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C AIRCRAFT MAINTENANCE MANUAL

TIME LIMITS/MAINTENANCE CHECKSLIST OF EFFECTIVE PAGES

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TIME LIMITS/MAINTENANCE CHECKS 05−00−00

Description and Operation 1

Effectivity: ON A/C ALL

General

SERVICE AND ROUTINE CHECKS 05−20−00

Inspection/Check 601


General

Service Check

Routine Check 605

ZONAL INSPECTIONS 05−21−00



GeneralInternal Zonal Inspection

External Zonal Inspection 603

Internal Inspection 605

External Inspection 607

General Visual Inspection for a

System/Powerplant

609

Zonal Inspection 611

Structural Inspection 612

UNSCHEDULED MAINTENANCE CHECKS 05−50−00

Description and Operation 1


General


TIME LIMITS/MAINTENANCE CHECKSTABLE OF CONTENTS

Subject

Chapter

SectionSubject Page


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HARD/OVERWEIGHT LANDING 05−51−01



General

Visual Inspection for Hard/Overweight Landing

INTEGRATED DRIVE GENERATOR (IDG)

DISCONNECTS WITH ENGINE RUNNING

05−51−02



General

EXTREME TURBULENCE OR MANEUVER 05−51−03



General

Visual Inspection for Extreme Turbulence or

Maneuver Damage

OVERSPEED CONDITION 05−51−04



General

Visual Inspection of the Flaps and the Landing

Gear for Overspeed Damage

LIGHTNING STRIKE AND STATIC DISCHARGE 05−

51−

05



Introduction

Visual En−Route Inspection for Lightning Strike

Damage

602


Subject

ChapterSectionSubject Page


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Detailed Check for Lightning Strike Damage 606

Detailed Inspection After a Lightning Strike to the

Nose

625


Nose when the Nose Landing Gear was not

Retracted

660


Wingtip

663


Vertical or Horizontal Stabilizer

673

Detailed Inspection After a Lightning Strike when

the EICAS gives Continuous Indications

678

VOLCANIC ASH CONTAMINATION 05−51−06



General

Inspection after Volcanic Ash Contamination

ENGINE 05−51−07



General

AUXILIARY POWER UNIT (APU) SURGES −

INSPECTION/CHECK

05−51−08



General


Subject



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AIR DRIVEN GENERATOR (ADG) DEPLOYMENT 05−51−19

Inspection/Check


General

Inspection Check After ADG Deployment

BIRD STRIKE CONDITION 05−51−25



General

Visual Inspection After a Bird Strike

HIGH ENERGY STOP/REJECTED TAKEOFF (RTO) 05−51−27



General

Visual Inspection for High Energy Stop (HES) or

Rejected Take−Off (RTO) Damage

TIRE BURST 05−51−29



General

Inspection Check of Aircraft for Tire Burst Damage

ENGINE DRIVEN PUMP (EDP) OPERATED DRY

AFTER HYDRAULIC FLUID LOSS

05−51−33



General

Inspection of Engine Driven Pump (EDP) after dry

operation due to hydraulic fluid loss


Subject



05−

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EMERGENCY/INADVERTENT DEPLOYMENT OF

PASSENGER OXYGEN MASKS −

INSPECTION/CHECK

05−51−35

Inspection/Check


General

Inspection Check After the Deployment of the

Passenger Oxygen System

AILERON WING PULLEYS 05−

51−

36



General

Inspection of the Aileron Wing Pulleys

Subsequent To An Aileron Binding Occurrence

OVERWEIGHT JACKING 05−51−39



General

Inspection of the Aircraft after Overweight Jacking

at the Structural Jacking Points


Subject



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**ON A/C ALL

TIME LIMITS/MAINTENANCE CHECKS − DESCRIPTION AND OPERATION

1. General

A. Section 5−

10−

00, Time Limits, and Section 5−

20−

00, Scheduled Maintenance Checks,are found in the Maintenance Requirements Manual (MRM), Document No.CSP− A−053. Part 1, Section 2 of the MRM contains the complete CL600−2B19Maintenance Review Board Report (MRBR) and is the only source of information for theRegional Jet Scheduled Maintenance Program.

B. Section 5−50−00 includes data of the unscheduled maintenance inspection/checkswhich are done when an aircraft was operated in unusual conditions.


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**ON A/C ALL

SERVICE AND ROUTINE − INSPECTION/CHECK

1. General

A. The tasks that follow are for the service and routine scheduled maintenance checks.These checks follow the order of a walk−around style check. These checks are made upof maintenance review board requirements found in the Maintenance RequirementsManual, CSP A−053.

TASK 05−20−00−200−801Service Check

1. Reason for the Job

Refer to MRB F12−20−00−01, MRB 26−21−01−03, MRB 28−11−00−01, MRB 28−11−00−05,MRB 28−12−00−01, MRB 32−40−00−01, MRB 32−40−00−03, MRB 32−40−00−05, MRB32−43−26−01, MRB 79−11−01−03, and MRB 79−12−00−01.

2. Job Set−Up Information

Subtask 05−20−00−946−001

A. Reference Information

REFERENCE DESIGNATION

TASK 12−00−07−861−801 Connect External AC Power

TASK 12−00−07−861−802 Remove External AC Power

TASK 12−11−28−750−802 Water Contamination Test

TASK 12−12−32−610−806 Tire Pressure Inspection

TASK 12−13−79−612−802 Service Engine Oil from Replenishment Tank

TASK 12−

21−

00−

110−

803 Cleaning of the Aircraft Windows

TASK 28−12−01−710−801 Operational Test of the Main Tank Relief Valve

TASK 32−10−00−210−801 Visual Inspection of the Main Landing Gear andDoor

TASK 28−12−02−710−801 Operational Test of the Center−Tank Relief Valve

TASK 32−20−00−210−801 Visual Inspection of the Nose Landing Gear andDoors

TASK 32−41−01−210−801 Visual Inspection of the Main Tire − RetreadableGoodyear Tires

TASK 32−41−01−210−802 Visual Inspection of the Main Tire −Non−Retreadable Michelin Tires

TASK 32−

41−

01−

210−

803 Visual Inspection of the Main Tire−

RetreadableMichelin Tires

TASK 32−42−01−210−801 Visual Inspection of the Nose Tire −Non−Retreadable Michelin Tires

TASK 32−42−01−210−802 Visual Inspection of the Nose Tire − RetreadableMichelin Tires

TASK 57−41−01−110−801 Cleaning of the Wing Leading Edges



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3. Job Set−Up

Subtask 05−20−00−010−001

A. Open the access door that follows:

ACCESS DESIGNATION311BB Aft equipment compartment door

4. Procedure

Subtask 05−20−00−890−001

A. Clean the windshields (Ref. TASK 12−21−00−110−803).

B. Do a visual check of the nose landing gear, doors and wheel assemblies for condition,leakage and safety of installation(Ref. TASK 32−20−00−210−801).

C. Examine the nose wheel tires for correct tread depth wear and damage (Ref. TASK

32−

42−

01−

210−

801 or TASK 32−

42−

01−

210−

802, as applicable).NOTE: The maximum tread wear allowed is to the bottom of the tread.

D. Measure the tire pressure of the nose landing gear and service as necessary (Ref. TASK 12−12−32−610−806).

E. Do a visual check of the left main landing gear wheel assemblies for condition, leakageand safety of installation(Ref. TASK 32−10−00−210−801).

F. Examine the left main wheel tires for correct tread depth, wear and damage (Ref. TASK 32−41−01−210−801 or TASK 32−41−01−210−802 or TASK 32−41−01−210−803, asapplicable).

NOTE: The maximum tread wear allowed is to the bottom of the tread.

