LHD Logbook

Basic Maintenance Experience Logbook

For EASA Part 66 license

Part 66 Basic Experience Requirements

Icelandic Civil Aviation Administration Page 1 of 35 Issue 1 29.04.2013

General:This document has been developed by Icelandic Civil Aviation Administration to assist applicant to comply with Commissionregulation (EC) No 2042/2003 by record his/her basic practical maintenance experience.

Objective:Before applying for initial Part-66 aircraft maintenance licence (AML) or additional category or sub-categories to existent licenceapplicant shall have acquired basic practical maintenance experience in relevant category or sub-categories.

The practical experience shall involve a representative cross section of maintenance tasks on aircraft. Applicant shall have gaineda detailed knowledge of the practical aspects and capacity to combine and apply the separate elements of knowledge in a logicaland comprehensive manner. The applicant should be able to:- Read and understand manufacturer instructions- Use tools and equipment as required in manufacturer instructions- Use and have knowledge of various material, both raw and consumable, and standard parts- Use his knowledge in a practical manner and use manufacturer instructions- Interpret results from various sources and measurements and apply corrective action where appropriate- Demonstrate knowledge of good maintenance standards and human factor limitation.

This document is based on ATA 100 specification principle as a way for applicant to demonstrate how he/she satisfy theserequirements.

Responsibility:It is the responsibility of the applicant to document correctly his/her practical maintenance experience. Each task shall besupervised and signed by qualified certifying or support staff.



Introduction:Tasks required to log depend on what category AML is sought. Thus, the applicant has to select tasks relevant to a category or sub-categories. For example tasks required for category B2 rating needs to be more in depth related to ATA chapter 22, 23, 24, 27, 31,34, 42, 44 and 46 than in other chapters while applicant seeking subcategory B1.3 rating needs to demonstrate work in ATAchapters 60-67 along with other chapters.

Maintenance tasks which are considered as A, B1 and B3 are:- Maintenance tasks performed on aircraft structure, power plant and mechanical and electrical systems- Work on avionics systems requiring only simple tests to prove their serviceability and not requiring troubleshooting.

Maintenance tasks which are considered as B2 are:- Maintenance tasks performed on avionic and electrical systems- Electrical and avionics tasks within power plant and mechanical systems, requiring only simple tests to prove their

serviceability

GM 66.A.20(a) provides information about definitions for maintenance task related to Electrical system, Avionics system,Simple test, Troubleshooting, Line maintenance and Base maintenance.

Basic experience requirements duration:- Implementing rule 66.A.30 provides information about basic experience requirements duration applicant needs to demon-

strate when applying for initial AML.- Appendix IV to Part 66 Implementing rule provides information about experience requirements duration applicant needs to

demonstrate when applying for extension to existing Part-66 AML with new category or sub-categories.

This logbook is constructed in a way to guide applicant to gain minimum relevant basic practical maintenance experience that rep-resent a cross section of maintenance activities. It is obvious that each applicant will perform more work in some ATA chapters thanin others. Thus, space given in this logbook for each ATA chapter should only been viewed as way to document minimum experi-ence. Additional pages are found at the end of the logbook for student to document additional work to support his/her application forEASA Part 66 AML.



Work in all ATA chapters in this logbook does not need to be accomplished by the applicant. Each applicant has to demonstratework in ATA chapter applicable to his/her category and sub-category.

Procedure:Text in blue explains the type of information needed to be documented in the logbook.

ATA Task title Aircrafttype

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Work accomplished with referenceto approved data Date Category

Supervisorsignature &

AML No.29 HYDRAULIC POWER

A330-300

A330-300

TF-RSS

TF-ALK

Troubleshooting L engine pump fault.Replaced engine driven pump iaw AMM 29-11-01-400-814, Rev Sep 01/12.

Replaced hydraulic return filter iaw AMM 29-13-01-400-814 Rev Aug 01/07.

12/02/2013

24/04/2013

B1

B1

Jón JónssonIS.66.3734

Árni ÁrnasonIS.66.3013

29-00 General29-10 Main29-20 Auxiliary29-30 Indicating


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AML No.34 Navigation

A330-300

A330-300

TF-EBR

TF-SBR

Performed troubleshooting on Traffic Alertand Collision Avoidance System (TCAS).Replaced broken pin in plug P 0123 iaw WM20-13-03 Rev Mar 01/08 and AMM 34-46-00-720-815 Rev Jun 01/11.

