1. Knowledge levels for Category A, B1, B2, B2L, B3 and C aircraft maintenance licences

Regulation (EU) 2018/1142

Basic knowledge for categories A, B1, B2, B2L and B3 is indicated by knowledge levels (1, 2 or 3) of each applicable subject. Category C applicants shall meet either the category B1 or the category B2 basic knowledge levels.

The knowledge level indicators are defined on 3 levels as follows:

               LEVEL 1: A familiarisation with the principal elements of the subject.

Objectives:

(a) The applicant should be familiar with the basic elements of the subject.

(b) The applicant should be able to give a simple description of the whole subject, using common words and examples.

(c) The applicant should be able to use typical terms.

               LEVEL 2: A general knowledge of the theoretical and practical aspects of the subject and an ability to apply that knowledge.

Objectives:

(a) The applicant should be able to understand the theoretical fundamentals of the subject.

(b) The applicant should be able to give a general description of the subject using, as appropriate, typical examples.

(c) The applicant should be able to use mathematical formulae in conjunction with physical laws describing the subject.

(d) The applicant should be able to read and understand sketches, drawings and schematics describing the subject.

(e) The applicant should be able to apply his knowledge in a practical manner using detailed procedures.

               LEVEL 3: A detailed knowledge of the theoretical and practical aspects of the subject and a capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner.

Objectives:

(a) The applicant should know the theory of the subject and interrelationships with other subjects.

(b) The applicant should be able to give a detailed description of the subject using theoretical fundamentals and specific examples.

(c) The applicant should understand and be able to use mathematical formulae related to the subject.

(d) The applicant should be able to read, understand and prepare sketches, simple drawings and schematics describing the subject.

(e) The applicant should be able to apply his knowledge in a practical manner using manufacturer's instructions.

(f) The applicant should be able to interpret results from various sources and measurements and apply corrective action where appropriate.

2. Modularisation

Regulation (EU) 2023/989

Qualification on basic subjects for each aircraft maintenance licence category or subcategory shall be in accordance with the following matrix, where applicable subjects are indicated by an ‘X’, while ‘n/a’ means that the subject module is neither applicable nor required.

Subject module

B1.1

A1

B1.2

A2

B1.3

A3

B1.4

A4

B3

 

 

 

B2

 

 

 

B2L

 

 

 

C

Turbine engine

Piston engine

Turbine engine

Piston engine

Piston-engine non- pressurised aeroplanes MTOM ≤ 2 t

1. MATHEMATICS

X

X

X

X

X

X

X

X

2. PHYSICS

X

X

X

X

X

X

X

X

3. ELECTRICAL

FUNDAMENTALS

X

X

X

X

X

X

X

X

4. ELECTRONICS

FUNDAMENTALS

X

(n/a for A1)

X

(n/a for A2)

X

(n/a for A3)

X

(n/a for A4)

X

X

X

X

5. DIGITAL TECHNIQUES/ELECTR-ONIC INSTRUMENT SYSTEMS

X

X

X

X

X

X

X

X

6. MATERIALS AND HARDWARE

X

X

X

X

X

X

X

X

7. MAINTENANCE PRACTICES

X

X

X

X

X

X

X

X

8. BASIC AERODYNAMICS

X

X

X

X

X

X

X

X

9. HUMAN FACTORS

X

X

X

X

X

X

X

X

10. AVIATION LEGISLATION

X

X

X

X

X

X

X

X

11. AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

X

X

n/a

n/a

X

n/a

n/a

11, 15 & 17

as B1.1

 or

 

11, 16 & 17

as B1.2

 or

 

12 & 15

as B1.3

or

 

12 & 16

as B1.4 or

 

13 & 14

as B2

12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

n/a

n/a

X

X

n/a

n/a

n/a

13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

n/a

n/a

n/a

n/a

n/a

X

X

14. PROPULSION

n/a

n/a

n/a

n/a

n/a

X

X

15. GAS TURBINE ENGINES

X

n/a

X

n/a

n/a

n/a

n/a

16. PISTON ENGINE

n/a

X

n/a

X

X

n/a

n/a

17. PROPELLER

X

X

n/a

n/a

X

n/a

n/a

MODULE 1. MATHEMATICS

Regulation (EU) 2023/989

MODULE 1. MATHEMATICS

LEVEL

A

B1

B2

B2L

B3

1.1 Arithmetic

1

2

1.2 Algebra

 

 

 

 

(a) Simple algebraic expressions;

1

2

(b) Equations.