G. Measure the tire pressure of the left main landing gear and service as necessary (Ref.

TASK 12−

12−

32−

610−

806).H. Clean the left wing leading edge of foreign objects (Ref. TASK 57−41−01−110−801).

I. Do a check of all water drain valves. Examine the fuel in the left wing and center fueltanks for contamination (Ref. TASK 12−11−28−750−802).

J. Examine the fuel access panels and the fuel drain valves (left and center fuel tanks).

K. Do an operational test of the fuel tank relief valves (left and center fuel tanks) as follows:

(1) Pull the T Handle down to unseat the relief valve and return the handle to reseat thevalve.

(2) Make sure that the valve opens and closes easily.

(Ref. TASK 28−12−01−710−801 and TASK 28−12−02−710−801).

L. Service the oil replenishment tank (Ref. TASK 12−

13−

79−

612−

802).M. Do an operational test of the fuel tank relief valves (right fuel tank) as follows:

(1) Pull the T Handle down to unseat the relief valve and return the handle to reseat thevalve.

(2) Make sure that the valve opens and closes easily.

(Ref. TASK 28−12−01−710−801).



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N. Examine the fuel access panels and the fuel drain valves (right fuel tank).

O. Do a check of all water drain valves. Examine the fuel for contamination (right fuel tank)(Ref. TASK 12−11−28−750−802).

P. Clean the right wing leading edge of foreign objects (Ref. TASK 57−41−01−110−801).

Q. Do a visual check of the left main landing gear wheel assemblies for condition, leakageand safety of installation (Ref. TASK 32−10−00−210−801).

R. Examine the right main wheel tires for correct tread depth, wear and damage (Ref. TASK 32−41−01−210−801 or TASK 32−41−01−210−802 or TASK 32−41−01−210−803, asapplicable).

NOTE: The maximum tread wear allowed is to the bottom of the tread.

S. Measure the tire pressure of the right main landing gear and service as necessary (Ref.TASK 12−12−32−610−806).

T. Connect external AC power (Ref. TASK 12−00−07−861−801).

U. Do the operational test of the LH ENG FIRE PUSH switch/light and the RH ENG FIREPUSH switch/light as follows:

(1) On the FIRE DETECTION panel installed in the overhead instrument panel, set theswitches that follow to BOTH:

± LH ENG

± LH JET

± RH ENG

± RH JET

± APU.

(2) Set and hold the TEST switch to WARN.

(3) Make sure that the results that follow occur:

± The LH ENG FIRE PUSH switch/light comes on in red± The RH ENG FIRE PUSH switch/light comes on in red.

(4) On the FIRE DETECTION panel, release the TEST switch.


± The LH ENG FIRE PUSH switch/light goes off

± The RH ENG FIRE PUSH switch/light goes off.

(6) Push the LH ENG FIRE PUSH switch/light.


± The BOTTLE 1 ARMED PUSH TO DISCH switch/light comes on in green


± On the primary engine indication and crew alerting system (EICAS) display(ED 1), make sure that the L ENG SOV CLSD indication is shown in amber

± On the secondary EICAS display (ED 2) status page, make sure that theHYD SOV 1 CLSD indication is shown in green.

(8) Push the LH ENG FIRE PUSH switch/light again.


± The BOTTLE 1 ARMED PUSH TO DISCH switch/light goes off



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± On ED 1, make sure that the L ENG SOV CLSD indication is not shown

± On ED 2 status page, make sure that the HYD SOV 1 CLSD indication is notshown.

(10) Push the RH ENG FIRE PUSH switch/light.




± On the primary engine indication and crew alerting system (EICAS) display(ED 1), make sure that the R ENG SOV CLSD indication is shown in amber

± On the secondary EICAS display (ED 2) status page, make sure that theHYD SOV 2 CLSD indication is shown in green.

(12) Push the RH ENG FIRE PUSH switch/light again.




± On ED 1, make sure that the R ENG SOV CLSD indication is not shown

± On ED 2 status page, make sure that the HYD SOV 2 CLSD indication is notshown.

V. Remove external AC power (Ref. TASK 12−00−07−861−802).

5. Close Out

Subtask 05−20−00−941−001

A. Remove all tools, equipment, and unwanted materials from the work area.

Subtask 05−20−00−410−001

B. Close the access door that follows:

ACCESS DESIGNATION

311BB Aft equipment compartment door



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TASK 05−20−00−200−802Routine Check


Refer to MRB 25−61−02−01, CMR C26−20−131−03, CMR C26−20−131−02, CMR

C27−

40−

113−

01, CMR C28−

00−

142−

01, CMR C30−

10−

141−

02, MRB 25−

61−

03−

01, MRB27−35−01−01, MRB 32−43−16−01, MRB 32−00−00−09, MRB 32−43−06−01, MRB 72−21−00−09,MRB 29−11−11−01, MRB 29−12−11−01, MRB 21−51−13−01, MRB 32−00−00−04, and MRB26−21−01−03.


Subtask 05−20−00−944−001

A. Consumable Materials


02−002 Hydraulic fluid, petroleum base

05−001 Cloths, cleaning, low−lint

Subtask 05−20−00−946−002

B. Reference Information


TASK 12−12−29−614−802 Replenish the Accumulators of the HydraulicSystems

TASK 12−20−32−640−807 Lubrication of the Shock Strut and Trailing Arm of the MLG

TASK 21−51−13−220−801 Detailed Inspection of the Air Cycle Machine (ACM)Oil Level

TASK 25−

61−

00−

220−

801 Detailed Inspection of the First Aid and Medical KitSeals

TASK 25−61−00−710−801 Operational Test of the Flashlights

TASK 26−11−00−710−801 Operational Test of the EngineFire/Overheat−Detection System

TASK 26−12−00−710−801 Operational Test of the APU Fire−DetectionSystem

TASK 26−21−01−710−801 Operational Test of the LH ENG FIRE PUSHSwitch/Light and the RH ENG FIRE PUSHSwitch/Light

TASK 26−22−00−710−801 Operational Test of the APU Fire−Extinguishing

SystemTASK 27−35−00−220−801 Detailed Inspection of the Angle−of − Attack Vanes

TASK 27−40−00−710−801 Operational Test of the Horizontal Stabilizer TrimSystem

TASK 28−13−00−710−801 Operational Test of the Fuel Manual−CrossflowSystem

TASK 30−11−00−740−801 Self −Test of the Anti Ice Duct System



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TASK 32−43−00−210−801 General Visual Inspection of the Brake SystemHydraulic Lines and Components

TASK 53−83−01−000−801 Remove MLG wheel bins

TASK 53−

83−

01−

400−

801 Install MLG wheel bins

TASK 79−21−13−210−801 Visual Inspection of the Engine Oil−DetectionPanel

3. Job Set−Up

Subtask 05−20−00−010−002

A. Open the access panels that follow:

ACCESS DESIGNATION

311AL Ground air supply connection door


311BZ APU compartment access panel

B. Remove the main landing gear wheel bins (Ref. TASK 53−83−01−000−801).

4. Procedure

Subtask 05−20−00−890−002

A. Do a detailed inspection of the first aid and medical kit seals (Ref. TASK 25−61−00−220−801).

B. Do a check of the flashlights (Ref. TASK 25−61−00−710−801).

C. Do a check of the LH ENG FIRE PUSH switch/light (Ref. TASK 26−

21−

01−

710−

801).