Altimeter inoperative. Removed and replaceair data computer and perform pitot static leakcheck iaw .AMM 34-12-01-400-814 Rev Sep01/12.

15/02/2013

30/03/2013

B2

B2



34-00 General34-10 Flight Environment Data34-20 Attitude & Direction34-30 Landing & Taxiing Aids34-40 Independent Position Determining34-50 Dependent Position Determining34-60 Flight Management Computing



Name of applicant: Category or sub-categoryTick in relevant boxes

Social security No.: A

B1.1 B1.2 B1.3 B1.4Nationality:

B2

B3

C

Name of Part 145/Subpart F organisation: Maintenance organisation approval reference:

Period From: To: From: To: From: To: Total working days:

Supervisor Name: AML Licence No. Company authorisation No.:











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AML No.05 Time limits/maintenance checks05-00 General05-10 Time limits05-20 Scheduled maintenance checks05-50 Unscheduled maintenance checks

06 DIMENSIONS & AREAS06-00 General06-10 Dimension and areas06-20 Zoning

06-30 Access panels, location andidentification

07 Lifting and shoring07-00 General07-10 Jacking07-20 Shoring




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AML No.08 LEVELING & WEIGHING08-00 General08-10 Weighing & Balancing08-20 Levelling

09 TOWING & TAXIING09-00 General09-10 Towing09-20 Taxiing

10PARKING, MORING,STORAGE & RETURN TOSERVICE

10-00 General10-10 Parking/Storage10-20 Mooring10-30 Return to Service

11 PLACARDS & MARKING11-00 General

11-10 Exterior Color Schemes &Markings

11-20 Exterior Placards & Markings11-20 Exterior Placards & Markings11-30 Interior Placards




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AML No.12 SERVICING –

ROUTINE MAINTENANCE12-00 General12-10 Replenishing12-20 Scheduled Servicing12-30 Unscheduled Servicing

18 VIBRATION & NOISE ANALYSIS(Helicopter only)

18-00 General18-10 Vibration Analysis18-20 Noise Analysis

20 STANDARD PRACTICES -AIRFRAME




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AML No.21 AIR CONDITIONING21-00 General21-10 Compression21-20 Distribution21-30 Pressurization Control21-40 Heating21-50 Cooling21-60 Temperature Control21-70 Moisture / Air Contaminant Control

22 AUTO FLIGHT22-00 General22-10 Autopilot22-20 Speed – Attitude Correction22-30 Auto Throttle22-40 System Monitor22-50 Aerodynamic Load Alleviating




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AML No.23 COMUNICATIONS23-00 General23-10 Speech Communications23-15 SATCOM23-20 Data Transmission & Automatic

Calling23-30 Passenger Address,

Entertainment & Comfort23-40 Interphone23-50 Audio Integrating23-60 Static Discharging23-70 Audio & Video Monitoring23-80 Integrated Automatic Tuning




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AML No.24 ELECTRICAL POWER24-00 General24-10 Generator Drive24-20 AC Generation24-30 DC Generation24-40 External Power24-50 AC Electrical Load Distribution24-60 DC Electrical Load Distribution




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AML No.25 EQUIPMENT / FURNISHINGS25-00 General25-10 Flight Compartment25-20 Passenger Compartment25-30 Buffet / Galley25-40 Lavatories25-50 Cargo Compartment25-60 Emergency25-70 Accessory Compartments25-70 Insulation

26 FIRE PROTECTION26-00 General26-10 Detection26-20 Extinguishing26-30 Explosion Suppression




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AML No.27 FLIGHT CONTROLS27-00 General27-10 Aileron & Tab27-20 Rudder / Ruddevator & Tab27-30 Elevator & Tab27-40 Horizontal Stabilizer / Stabilator27-50 Flaps27-60 Spoiler, Drag Devices & Variable

Aerodynamic Fairings27-70 Gust Lock & Damper27-80 Lift Augmenting

28 FUEL28-00 General28-10 Storage28-20 Distribution – Drain Valves28-30 Dump28-40 Indicating




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AML No.29 HYDRAULIC POWER29-00 General29-10 Main29-20 Auxiliary29-30 Indicating

30 ICE & RAIN PROTECTION30-00 General30-10 Air foil30-20 Air Intakes30-30 Pitot & Static30-40 Windows, Windshields, & Doors30-50 Antennas & Radomes30-60 Propellers / Rotors30-70 Water Lines30-80 Detection