1

1.3 Geometry

 

 

 

(a) Simple geometrical constructions;

1

 

(b) Graphical representation;

2

2

 

(c) Trigonometry.

2

MODULE 2. PHYSICS

Regulation (EU) 2023/989

MODULE 2. PHYSICS

LEVEL

A

B3

B1

B2

B2L

2.1 Matter

1

2

2.2. Mechanics

 

 

2.2.1 Statics

1

2

2.2.2 Kinetics

1

2

2.2.3 Dynamics

 

 

 

 

(a) Mass, force and energy;

1

2

(b) Momentum and conservation of momentum.

1

2

2.2.4 Fluid dynamics

 

 

 

(a) Gravity and density;

2

2

 

(b) Viscosity; compressibility on fluids; static, dynamic, and total pressure.

1

2

2.3 Thermodynamics

 

 

 

(a) Temperature;

2

2

 

(b) Heat.

1

2

2.4 Optics (light)

2

2.5 Wave motion and sound

2

MODULE 3. ELECTRICAL FUNDAMENTALS

Regulation (EU) 2023/989

MODULE 3. ELECTRICAL FUNDAMENTALS

LEVEL

A

B1

B2

B2L

B3

3.1 Electron theory

1

1

1

3.2 Static electricity and conduction

1

2

1

3.3 Electrical terminology

1

2

1

3.4 Generation of electricity

1

1

1

3.5 Sources of DC electricity

1

2

2

3.6 DC circuits

1

2

1

3.7 Resistance/resistor

 

 

 

 

(a) Resistance;

2

1

 

(b) Resistors.

1

3.8 Power

2

1

3.9 Capacitance/capacitor

2

1

3.10 Magnetism

 

 

 

 

(a) Theory of magnetism;

2

1

 

(b) Magnetomotive force.

2

1

3.11 Inductance/inductor

2

1

3.12 DC motor/generator theory

2

1

3.13 AC theory

1

2

1

3.14 Resistive (R), capacitive (C) and inductive (L) circuits

2

1

3.15 Transformers

2

1

3.16 Filters

1

3.17 AC generators

2

1

3.18 AC motors 

2

1

MODULE 4. ELECTRONIC FUNDAMENTALS

Regulation (EU) 2023/989

MODULE 4. ELECTRONICS FUNDAMENTALS

LEVEL

A

B1

B3

B2

B2L

4.1 Semiconductors

 

 

 

4.1.1 Diodes

 

 

 

 

(a) Description and characteristics;

2

2

 

(b) Operation and function.

2

4.1.2 Transistors

 

 

 

 

(a) Description and characteristics;

1

2

 

(b) Filters.

2

4.1.3 Integrated circuits

 

 

 

 

(a) Basic description and operation;

1

2

 

(b) Description and operation.

2

4.2 Printed circuit boards

1

2

4.3 Servomechanisms

 

 

 

 

(a) Principles;

1

2

 

(b) Construction, operation, and use.

2

MODULE 5. DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT SYSTEMS

Regulation (EU) 2023/989

MODULE 5. DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT SYSTEMS

LEVEL

A

B3

B1

B2

B2L

5.1 Electronic instrument systems

1

1

1

1

5.2 Numbering systems

1

2

5.3 Data conversion

1

2

5.4 Data buses

2

2

5.5 Logic circuits

 

 

 

 

 

(a) Identification and applications;

2

2

 

(b) Interpretation of logic diagrams.

2

5.6 Basic computer structure

 

 

 

 

 

(a) Computer terminology and technology;

1

1

2

2

 

(b) Computer operation.