D. Do a check of the RH ENG FIRE PUSH switch/light (Ref. TASK 26−21−01−710−801).

E. Do a check of the Engine fire/oveheat−detection system (Ref. TASK 26−11−00−710−801).

F. Do a detailed inspection of the air cycle machine (ACM) oil leve(Ref. TASK 21−51−13−220−801).

G. Do a check of the APU fire−detection system (Ref. TASK 26−12−00−710−801).

H. Do a check of the APU fire−extinguishing system (Ref. TASK 26−22−00−710−801).

I. Do a check of the horizontal stabilizer trim system (Ref. TASK 27−40−00−710−801).

J. Do a check of the fuel manual−crossflow system (Ref. TASK 28−13−00−710−801).

K. Do a self −test of the anti−ice duct system (Ref. TASK 30−11−00−740−801).

L. Do a check of the AOA vanes for freedom of movement (Ref. TASK 27−35−00−220−801) and ensure drain holes are clear.

M. Do a check of all the hydraulic lines and components in the nose hydraulic compartmentfor condition, leakage and safety of installation (Ref. TASK 32−43−00−210−801).

N. Do a detailed inspection of the nose landing gear shock strut for leakage, security andcondition.



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O. Clean the nose landing gear piston with a 05−001 clean cloth moistened with 02−002hydraulic fluid (MIL−H−5606) and rub with a 05−001 clean dry cloth.

P. Do a check of the No. 2 and 3 hydraulic system brake accumulator and service asnecessary (Ref. TASK 12−12−29−614−802).

Q. Do a detailed inspection of the left main landing gear shock strut for leakage, securityand condition.

R. Clean the left landing gear piston with a 05−001 clean cloth moistened with 02−002hydraulic fluid (MIL−H−5606) and rub with a 05−001 clean dry cloth.

S. Lubricate the left landing gear shock strut and the left trailing arm (Ref. TASK 12−20−32−640−807).

T. Do a visual check of the engine oil−detection panel (Ref. TASK 79−21−13−210−801).

U. Do a visual check of the nitrogen charge of the No. 1 and 2 hydraulic systemaccumulators and service as necessary (Ref. TASK 12−12−29−614−802).

V. Do a visual inspection for the conditions of the items that follow:

± Cables

± Wires

± APU and related components

± Fay sealant

± Upper and lower titanium ducts

± Bellows

± Structure.

W. Do a detailed inspection of the right main landing gear shock strut for leakage, securityand condition.

X. Clean the right landing gear piston with a 05−001 clean cloth moistened with 02−002hydraulic fluid (MIL−H−5606) and rub with a 05−001 clean dry cloth.

Y. Lubricate the right landing gear shock strut and the right trailing arm (Ref. TASK 12−20−32−640−807).

Z. Do a visual check of the nitrogen charge of the No. 3 hydraulic system accumulators andservice as necessary (Ref. TASK 12−12−29−614−802).

Subtask 05−20−00−941−002

AA. Remove all tools, equipment, and unwanted materials from the work area.

Subtask 05−20−00−410−002

AB. Close the access panels that follow:

ACCESS DESIGNATION

311AL Ground air supply connection door


311BZ APU compartment access panel

AC. Install the main landing gear wheel bins (Ref. TASK 53−83−01−400−801).



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**ON A/C ALL

SCHEDULED MAINTENANCE INSPECTION REQUIREMENTS − INSPECTION/CHECK

1. General

A. The definitions and procedures that follow identify the intent of the types of inspectionthat follow:

± General Visual Inspection for the Systems/Powerplant (Maintenance Review Board(MRB) Task)

± Zonal Inspection (MRB Task)

± Structural Inspection (MRB Task).

B. The applicable task card will identify the steps and/or specifics that are required for eachscheduled inspection.

TASK 05−21−00−210−801

Internal Zonal Inspection1. Reason for the Job

A. All of the internal zonal inspections are given in the Maintenance Requirements Manual.The task card will give the specific area to be inspected.


Subtask 05−21−00−943−001

A. Tools and Equipment


None Specified Flashlight

None Specified Hand tools (as necessary)None Specified Work stands (as necessary)

Subtask 05−21−00−010−001

B. Where applicable, access to a specified zone is given on the task card.

3. Job Set−Up

Subtask 05−21−00−010−002

A. Where applicable, refer to the task card to remove or open access panels, fairings, ordoors.



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4. Procedure

Subtask 05−21−00−210−001

A. Do an internal zonal inspection of the zone that is specified on the task card as follows:

(1) Examine the area for cleanliness.(2) If the surfaces of the components have a protective coating (paint, alodine, etc.),

examine the protective coating condition for signs of damage.

(3) Examine the condition of all related fasteners for signs of corrosion or failure.

(4) Examine all of the electrical wires, connectors, and harness runs in the zone forcondition and safety of installation.

(5) Examine all of the hydraulic, oil, and fuel lines, and the pneumatic lines and ductsfor signs of leakage, condition, and safety of installation.

(6) Look for signs that water or contaminants have gone into the zone, or signs that(items in) the zone have become too hot.

(7) Examine the operation of the drain ports and cleanliness of drain holes.

(8) Examine all the access panels, fairings and doors used for access.

(9) Make sure that there are no unwanted objects in the work area.

5. Close Out

Subtask 05−21−00−410−001

A. Where applicable, install or close the access panels, fairings, or doors.

Subtask 05−21−00−941−001

B. Remove all tools, equipment, and unwanted materials from the work area.



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**ON A/C 7011−7014, 7017−7018, 7022, 7026−7027, 7031, 7035, 7037−7038, 7040, 7042−7044,7046, 7048, 7050, 7080, 7091−7092, 7100, 7105, 7109, 7111, 7116−7117, 7123, 7127, 7129,7131−7132, 7134, 7141, 7145−7146, 7150−7151, 7157−7159, 7163, 7168−7169, 7171, 7174,7199, 7204, 7215−7216, 7229−7230, 7235, 7238, 7241, 7244−7245, 7250, 7253, 7259, 7265,7267, 7273, 7306, 7312, 7315, 7319, 7326, 7333, 7338, 7344, 7348, 7352, 7354, 7359, 7364,

7366, 7370, 7380−

7381, 7387, 7397, 7408, 7415, 7420, 7427−

7428, 7440−

7441, 7451,7460−7461, 7472−7473, 7482, 7539, 7546, 7552, 7562, 7592, 7612−7613, 7627, 7637,7649−7650, 7655, 7667−7668, 7670−7671, 7675, 7689, 7702, 7707, 7729−7730, 7755−7756,7763, 7765, 7774, 7791−7793, 7796, 7802, 7809, 7816, 7821, 7824, 7841

TASK 05−21−00−210−802External Zonal Inspection


A. All of the external zonal inspections are given in the Maintenance Requirements Manual.The task card will give the specific area to be inspected.


Subtask 05−

21−

00−

943−

002 A. Tools and Equipment



None Specified Hand tools (as necessary)

None Specified Work stands (as necessary)

Subtask 05−21−00−010−003

B. Where applicable, access to a specified zone is given on the task card.

3. Job Set−Up

Subtask 05−21−00−010−004


4. Procedure

Subtask 05−21−00−210−002

A. Do an external zonal inspection of the zone that is specified on the task card as follows:

(1) Examine the area for cleanliness.(2) If the surfaces of the components have a protective coating (paint, alodine, etc.),

examine the protective coating condition for signs of damage.


(4) Examine all of the electrical wires, connectors, and harness runs in the zone forcondition and safety of installation.



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(6) Look for items in the zone that show signs that they have become too hot.

(7) Examine the operation of the drain ports and cleanliness of drain holes.

(8) Examine all the access panels, fairings and doors used for access.


5. Close Out

Subtask 05−21−00−410−002


Subtask 05−21−00−941−002




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TASK 05−21−00−210−803Internal Inspection


A. Where applicable, all of the internal inspections are given in the Maintenance

Requirements Manual. The task card will give the specific area or component that has tobe inspected.