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AML No.31 INDICATING /RECORDING

SYSTEM31-00 General31-10 Instrument & Control Panels31-20 Independent Instrument31-30 Recorders31-40 Central Computers31-50 Central Warning Systems31-60 Central Display Systems31-70 Automatic Data Reporting

Systems

32 LANDING GEAR32-00 General32-10 Main Gear & Doors32-20 Nose Gear / Tail Gear & Doors32-30 Extension & Retraction32-40 Wheel & Brakes32-50 Steering32-60 Position , Warning, & Ground

Safety Switch32-70 Supplementary Gear – Skis,

Floats




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AML No.33 LIGHTS33-00 General33-10 Flight Compartment & Annunciator

Panel33-20 Passenger Compartment33-30 Cargo & Service Compartments33-40 Exterior Lighting33-50 Emergency Lighting

34 NAVIGATION34-00 General34-10 Flight Environment Data34-20 Attitude & Direction34-30 Landing & Taxiing Aids34-40 Independent Position Determining34-50 Dependent Position Determining34-60 Flight Management Computing




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AML No.34 NAVIGATION34-00 General34-10 Flight Environment Data34-20 Attitude & Direction34-30 Landing & Taxiing Aids34-40 Independent Position Determining34-50 Dependent Position Determining34-60 Flight Management Computing




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AML No.35 OXYGEN35-00 General35-10 Crew35-20 Passenger35-30 Portable

36 PNEUMATIC36-00 General36-10 Distribution36-20 Indicating

37 VACUUM37-00 General37-10 Distribution37-20 Indicating




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AML No.38 WATER / WASTE38-00 General38-10 Portable38-20 Wash38-30 Waste Disposal38-40 Air Supply

39 ELECTRICAL - ELECTRONICPANELS & MULTPURPOSECOMPONENTS

39-00 General39-10 Instrument & Control Panels39-20 Electrical & Electronic Equipment

Racks39-30 Electrical & Electronic Junction

Boxes39-50 Integrated Circuits39-60 Printed Circuit Card Assemblies




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AML No.41 WATER BALLAST41-00 General41-10 Storage41-20 Dump41-30 Indication

42 INTEGRATED MODULARAVIONICS

44 CABIN SYSTEMS44-00 General44-10 Cabin Core System44-20 Inflight Entertainment System44-30 External Communication System44-40 Cabin Mass Memory System44-50 Cabin Monitoring System44-60 Miscellaneous Cabin System




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AML No.45 CENTRAL MAINTENANCE

SYSTEM(CMS)

45-00 General45-05 CMS / Aircraft General45-1945-20 CMS / Airframe Systems45-4445-45 45 Central Maintenance Systems45-46 CMS / Airframe Systems45-4945-50 CMS / Structures45-5945-60 CMS / Propellers45-6945-70 CMS / Power Plant45-89




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AML No.46 INFORMATION SYSTEM46-00 General46-10 Airplane General Information

Systems46-20 Flight Deck Information Systems46-30 Maintenance Information Systems46-40 Passenger Information Systems46-50 Miscellaneous Information

Systems

49 AIRBORNE AUXILIARY POWER49-00 General49-10 Power Plant49-20 Engine49-30 Engine Fuel & Control49-40 Ignition / Starting49-50 Air49-60 Engine Controls49-70 Indicating49-80 Exhaust49-90 Oil




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AML No.51 STANDARD PRACTICES &

STRUCTURES - GENERAL51-00 General51-10 Investigation, Clean up &

Aerodynamic Smoothness51-20 Processes51-30 Materials51-40 Fasteners51-50 Support of Airplane for Repair &

Alignment procedures51-60 Control – Surface Balancing51-70 Repairs51-80 Electrical Bonding

52 DOORS52-00 General52-10 Passenger / Crew52-20 Emergency Exit52-30 Cargo52-40 Service52-50 Fixed Interior52-60 Entrance Stairs52-70 Door Warning52-80 Landing Gear




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AML No.53 FUSELAGE53-00 General53-10 Main Frame53-20 Auxiliary Structure53-30 Plates - Skin53-40 Attach Fittings53-50 Aerodynamic Fairings