2

5.7 Microprocessors

2

5.8 Integrated circuits

2

5.9 Multiplexing

2

5.10 Fibre optics

1

2

5.11 Electronic displays

1

1

2

2

5.12 Electrostatic sensitive devices

1

1

2

2

5.13 Software management control

1

2

2

5.14 Electromagnetic environment

1

2

2

5.15 Typical electronic/digital aircraft systems

1

1

1

1

MODULE 6. MATERIALS AND HARDWARE

Regulation (EU) 2023/989

MODULE 6. MATERIALS AND HARDWARE

LEVEL

A

B1

B3

B2

B2L

6.1 Aircraft materials — ferrous

 

 

 

 

(a) Alloy steels used in aircraft;

1

2

1

 

(b) Testing of ferrous materials;

1

1

 

(c) Repair and inspection procedures.

2

1

6.2 Aircraft materials — non-ferrous

 

 

 

 

(a) Characteristics;

1

2

1

 

(b) Testing of non-ferrous materials;

1

1

 

(c) Repair and inspection procedures.

2

1

6.3 Aircraft materials – composite and non-metallic

 

 

 

   6.3.1 Composite and non-metallic other than wood and fabric

 

 

 

 

(a) Characteristics;

1

2

2

 

(b) Detection of defects

1

2

 

(c) Repairs and inspection procedures.

2

1

6.3.2 Wooden structures

1

1

6.3.3 Fabric covering

1

6.4 Corrosion

 

 

 

 

(a) Chemical fundamentals;

1

1

1

 

(b) Types of corrosion.

2

3

2

6.5 Fasteners

 

 

 

   6.5.1 Screw threads

2

2

2

   6.5.2 Bolts, studs and screws

2

2

2

   6.5.3 Locking devices

2

2

2

   6.5.4 Aircraft rivets

1

2

1

6.6 Pipes and unions

 

 

 

 

(a) Identification;

2

2

2

 

(b) Standard unions.

2

2

1

6.7 Springs

2

1

6.8 Bearings

1

2

2

6.9 Transmissions

1

2

2

6.10 Control cables

1

2

1

6.11 Electrical cables and connectors

1

2

2

MODULE 7. MAINTENANCE PRACTICES

Regulation (EU) 2023/989

MODULE 7. MAINTENANCE PRACTICES

LEVEL

A

B1

B3

B2

B2L

7.1 Safety precautions – aircraft and workshop

3

3

3

7.2 Workshop practices

3

3

3

7.3 Tools

3

3

3

7.4 (Reserved)

7.5 Engineering drawings, diagrams and standards

1

2

2

7.6 Fits and Clearances

1

2

1

7.7 Electrical wiring interconnection system (EWIS)

1

3

3

7.8 Riveting

1

2

7.9 Pipes and Hoses

1

2

7.10 Springs

1

2

7.11 Bearings

1

2

7.12 Transmissions

1

2

7.13 Control cables

1

2

7.14 Material handling

 

 

 

   7.14.1 Sheet metal

2

   7.14.2 Composite and non-metallic

2

   7.14.3 Additive manufacturing

1

1

1

7.15 (Reserved)

 

 

 

7.16 Aircraft weight and balance

 

 

 

 

(a) Centre-of-gravity calculation;

2

2

 

(b) Aircraft weighing.

2

7.17 Aircraft handling and storage

2

2

2

7.18 Disassembly, inspection, repair and assembly techniques

 

 

 

 

(a) Types of defects and visual inspection techniques;

2

3

3

 

(b) General repair methods – structural repair manual;

2

 

(c) Non-destructive inspection techniques;

2

1

 

(d) Disassembly and re-assembly techniques;

2

2

2

 

(e) Troubleshooting techniques.

2

2

7.19 Abnormal events

 

 

 

 

(a) Inspections following lightning strikes and HIRF penetration;

2

2

2

 

(b) Inspections following abnormal events such as heavy landings and flight through turbulence.

2

2

7.20 Maintenance Procedures

1

2

2

7.21 Documentation & communication

1

2

2

MODULE 8. BASIC AERODYNAMICS

Regulation (EU) 2023/989

MODULE 8. BASIC AERODYNAMICS

LEVEL

A

B3

B1

B2

B2L

8.1 Physics of the atmosphere

1

2

 

International Standard Atmosphere (ISA), application to aerodynamics.