Subtask 05−21−00−943−003






Subtask 05−21−00−010−005

B. Where applicable, access to a specified area or component is given on the task card.

3. Job Set−Up

Subtask 05−21−00−010−006


4. Procedure

Subtask 05−21−00−210−003

A. Do an internal inspection of the specified area as follows:

(1) If the surfaces of the components have a protective coating (paint, alodine, etc.),examine the protective coating condition for signs of damage.


(3) Examine all of the electrical wires, connectors, and harness runs for condition andsafety of installation.





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5. Close Out

Subtask 05−21−00−410−003


Subtask 05−

21−

00−

943−

004




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TASK 05−21−00−210−804External Inspection


A. Where applicable, all of the external inspections are given in the Maintenance

Requirements Manual. The task card will give the specific area or component that has tobe inspected.


Subtask 05−21−00−943−005






Subtask 05−21−00−010−007

B. Where applicable, access to a specified area or component is given on the task card.

3. Job Set−Up

Subtask 05−21−00−010−008


4. Procedure

Subtask 05−21−00−210−004

A. Do an external inspection of the specified area as follows:

(1) If the surfaces of the components have a protective coating (paint, alodine, etc.),examine the protective coating condition for signs of damage.


(3) Examine all of the electrical wires, connectors, and harness runs for condition andsafety of installation.





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5. Close Out

Subtask 05−21−00−410−004


Subtask 05−

21−

00−

943−

006




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**ON A/C ALL

TASK 05−21−00−210−805General Visual Inspection for a System/Powerplant


A. All general visual inspections are identified in the Maintenance Requirements Manual.The Maintenance Requirements Board (MRB) task card will give the specific equipmentto be inspected.


Subtask 05−21−00−943−008






Subtask 05−21−00−010−009

B. Where applicable, access to the specified equipment is given with the task cards.

3. Job Set−Up

Subtask 05−21−00−010−010

A. Where applicable, refer to the task cards for removal or open of access panels, fairings,or doors.

4. Procedure

Subtask 05−21−00−210−005

A. The definition of a general visual inspection for a systems/powerplant MRB Task is asfollows:

(1) A visual examination that will detect obvious unsatisfactoryconditions/discrepancies. This type of inspection may require cleaning, removal of fillets, fairings, access panels/doors, etc. Workstands, ladders, etc., may berequired to gain proximity.

5. Close Out

Subtask 05−21−00−410−005

A. Where applicable, install or close the access panels, fairings, or doors as shown on thetask cards.



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Subtask 05−21−00−941−003




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TASK 05−21−00−210−806Zonal Inspection


A. All zonal inspections are identified in the Maintenance Requirements Manual. The

Maintenance Requirements Board (MRB) task card will give the specific area to beinspected.


Subtask 05−21−00−943−009






Subtask 05−21−00−010−011

B. Where applicable, access to the specified area is given with the task cards.

3. Job Set−Up

Subtask 05−21−00−010−012


4. Procedure

Subtask 05−21−00−210−006

A. The definition of a zonal inspection is as follows:

(1) The entire visible contents of the zone must be inspected for obvious damage,chafing, dents, security of installation of pulleys, wiring ducting, tubing, etc., andgeneral condition including corrosion or leaks. Zonal inspections will be conductedwithin touching distance, unless otherwise stated.

5. Close Out

Subtask 05−21−00−410−006

A. Where applicable, install or close the access panels, fairings, or doors as shown on taskcards.

Subtask 05−21−00−943−010




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TASK 05−21−00−220−801Structural Inspection


A. All structural inspections are identified in the Maintenance Requirements Manual. The

Maintenance Requirements Board (MRB) task card will give the specific area to beinspected.


Subtask 05−21−00−943−011






Subtask 05−21−00−010−013

B. Where applicable, access to the specified structure is given with the task cards.

3. Job Set−Up

Subtask 05−21−00−010−014


4. Procedure

Subtask 05−21−00−210−007

A. The definition of a structural inspection is as follows:

(1) An intensive visual examination of a specified structure. It searches for evidence of irregularity using adequate lighting and, where necessary, inspection aids such asmirrors, hand lens, etc. Surface cleaning and elaborate access procedures may berequired.

5. Close Out

Subtask 05−21−00−410−007

A. Where applicable, install or close the access panels, fairings, or doors as shown on taskcards.

Subtask 05−21−00−943−012




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**ON A/C ALL

UNSCHEDULED MAINTENANCE CHECKS − DESCRIPTION AND OPERATION

1. General

A. This section includes the data on the unscheduled maintenance checks that must bedone when an aircraft is operated, or when servicing is done, in unusual conditions. Forsome conditions there is more than one task. The data is given in the sections thatfollow:

± Hard/Overweight Landing − Inspection/Check (Ref. AMM 05−51−01)

± Integrated Drive Generator (IDG) Disconnects with Engine Running −Inspection/Check (Ref. AMM 05−51−02)

± Severe Turbulence − Inspection/Check (Ref. AMM 05−51−03)

± Overspeed Condition − Inspection/Check (Ref. AMM 05−51−04)

± Lightning Strike − Inspection/Check (Ref. AMM 05−51−05)

± Volcanic Ash Contamination −

Inspection/Check (Ref. AMM 05−

51−

06)± Engine − Inspection/Check (Ref. AMM 05−51−07).

± Auxiliary Power Unit (APU) Surges − Inspection/Check (Ref. AMM 05−51−08)

± Air Driven Generator (ADG) Deployment − Inspection/Check (Ref. AMM 05−51−19)

± Bird Strike Condition − Inspection/Check (Ref. AMM 05−51−25)

± High Energy Stop (HES)/Rejected Takeoff (RTO) − Inspection/Check (Ref. AMM 05−51−27)

± Tire Burst − Inspection/Check (Ref. AMM 05−51−29)

± Engine Driven Pump (EDP) Operated Dry After Hydraulic Fluid Loss −Inspection/Check (Ref. AMM 05−51−33).

± Emergency/Accidental Deployment of the Passenger Oxygen System−

Inspection/Check (Ref. AMM 05−51−35)

± Aileron Wing Pulleys − Inspection/Check (Ref. AMM 05−51−36)

± Overweight Jacking − Inspection/Check (Ref. AMM 05−51−39).



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**ON A/C ALL

HARD/OVERWEIGHT LANDING − INSPECTION/CHECK

1. General

A. The maintenance procedure that follows is for the visual inspection of the aircraft after ahard or overweight landing. The visual inspection is used to make sure that the aircraft isserviceable after a hard or overweight landing.

TASK 05−51−01−210−801 Visual Inspection for Hard/Overweight Landing

NOTE: At this time there is no accurate procedure to calculate the vertical speed of the aircraftwhen it touches the runway. You must do this inspection if the pilot makes a report thatthe aircraft made a hard or overweight landing.

1. Definitions

A. The Maximum Landing Weight (MLW) is the maximum weight (pounds/kilograms)

approved for the landing touchdown.

B. The Maximum Take−off Weight (MTOW) is the maximum weight (pounds/kilograms)approved for the start of take−off.

C. An Overweight Landing is defined as a landing at more than MLW.

D. A Hard Landing is defined as follows:

± A landing at a vertical descent rate greater than 600 ft/min (feet per minute) when thegross weight of the aircraft is less than or equal to MLW

± A landing at a vertical descent rate greater than 360 ft/min when the gross weight of the aircraft is greater than MLW, but less than or equal to MTOW.