54 NACELLES / PYLONS54-00 General

55 STABILIZERS55-00 General55-10 Horizontal Stabilizer / Stabilator or

Canard55-20 Elevator - Elevon55-30 Vertical Stabilizer55-40 Rudder - Ruddevator




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AML No.56 WINDOWS56-00 General56-10 Flight Compartment56-20 Passenger Compartment56-30 Door56-40 Inspection & Observation

57 WINGS57-00 General57-10 Center57-20 Outer57-30 Wing Tip57-40 Leading Edge & Leading Edge

Devices57-50 Trailing Edge & Trailing Edge

Devices57-60 Ailerons & Elevons57-70 Spoilers57-90 Wing Folding System

60 STANDARD PRACTICES –PROPELLER / ROTOR




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AML No.61 PROPELLERS / PROPULSORS61-00 General61-10 Propeller Assembly61-20 Controlling61-30 Braking61-40 Indicating61-50 Propulsor Duct

62 MAIN ROTORS62-00 General62-10 Rotor Blades62-20 Rotor Head (s)62-30 Rotor Shaft (s) / Swashplate

Assembly (ies)62-40 Indicating




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AML No.63 MAIN ROTOR DRIVE(S)63-00 General63-10 Engine / Gearbox Couplings63-20 Gearbox(es)63-30 Mounts, Attachments63-40 Indicating

64 TAIL ROTOR64-00 General64-10 Rotor Blades64-20 Rotor Head64-40 Indicating




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AML No.65 TAIL ROTOR DRIVE65-00 General65-10 Shafts65-20 Gearboxes65-40 Indicating

66 ROTOR BLADE & TAILPYLON FOLDING

66-00 General66-10 Rotor Blades66-20 Tail Pylon66-30 Controls & Indicating

67 ROTORS FLIGHT CONTROL67-00 General67-10 Rotor Control67-20 Anti – Torque Rotor Control (Yaw

Control)67-30 Servo – Control System




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AML No.70 STANDARD PRACTICES ENGINE

71 POWER PLANT - GENERAL71-00 General71-10 Cowling71-20 Mounts71-30 Fire seals & Shrouds71-40 Attach Fittings71-50 Electrical Harness71-60 Engine Air Intakes71-70 Engine Drains




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AML No.72 (T) ENGINE – TURBINE /

TURBOPROP, DUCTED FAN /UNDUCTED FAN

72-00 General72-10 Reduction Gear & Shaft Section

(Turboprop and/or Front MountedDriven Propulsor)

72-20 Air Inlet Section72-30 Compressor Section72-40 Combustion Section72-50 Turbine Section72-60 Accessory Drives72-70 By – Pass Section72-80 Propulsor Section (Rear mounted)




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AML No.72 (R) ENGINE - RECIPROCATING72-00 General72-10 Front Section72-20 Power Section72-30 Cylinder Section72-40 Supercharger Section72-50 Lubrication

73 ENGINE – FUEL & CONTROL73-00 General73-10 Distribution73-20 Controlling - Governing73-30 Indicating




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AML No.74 IGNITION74-00 General74-10 Electrical Power Supply74-20 Distribution74-30 Switching

75 BLEED AIR75-00 General75-10 Engine Anti - Icing75-20 Engine Cooling75-30 Compressor Control75-40 Indicating

76 ENGINE CONTROLS76-00 General76-10 Power Control76-20 Emergency Shutdown




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AML No.77 ENGINE INDICATING77-00 General77-10 Power77-20 Temperature77-30 Analyser77-40 Integrated Engine Instrument

Systems

78 EXHAUST78-00 General78-10 Collector - Nozzle78-20 Noise Suppressor78-30 Thrust Reverser78-40 Supplemental Air

79 OIL79-00 General79-10 Storage (Dry Sump)79-20 Distribution79-30 Indicating




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AML No.80 STARTING80-00 General80-10 Cranking

81 TURBINES(RECIPROCATING ENGINES)

81-00 General81-10 Power Recovery81-20 Turbo - Supercharger

82 WATER INJECTION82-00 General82-10 Storage82-20 Distribution82-30 Dumping & Purging82-40 Indicating




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AML No.83 ACCESSORY GEAR BOXES

(ENGINE DRIVEN)83-00 General83-10 Drive Shaft Section83-20 Gear Box Section

84 PROPULSION AUGMENTATION84-00 General84-10 Jet Assisted Take off

91 CHARTS


Icelandic Civil Aviation Administration


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AML No.

