item(s), which are completed at the first 11,000hours, then every 4200 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A571009 Lower Wing Main Spar at WS 114.57 (Chapter 4requirement) Task 57-10-00-252

521, 522,621, 622

*** End of Inspection Document MM InspectionItems ***

5-92-MM Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MN

Date:_______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MN gives a list of Inspection item(s), which are completed at the first 9000hours, then every 3400 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER



521, 522,621, 622

*** End of Inspection Document MN InspectionItems ***

5-92-MN Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MO

Date:_______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MO gives a list of Inspection item(s), which are completed at the first 12,500hours, then every 6100 hours thereafter. This inspection is a Chapter 4 requirement, and as such,the interval limitation CANNOT be exceeded.






ITEM CODENUMBER



521, 522,621, 622

*** End of Inspection Document MO InspectionItems ***

5-92-MO Page 1© TEXTRON AVIATION INC. Apr 1/2009

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MP

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MP gives a list of Inspection item(s), which are completed every 300 hours.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A215206 Vapor Cycle Cooling System Hour Meter Check.Task 21-52-00-210

332

*** End of Inspection Document MP InspectionItems ***

5-92-MP Page 1© TEXTRON AVIATION INC. Jul 1/2012

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MQ

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MQ gives a list of Inspection item(s), which are completed every 170 hours.This inspection is a Chapter 4 requirement, and as such, the interval limitation CANNOT be exceeded.






ITEM CODENUMBER


A761600 Time Limited Dispatch Operational Check(Airplanes -6001 and On) Task 76-16-00-710

235

*** End of Inspection Document MQ InspectionItems ***

5-92-MQ Page 1© TEXTRON AVIATION INC. Jul 1/2012

CESSNA®MODEL 560XL

MAINTENANCE MANUAL

INSPECTION DOCUMENT MR

Date: _______________



Total Time: _______________

1. Description

A. Inspection Document 5-92-MR gives a list of Inspection item(s), which are completed at the first 10,000hours and every 5000 hours thereafter. This inspection is a Chapter 4 requirement, and as such, theinterval limitation CANNOT be exceeded.






ITEM CODENUMBER



340

*** End of Inspection Document MR InspectionItems ***

5-92-MR Page 1© TEXTRON AVIATION INC. Apr 1/2013

Citation SERVICELETTER REASON - Cessna

Documents

Transcript of Citation SERVICELETTER REASON - Cessna