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**ON A/C 7004−7019, 7021−7031, 7034−7051, 7054−7056, 7058, 7060, 7062, 7064−7067, 7069,7071−7075, 7077−7080, 7082−7083, 7086−7087, 7089−7093, 7095−7102, 7104−7105, 7107,7109, 7111−7124, 7127−7132, 7134−7135, 7137−7139, 7141, 7145−7146, 7149−7161, 7163,

7165, 7168−

7169, 7171−

7175, 7178−

7181, 7185−

7189, 7191−

7196, 7198−

7204, 7206−

7218,7220, 7225, 7228−7241, 7243−7246, 7250−7251, 7253−7261, 7263−7271, 7273−7295,7297−7300, 7302−7315, 7317−7319, 7322, 7324−7331, 7333−7342, 7344−7349, 7351−7364,7366−7370, 7372, 7374, 7376, 7379−7383, 7385, 7387−7388, 7390, 7392−7393, 7395−7402,7404−7406, 7408−7429, 7432−7435, 7437−7438, 7440−7448, 7450−7463, 7465, 7467−7477,7479, 7481−7485, 7487−7492, 7495−7498, 7500−7507, 7509−7513, 7515−7528, 7530−7546,7548−7562, 7564, 7566, 7568−7569, 7571−7572, 7574−7582, 7584−7590, 7592−7604, 7606,7608−7618, 7620−7621, 7623, 7626−7628, 7631−7660, 7662−7672, 7675, 7677−7682,7684−7685, 7687, 7689−7695, 7697, 7699, 7701−7704, 7707−7708, 7711−7717, 7719−7720,7722−7731, 7733−7737, 7739−7744, 7748−7750, 7752−7757, 7759−7774, 7776−7783,7786−7789, 7791−7796, 7798−7806, 7809−7827, 7829−7835, 7837−7838, 7840−7845,7848−7850, 7852−7854, 7856−7861, 7863, 7865, 7867−7868, 7870−7876, 7878−7883, 7885,7887, 7889−7893, 7895, 7897−7900, 7904, 7906, 7909, 7911−7913, 7916−7917, 7919−7920,

7922, 7925−

7927, 7929, 7931, 7934−

7939, 7941, 7945, 7947, 7949, 7951−

7959, 7961−

7963,7966−7967, 7978−7979, 7983, 7985, 7987−7988, 7990, 8002−8004, 8006−8007, 8009−8011,8014−8018, 8022, 8028, 8037−8038, 8042−8043, 8050, 8058−8059, 8061−8063 and ON A/C7033, 7052, 7136, 7140, 7176, 7224, 7227, 7242, 7320, 7350, 7478, 7486, 7494, 7508, 7565,7622, 7624−7625, 7629 Pre SB601R−25−164

Subtask 05−51−01−946−001

A. Reference Information


TASK 07−12−01−582−801 Jacking of the Main Landing Gear

TASK 07−12−03−582−801 Jacking of the Nose Landing Gear

TASK 10−11−01−587−801 Parking

TASK 12−00−06−863−801 Pressurize Hydraulic Systems No. 1 and No. 2

TASK 12−00−06−863−802 Release Hydraulic Pressure − Systems No. 1 andNo. 2

TASK 12−00−06−863−803 Pressurize Hydraulic System No. 3

TASK 12−00−06−863−804 Release Hydraulic Pressure − System No. 3


TASK 24−00−00−910−801 Electrical/Electronic Safety Precautions

TASK 24−32−01−210−801 Visual Inspection of the Main Battery

TASK 24−32−02−210−801 Visual Inspection of the APU Battery

TASK 25−

62−

00−

710−

801 Operational Test of the Artex 2−

Frequency ELTSystem

TASK 26−21−07−210−801 Visual Inspection of the Engine Fire−ExtinguisherContainer Pressure−Gauge

TASK 26−25−01−210−801 Visual Check of the Cargo Fire−ExtinguisherContainer Pressure−Gauge

TASK 27−11−00−710−801 Operational Test of the Aileron Control System



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TASK 27−13−00−710−801 Operational Test of the Aileron Disconnect System

TASK 27−21−00−710−801 Operational Test of the Rudder Control System

TASK 27−31−00−710−801 Operational Test of the Elevator Control System

TASK 27−31−00−710−802 Operational Test of the Pitch Feel System

TASK 27−40−00−720−801 Functional Test of the Horizontal Stabilizer TrimSystem

TASK 27−54−00−710−801 Operational Test of the Flaps

TASK 27−64−00−710−801 Operational Test of the Flight Spoiler/Spoileron



TASK 32−41−01−210−801 Visual Inspection of the Main Wheel/Tire Assembly − Retreadable Goodyear Tires

TASK 32−41−01−210−802 Visual Inspection of the Main Wheel/Tire Assembly − Non−retreadable Michelin Tires

TASK 32−42−01−210−801 Visual Inspection of the Nosewheel/Tire Assembly− Retreadable Goodyear Tires

TASK 32−42−01−210−802 Visual Inspection of the Nosewheel/Tire Assembly− Non−retreadable Michelin Tires

TASK 32−43−26−210−801 Visual Inspection of the Wear Pin Indicator

TASK 53−82−01−000−801 Removal of the Forward Fairing Access−Panel

TASK 53−82−01−000−802 Removal of the Right Forward Wing−to−FuselageFairing

TASK 53−82−01−000−803 Removal of the Left Forward Wing−to−FuselageFairing

TASK 53−82−01−000−804 Removal of the Wing−to−Fuselage Side Panels

TASK 53−82−01−000−805 Removal of the Forward Side Fairings

TASK 53−82−01−000−806 Removal of the Center Side Fairings

TASK 53−82−01−000−807 Removal of the Rear Side Fairings

TASK 53−82−01−000−808 Removal of the Flap Stub Fairings

TASK 53−82−01−000−809 Removal of the Right Outboard−Panel WingFairing

TASK 53−82−01−000−810 Removal of the Left Outboard−Panel Wing Fairing

TASK 53−82−01−000−811 Removal of the Aft−Panel Wing Fairing

TASK 53−

82−

01−

000−

812 Removal of the Center−

Panel Wing FairingTASK 53−82−01−400−801 Installation of the Forward−Fairing Access Panel

TASK 53−82−01−400−802 Installation of the Right ForwardWing−to−Fuselage Fairing

TASK 53−82−01−400−803 Installation of the Left Forward Wing−to−FuselageFairing

TASK 53−82−01−400−804 Installation of the Wing−to−Fuselage Side Panels



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TASK 53−82−01−400−805 Installation of the Forward Side Fairings

TASK 53−82−01−400−806 Installation of the Center Side Fairings

TASK 53−82−01−400−807 Installation of the Rear Side Fairings

TASK 53−82−01−400−808 Installation of the Flap Stub Fairings

TASK 53−82−01−400−809 Installation of the Right Outboard−Panel WingFairing

TASK 53−82−01−400−810 Installation of the Left Outboard−Panel wingFairing

TASK 53−82−01−400−811 Installation of the Aft−Panel Wing Fairing

TASK 53−82−01−400−812 Installation of the Center−Panel Wing Fairing

TASK 53−83−01−000−801 Removal of the MLG Wheel Bin

TASK 53−83−01−400−801 Installation of the MLG Wheel Bin

**ON A/C 7003, 7020, 7053, 7057, 7070, 7076, 7081, 7084−

7085, 7088, 7106, 7108, 7126,7143−7144, 7147, 7162, 7164, 7177, 7182−7184, 7190, 7197, 7219, 7221−7223, 7226,7247−7248, 7262, 7296, 7301, 7316, 7321, 7323, 7332, 7365, 7371, 7373, 7375, 7377−7378,7386, 7389, 7391, 7394, 7403, 7407, 7431, 7436, 7439, 7449, 7464, 7480, 7499, 7567, 7570,7573, 7583, 7605, 7607, 7619, 7630, 7738, 7846, 7862, 7864, 7901−7902, 7910