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Part-66 and AMC/GM rev. May 2012 GM 66.A.20(a) Privileges

GM 66.A.20(a) Privileges

1. The following definitions apply:

Electrical system means the aircraft electrical power supply source, plus the distribution systemto the different components contained in the aircraft and relevant connectors. Lighting systemsare also included in this definition. When working on cables and connectors which are part ofthese electrical systems, the following typical practices are included in the privileges:

• Continuity, insulation and bonding techniques and testing;

• Crimping and testing of crimped joints;

• Connector pin removal and insertion;

• Wiring protection techniques.

Avionics system means an aircraft system that transfers, processes, displays or stores analogueor digital data using data lines, data buses, coaxial cables, wireless or other data transmissionmedium, and includes the system’s components and connectors. Examples of avionics systemsinclude the following:

• Autoflight;

• Communication, Radar and Navigation;

• Instruments (see NOTE below);

• In Flight Entertainment Systems;

• Integrated Modular Avionics (IMA);

• On-Board Maintenance Systems;

• Information Systems;

• Fly by Wire Systems (related to ATA27 “Flight Controls”);

• Fibre Optic Control Systems.

NOTE: Instruments are formally included within the privileges of the B2 licence holders.However, maintenance on electromechanical and pitot-static components may also bereleased by a B1 license holder.

Simple test means a test described in approved maintenance data and meeting all the followingcriteria:

• The serviceability of the system can be verified using aircraft controls, switches, Built-inTest Equipment (BITE), Central Maintenance Computer (CMC) or external test equip-ment not involving special training.

• The outcome of the test is a unique go – no go indication or parameter, which can be asingle value or a value within an interval tolerance. No interpretation of the test resultor interdependence of different values is allowed.

• The test does not involve more than 10 actions as described in the approved mainte-nance data (not including those required to configure the aircraft prior to the test, i.e.jacking, flaps down, etc, or to return the aircraft to its initial configuration). Pushing acontrol, switch or button, and reading the corresponding outcome may be consideredas a single step even if the maintenance data shows them separated.

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Part-66 and AMC/GM rev. May 2012 GM 66.A.20(a) Privileges

Troubleshooting means the procedures and actions necessary, using approved maintenancedata, in order to identify the root cause of a defect or malfunction. It may include the use ofBITE or external test equipment.

Line maintenance means any maintenance that is carried out before flight to ensure that theaircraft is fit for the intended flight. It may include:

• trouble shooting;

• defect rectification;

• component replacement with use of external test equipment, if required. Componentreplacement may include components such as engines and propellers;

• scheduled maintenance and/or checks including visual inspections that will detectobvious unsatisfactory conditions/discrepancies but do not require extensive in depthinspection. It may also include internal structure, systems and powerplant items whichare visible through quick opening access panels/doors;

• minor repairs and modifications which do not require extensive disassembly and canbe accomplished by simple means;

• for temporary or occasional cases (Airworthiness Directives, hereinafter AD; servicebulletins, hereinafter SB) the quality manager may accept base maintenance tasksto be performed by a line maintenance organisation provided all requirements arefulfilled. The Member State will prescribe the conditions under which these tasks maybe performed.

Base Maintenance means any task falling outside the criteria that are given above for LineMaintenance.

NOTE:

Aircraft maintained in accordance with "progressive" type programmes need to be indi-vidually assessed in relation to this paragraph. In principle, the decision to allow some"progressive" checks to be carried out is determined by the assessment that all tasks withinthe particular check can be carried out safely to the required standards at the designatedline maintenance station.

2. The category B3 licence does not include any A subcategory. Nevertheless, this does not pre-vent the B3 licence holder from releasing maintenance tasks typical of the A1.2 subcategory forpiston-engine non-pressurized aeroplanes of 2000 Kg MTOM and below, within the limitationscontained in the B3 licence.

3. The category C licence permits certification of scheduled base maintenance by the issue of asingle certificate of release to service for the complete aircraft after the completion of all suchmaintenance. The basis for this certification is that the maintenance has been carried out bycompetent mechanics and category B1, B2 and B3 support staff, as appropriate, have signed forthe maintenance tasks under their respective specialisation. The principal function of the cat-egory C certifying staff is to ensure that all required maintenance has been called up and signedoff by the category B1, B2 and B3 support staff, as appropriate, before issue of the certificate ofrelease to service. Only category C personnel who also hold category B1, B2 or B3 qualificationsmay perform both roles in base maintenance.

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