Subtask 05−51−01−946−002

B. Reference Information




TASK 10−

11−

01−

587−

801 Parking






TASK 24−00−00−910−801 Electrical/Electronic Safety Precautions

TASK 24−32−01−210−801 Visual Inspection of the Main Battery


TASK 25−

62−

00−

710−

802 Operational Test of the Socata ELT 96 SystemTASK 26−21−07−210−801 Visual Inspection of the Engine Fire−Extinguisher

Container Pressure−Gauge



TASK 27−13−00−710−801 Operational Test of the Aileron Disconnect System



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TASK 32−41−01−210−802 Visual Inspection of the Main Wheel/Tire Assembly

− Non

−retreadable Michelin Tires







TASK 53−

82−

01−

000−

804 Removal of the Wing−

to−

Fuselage Side Panels





TASK 53−82−01−000−809 Removal of the Right Outboard−Panel WingFairing

TASK 53−82−01−000−810 Removal of the Left Outboard−Panel Wing Fairing


TASK 53−82−01−000−812 Removal of the Center−Panel Wing Fairing

TASK 53−

82−

01−

400−

801 Installation of the Forward−

Fairing Access PanelTASK 53−82−01−400−802 Installation of the Right Forward

Wing−to−Fuselage Fairing



TASK 53−82−01−400−805 Installation of the Forward Side Fairings



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TASK 53−83−01−000−801 Removal of the MLG Wheel Bin

TASK 53−83−01−400−801 Installation of the MLG Wheel Bin

**ON A/C 7032, 7059, 7061, 7063, 7094, 7103, 7110, 7125, 7133, 7142, 7148, 7166−7167, 7170,7205, 7249, 7252, 7272, 7343, 7384, 7430, 7466, 7493, 7514, 7529, 7547, 7563, 7591, 7661,7673

−7674, 7676, 7683, 7686, 7688, 7696, 7698, 7700, 7705

−7706, 7709

−7710, 7718, 7721,

7732, 7745−7747, 7751, 7758, 7775, 7784−7785, 7790, 7797, 7807−7808, 7828, 7836, 7839,7847, 7851, 7855, 7866, 7869, 7877, 7884, 7886, 7888, 7894, 7896, 7903, 7905, 7907−7908,7914−7915, 7918, 7921, 7923−7924, 7928, 7930, 7932−7933, 7940, 7942−7944, 7946, 7948,7950, 7960, 7964−7965, 7968−7977, 7980−7982, 7984, 7986, 7989, 8000−8001, 8005, 8008,8012−8013, 8019−8021, 8023−8027, 8029−8036, 8039−8041, 8044−8049, 8051−8057, 8060,8064, 8066−8068 and ON A/C 7033, 7052, 7136, 7140, 7176, 7224, 7227, 7242, 7320, 7350,7478, 7486, 7494, 7508, 7565, 7622, 7624−7625, 7629 Post SB601R−25−164

Subtask 05−51−01−946−003

C. Reference Information




TASK 10−11−01−587−801 Parking






TASK 24−

00−

00−

910−

801 Electrical/Electronic Safety PrecautionsTASK 24−32−01−210−801 Visual Inspection of the Main Battery


TASK 25−62−00−710−803 Operational Test of the Artex 3−Frequency ELTSystem

TASK 26−21−07−210−801 Visual Inspection of the Engine Fire−ExtinguisherContainer Pressure−Gauge



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TASK 27−

13−

00−

710−

801 Operational Test of the Aileron Disconnect System








TASK 32−

20−

00−

210−

801 Visual Inspection of the Nose Landing Gear andDoors


TASK 32−41−01−210−802 Visual Inspection of the Main Wheel/Tire Assembly − Non−retreadable Michelin Tires







TASK 53−82−01−000−804 Removal of the Wing−to−Fuselage Side Panels





TASK 53−82−01−000−809 Removal of the Right Outboard−Panel Wing

FairingTASK 53−82−01−000−810 Removal of the Left Outboard−Panel Wing Fairing


TASK 53−82−01−000−812 Removal of the Center−Panel Wing Fairing

TASK 53−82−01−400−801 Installation of the Forward−Fairing Access Panel

TASK 53−82−01−400−802 Installation of the Right ForwardWing−to−Fuselage Fairing



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TASK 53−

82−

01−

400−

805 Installation of the Forward Side Fairings








TASK 53−

83−

01−

000−

801 Removal of the MLG Wheel BinTASK 53−83−01−400−801 Installation of the MLG Wheel Bin

**ON A/C ALL

3. Job Set−Up

Subtask 05−51−01−941−001

WARNING: PUT THE SAFETY DEVICES, THE WARNING SIGNS, AND THE WARNINGPLACARDS IN POSITION BEFORE YOU START A PROCEDURE ON ORNEAR:

± FLIGHT CONTROLS

± FLIGHT CONTROL SURFACES

± COMPONENTS THAT MOVE.

MAKE SURE THAT THERE ARE NO PERSONS OR EQUIPMENT ON ORNEAR THE FLIGHT CONTROL SURFACES. ACCIDENTAL MOVEMENT OFTHE FLIGHT CONTROLS CAN CAUSE INJURIES TO PERSONS AND/ORDAMAGE TO EQUIPMENT.

A. Put the safety devices and the warning signs in the applicable positions.

B. Install the applicable warning tags on the pilot’s and copilot’s control columns.

Subtask 05−51−01−910−001

C. Park the aircraft (Ref. TASK 10−

11−

01−

587−

801).WARNING: OBEY ALL THE SAFETY PRECAUTIONS WHEN YOU DO MAINTENANCE

ON OR NEAR ELECTRICAL/ELECTRONIC EQUIPMENT. IF YOU DO NOTDO THIS, YOU CAN CAUSE INJURIES TO PERSONS AND/OR DAMAGETO THE EQUIPMENT.

D. Obey all the electrical safety precautions (Ref. TASK 24−00−00−910−801).



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Subtask 05−51−01−010−001

E. Open the access panels during the inspection/check as necessary.

4. ProcedureSubtask 05−51−01−210−001

A. Do a visual inspection of the wings as follows:

(1) Examine the web of the wing rear spar for damage, distortion in the skin panels,and pulled fasteners.

(2) Examine the winglets for damage.

(3) Examine the leading edge of the wing for distortion in the panels.

(4) Examine the wing upper surface above the MLG attachment points for distortion.

(5) Examine the skin panel of the upper wing, adjacent to the wing/fuselage attachmentfittings, for distortion or pulled fasteners.

(6) Examine the leading−

edge wing−

to−

fuselage fairing for displacement, access doordistortion, damaged fastener holes, and skin cracks.

(7) Examine the lower wing−to−fuselage structure for distortion, cracks in the skin, ordamaged paint.

(8) Examine the wings for hydraulic fluid leakage.

(9) Examine the wings for fuel leakage.

Subtask 05−51−01−210−002

B. Do a visual inspection of the engines as follows:

(1) Examine the nacelles of the engines for signs of damage, cracks and pulledfasteners.

(2) Examine the pylons for signs of paint damage, cracks and pulled fasteners.

Subtask 05−51−01−210−003

C. If paint damage is found, open the access panels to the engine pylons and do a visualinspection of each component as follows:

(1) Examine the pylon for cracks or distortion.

(2) Examine the pylon to aircraft beam attachments for cracks.

(3) Look for torn or damaged fasteners.

(4) Examine the inner structure for paint damage.

(5) Examine the pylon for cracks.

(6) Examine the pipes and the ducts for leakage.

(7) Examine the bleed air ducts for distortion.



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Subtask 05−51−01−210−004

D. Do a visual inspection of the outer surfaces of the aircraft fuselage as follows:

(1) Examine the fuselage skin panels for damage, distortion or pulled fasteners.

(2) Examine the bottom side of the fuselage for signs of damage or distortion of thefuselage skin panels.

(3) Examine the fuselage splices for distortion of the aircraft skin or damage to thepaint finish.

(4) Examine the fuselage for hydraulic fluid leakage.

(5) Examine the fuselage for fuel leakage.

(6) Examine the passenger door, open and closed, for distortion.

(7) Examine the service door, open and closed, for distortion.

(8) Examine the left and right emergency exits for distortion.

(9) Examine all of the access panels and the compartment doors.

(10) If external damage is found to the fuselage, continue as follows:(a) Open the access panels, as necessary, to examine the aircraft internally.

(b) Look for cracks or distortion of the stringers, the fittings, and the componentmounts.

(c) Look for hydraulic fluid leakage.

(d) Look for fuel leakage.

Subtask 05−51−01−210−006

E. Examine the floor structure of the flight compartment, the attachment fittings of the pilotand copilot seats, the overhead console and the pilot and copilot instrument panels forthe conditions that follow:

± Distortion

± Damage to the paint finish

± Pulled fasteners.

Subtask 05−51−01−210−008

F. Do a visual check of the cargo fire−extinguisher container for the pressure gauge (Ref.TASK 26−25−01−210−801).

Subtask 05−51−01−210−009

G. Do a visual inspection of the auxiliary power unit (APU) as follows:

(1) Examine all of the external pipes and ducts for damage or leakage.(2) Remove the access door of the APU.

(3) Look for torn fasteners.

(4) Bulkhead FS755.00 for distortion, damage and cracks.



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Subtask 05−51−01−210−010

H. Do a visual inspection of the main battery (Ref. TASK 24−32−01−210−801).

Subtask 05−51−01−210−011

I. Do a visual inspection of the APU battery (Ref. TASK 24−

32−

02−

210−

801).

Subtask 05−51−01−210−012

J. Do a visual inspection of the engine fire−extinguisher container for the pressure gauge(Ref. TASK 26−21−07−210−801).

K. Do a visual inspection of the APU fire−extinguisher container for the pressure gauge.

Subtask 05−51−01−210−018

L. Lift the nose landing gear (NLG) clear of the ground (Ref. TASK 07−12−03−582−801)and do the steps that follow:

(1) Do a visual inspection of the NLG and doors (Ref. TASK 32−20−00−210−801).

(2) Do a visual inspection of the NLG attachment points.

(3) Do a visual inspection of the NLG wheel condition.

(4) Do an inspection of the NLG tires (Ref. TASK 32−42−01−210−801) (Forretreadable Michelin tires Ref. TASK 32−42−01−210−802).

(5) Do a visual inspection of all components of the gear.

(6) Do a visual inspection of the wheel well for distortion and damage.

M. Repair or replace the components that you find damaged.

N. Lower the nose landing gear to the ground (Ref. TASK 07−12−03−582−801).

Subtask 05−51−01−210−019

O. Lift the main landing gear (MLG) clear of the ground (Ref. TASK 07−12−01−582−801)and do the steps that follow:

(1) Do a visual inspection of the MLG and doors (Ref. TASK 32−10−00−210−801).

(2) Examine the MLG wheels for cracks or other damage.

(3) Turn the MLG wheels. Make sure that they move freely.

(4) Remove the MLG wheel bin (Ref. TASK 53−83−01−000−801).

(5) Examine the wheel bin for damage.

(6) Do a visual inspection of the main wheel/tire assembly (For retreadable Goodyeartires Ref. TASK 32−41−01−210−801) (For non−retreadable Michelin tires Ref.TASK 32−41−01−210−802).

(7) Do a visual inspection of the MLG attachment points.

(8) Install the MLG wheel bin (Ref. TASK 53−83−01−400−801).

P. If damage to the tires or wheels is found, do the steps that follow:

(1) Do a visual inspection of the wear pin indicator (Ref. TASK 32−43−26−210−801).

(2) Examine the upper and lower ends of the MLG shock strut for leakage of fluid.



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(3) Examine the MLG struts and linkage for distortion, cracks, or other damage.

(4) Examine the MLG trailing arm, stay actuator and fittings for distortion, damage orcracks.

(5) Examine the outboard end fuse−pins of the MLG beam for distortion.

Q. Lower the MLG to the ground (Ref. TASK 07−

12−

03−

582−

801).

Subtask 05−51−01−220−002

R. If damage is found during the external wing inspection, do a detailed inspection of thewings as follows:

(1) Remove, as necessary, the access panels and fairings that follow:

± Forward−fairing access panel (Ref. TASK 53−82−01−000−801)

± Right forward wing−to−fuselage fairing (Ref. TASK 53−82−01−000−802)

± Left forward wing−to−fuselage fairing (Ref. TASK 53−82−01−000−803)

± Wing−to−fuselage side panels (Ref. TASK 53−82−01−000−804)

± Forward side fairings (Ref. TASK 53−

82−

01−

000−

805)± Center side fairings (Ref. TASK 53−82−01−000−806)

± Rear side fairings (Ref. TASK 53−82−01−000−807)

± Flap stub fairings (Ref. TASK 53−82−01−000−808)

± Right outboard panel wing−fairing (Ref. TASK 53−82−01−000−809)

± Left outboard panel wing−fairing (Ref. TASK 53−82−01−000−810)

± Aft panel wing−fairing (Ref. TASK 53−82−01−000−811)

± Center panel wing−fairing (Ref. TASK 53−82−01−000−812).

(2) Examine the left and right wing−to−fuselage joints for distortion, cracks, and pulledfasteners.

(3) Examine the wheel well bulkheads for distortion, paint damage, cracks, and pulledfasteners.

(4) Examine the upper fuselage structure above the primary wing spars and MLGwheel−well bulkheads for the conditions that follow:

± Metal distortion

± Paint damage

± Cracks

± Pulled fasteners

± Fasteners that are not there.

(5) Examine the area below the floor beams aft of the wing center section for paint

damage or distortion.

(6) Examine the rear spar for distortion between the end of the fuel tank and the side of the fuselage.



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Subtask 05−51−01−410−001

S. Install the access panels and fairings.

(1) Install, as necessary, the access panels and fairings that follow:

±Forward

−

fairing access panel (Ref. TASK 53−

82−

01−

400−

801)± Right forward wing−to−fuselage fairing (Ref. TASK 53−82−01−400−802)

± Left forward wing−to−fuselage fairing (Ref. TASK 53−82−01−400−803)

± Wing−to−fuselage side panels (Ref. TASK 53−82−01−400−804)

± Forward side fairings (Ref. TASK 53−82−01−400−805)

± Center side fairings (Ref. TASK 53−82−01−400−806)

± Rear side fairings (Ref. TASK 53−82−01−400−807)

± Flap stub fairings (Ref. TASK 53−82−01−400−808)

± Right outboard panel wing−fairing (Ref. TASK 53−82−01−400−809)

± Left outboard panel wing−fairings (Ref. TASK 53−82−01−400−810)

± Aft panel wing−

fairing (Ref. TASK 53−

82−

01−

400−

811)

± Center panel wing−fairing (Ref. TASK 53−82−01−400−812).

Subtask 05−51−01−220−004

T. Do a detailed inspection of the horizontal stabilizer as follows:

(1) Examine the leading edge for damage to the skin.

(2) Examine the skin panels of the upper and lower horizontal stabilizer for distortion.

Subtask 05−51−01−220−005

U. Do a detailed inspection of the vertical stabilizer as follows:

(1) Examine the fasteners for damage.(2) Examine the leading edge for damage to the skin.

(3) Examine the skin panels of the vertical stabilizer for distortion.

Subtask 05−51−01−863−001

V. Pressurize hydraulic systems No. 1 and No. 2 (Ref. TASK 12−00−06−863−801).

W. Pressurize hydraulic system No. 3 (Ref. TASK 12−00−06−863−803).

X. Look for hydraulic fluid leaks.

Subtask 05−51−01−710−001

Y. Do an operational test of the flaps (Ref. TASK 27−

54−

00−

710−

801).

Subtask 05−51−01−710−002

Z. Do an operational test of the flight spoiler/spoileron (Ref. TASK 27−64−00−710−801).



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Subtask 05−51−01−710−003

AA. Do an operational test of the elevator control system (Ref. TASK 27−31−00−710−801).

Subtask 05−51−01−710−004

AB. Do an operational test of the rudder control system (Ref. TASK 27−

21−

00−

710−

801).

Subtask 05−51−01−720−001

AC. Do an operational test of the horizontal stabilizer trim system (Ref.TASK 27−40−00−710−801).

Subtask 05−51−01−710−006

AD. Do an operational test of the aileron control system (Ref. TASK 27−11−00−710−801).

AE. Do an operational test of the aileron disconnect system (Ref.TASK 27−13−00−710−801).

Subtask 05−

51−

01−

710−

007

AF. Do an operational test of the pitch feel system (Ref. TASK 27−31−00−710−802).

**ON A/C 7004−7019, 7021−7031, 7034−7051, 7054−7056, 7058, 7060, 7062, 7064−7067, 7069,7071−7075, 7077−7080, 7082−7083, 7086−7087, 7089−7093, 7095−7102, 7104−7105, 7107,7109, 7111−7124, 7127−7132, 7134−7135, 7137−7139, 7141, 7145−7146, 7149−7161, 7163,7165, 7168−7169, 7171−7175, 7178−7181, 7185−7189, 7191−7196, 7198−7204, 7206−7218,7220, 7225, 7228−7241, 7243−7246, 7250−7251, 7253−7261, 7263−7271, 7273−7295,7297−7300, 7302−7315, 7317−7319, 7322, 7324−7331, 7333−7342, 7344−7349, 7351−7364,7366−7370, 7372, 7374, 7376, 7379−7383, 7385, 7387−7388, 7390, 7392−7393, 7395−7402,7404−7406, 7408−7429, 7432−7435, 7437−7438, 7440−7448, 7450−7463, 7465, 7467−7477,7479, 7481−7485, 7487−7492, 7495−7498, 7500−7507, 7509−7513, 7515−7528, 7530−7546,

7548−

7562, 7564, 7566, 7568−

7569, 7571−

7572, 7574−

7582, 7584−

7590, 7592−

7604, 7606,7608−7618, 7620−7621, 7623, 7626−7628, 7631−7660, 7662−7672, 7675, 7677−7682,7684−7685, 7687, 7689−7695, 7697, 7699, 7701−7704, 7707−7708, 7711−7717, 7719−7720,7722−7731, 7733−7737, 7739−7744, 7748−7750, 7752−7757, 7759−7774, 7776−7783,7786−7789, 7791−7796, 7798−7806, 7809−7827, 7829−7835, 7837−7838, 7840−7845,7848−7850, 7852−7854, 7856−7861, 7863, 7865, 7867−7868, 7870−7876, 7878−7883, 7885,7887, 7889−7893, 7895, 7897−7900, 7904, 7906, 7909, 7911−7913, 7916−7917, 7919−7920,7922, 7925−7927, 7929, 7931, 7934−7939, 7941, 7945, 7947, 7949, 7951−7959, 7961−7963,7966−7967, 7978−7979, 7983, 7985, 7987−7988, 7990, 8002−8004, 8006−8007, 8009−8011,8014−8018, 8022, 8028, 8037−8038, 8042−8043, 8050, 8058−8059, 8061−8063 and ON A/C7033, 7052, 7136, 7140, 7176, 7224, 7227, 7242, 7320, 7350, 7478, 7486, 7494, 7508, 7565,7622, 7624−7625, 7629 Pre SB601R−25−164

Subtask 05−

51−

01−

720−

002

AG. Do an operational test of the Artex 2−frequency ELT system (Ref.TASK 25−62−00−710−801).



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**ON A/C 7003, 7020, 7053, 7057, 7070, 7076, 7081, 7084−7085, 7088, 7106, 7108, 7126,7143−7144, 7147, 7162, 7164, 7177, 7182−7184, 7190, 7197, 7219, 7221−7223, 7226,7247−7248, 7262, 7296, 7301, 7316, 7321, 7323, 7332, 7365, 7371, 7373, 7375, 7377−7378,7386, 7389, 7391, 7394, 7403, 7407, 7431, 7436, 7439, 7449, 7464, 7480, 7499, 7567, 7570,7573, 7583, 7605, 7607, 7619, 7630, 7738, 7846, 7862, 7864, 7901−7902, 7910

Subtask 05−51−01−720−003

AH. Do an operational test of the Socata ELT 96 (Ref. TASK 25−62−00−710−802).

**ON A/C 7032, 7059, 7061, 7063, 7094, 7103, 7110, 7125, 7133, 7142, 7148, 7166−7167, 7170,7205, 7249, 7252, 7272, 7343, 7384, 7430, 7466, 7493, 7514, 7529, 7547, 7563, 7591, 7661,7673−7674, 7676, 7683, 7686, 7688, 7696, 7698, 7700, 7705−7706, 7709−7710, 7718, 7721,7732, 7745−7747, 7751, 7758, 7775, 7784−7785, 7790, 7797, 7807−7808, 7828, 7836, 7839,7847, 7851, 7855, 7866, 7869, 7877, 7884, 7886, 7888, 7894, 7896, 7903, 7905, 7907−7908,7914−7915, 7918, 7921, 7923−7924, 7928, 7930, 7932−7933, 7940, 7942−7944, 7946, 7948,7950, 7960, 7964−7965, 7968−7977, 7980−7982, 7984, 7986, 7989, 8000−8001, 8005, 8008,8012−8013, 8019−8021, 8023−8027, 8029−8036, 8039−8041, 8044−8049, 8051−8057, 8060,

8064, 8066−

8068 and ON A/C 7033, 7052, 7136, 7140, 7176, 7224, 7227, 7242, 7320, 7350,7478, 7486, 7494, 7508, 7565, 7622, 7624−7625, 7629 Post SB601R−25−164

Subtask 05−51−01−720−004

AI. Do an operational test of the Artex 3−frequency ELT system (Ref.TASK 25−62−00−710−803).

**ON A/C ALL

5. Close Out

Subtask 05−51−01−863−002

A. Release the hydraulic pressure from systems No. 1 and No. 2 (Ref.TASK 12−00−06−863−802).

B. Release the hydraulic pressure from system No. 3 (Ref. TASK 12−00−06−863−804).

Subtask 05−51−01−861−001

C. Remove the external ac power (Ref. TASK 12−00−07−861−802).

Subtask 05−51−01−941−002

D. Remove the applicable warning tags from the pilot and copilot rudder pedals.

E. Remove the safety devices and the warning signs from the applicable positions.

Subtask 05−51−01−941−003

F. Remove all tools, equipment, and unwanted materials from the work area.



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**ON A/C ALL

INTEGRATED DRIVE GENERATOR (IDG) DISCONNECTS WITH ENGINE RUNNING −INSPECTION/CHECK

1. General A. The time that an engine is operated with the integrated drive generator (IDG)

disconnected must be recorded in the aircraft logbook. The logged time is permitted toadd up to 30 hours. Replace the IDG if the logged time is more than this limit (Ref. TASK 24−11−01−000−801 and TASK 24−11−01−400−801).



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**ON A/C ALL

EXTREME TURBULENCE − INSPECTION/CHECK

1. General

A. The procedure that follows is for the inspection of an ai

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