8.2 Aerodynamics

1

2

8.3 Theory of flight

1

2

8.4 High-speed airflow

1

2

8.5 Flight stability and dynamics

1

2

MODULE 9. HUMAN FACTORS

Regulation (EU) 2023/989

MODULE 9. HUMAN FACTORS

LEVEL

ALL

9.1 General

2

9.2 Human performance and limitations

2

9.3 Social psychology

1

9.4 Factors that affect performance

2

9.5 Physical Environment

1

9.6 Tasks

1

9.7 Communication

2

9.8 Human error

2

9.9 Safety management

2

9.10 The ‘Dirty Dozen’ and risk mitigation

2

MODULE 10. AVIATION LEGISLATION

Regulation (EU) 2023/989

MODULE 10. AVIATION LEGISLATION

LEVEL

A

B1

B2

B2L

 B3

10.1 Regulatory framework

1

1

10.2 Certifying Staff — maintenance

2

2

10.3 Approved maintenance organisations

2

2

10.4 Independent certifying staff

3

10.5 Air operations

1

1

10.6 Certification of aircraft, parts, and appliances

2

2

10.7 Continuing airworthiness

2

2

10.8 Oversight principles in continuing airworthiness

1

1

10.9 Maintenance and certification beyond the current EU regulations (if not superseded by EU requirements)

1

10.10 Cybersecurity in aviation maintenance

1

1

MODULE 11. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Regulation (EU) 2023/989

MODULE 11. AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

A1

A2

B1.1

B1.2

B3

11.1 Theory of flight

 

 

 

 

 

 

(a) Aeroplane aerodynamics and flight controls;

1

1

2

2

1

 

(b) Aeroplane, other aerodynamic devices.

1

1

2

2

1

11.2 Airframe structures (ATA 51)

 

 

 

 

 

 

 

(a) General concepts;

2

2

2

2

2

(b) Airworthiness requirements for structural strength;

2

2

2

2

2

 

(c) Construction methods.

1

1

2

2

2

11.3 Airframe Structures — aeroplanes

 

 

 

 

 

   11.3.1 Fuselage, doors, windows (ATA 52/53/56)

 

 

 

 

 

 

(a) Construction principles;

1

1

2

2

1

 

(b) Airborne towing devices;

1

1

1

1

1

 

(c) Doors.

1

1

2

1

-

   11.3.2 Wings (ATA 57)

1

1

2

2

1

   11.3.3 Stabilisers (ATA 55)

1

1

2

2

1

   11.3.4 Flight control surfaces (ATA 55/57)

1

1

2

2

1

   11.3.5 Nacelles/pylons (ATA 54)

1

1

2

2

1

11.4 Air conditioning and cabin pressurisation (ATA 21)

 

 

 

 

 

 

(a) Pressurisation;

1

1

3

3

 

(b) Air supply;

1

3

 

(c) Air conditioning;

1

3

 

(d) Safety and warning devices;

1

1

3

3

 

(e) Heating and ventilation system.

1

3

1

11.5 Instruments/avionic systems

 

 

 

 

 

   11.5.1 Instrument systems (ATA 31)

1

1

2

2

2

   11.5.2 Avionic Systems

1

 

1

 

1

1

1

 

Fundamentals of system layouts and operation of:

— Autoflight (ATA 22),

— Communications (ATA 23),

— Navigation Systems (ATA 34).

 

 

 

11.6 Electrical power (ATA 24)

1

1

3

3

3

11.7 Equipment and furnishings (ATA 25)

 

 

 

 

 

 

(a) Emergency equipment;

2

2

2

2

2

 

(b) Cabin and cargo layout.

1

1

1

1

11.8 Fire protection (ATA 26)

 

 

 

 

 

 

(a) Fire and smoke detection system and fire extinguishing systems;

1

1

1

1

 

(b) Portable fire extinguisher.

1

1

1

1

1

11.9 Flight controls (ATA 27)

 

 

 

 

 

 

(a) Primary and secondary flight controls;

1

1

3

2

2

 

(b) Actuation and protection;

1

3

 

(c) System operation;

1

3

 

(d) Balancing and rigging.

1

1

3

3

2

11.10 Fuel systems (ATA 28, ATA 47)

 

 

 

 

 

 

(a) Systems layout;

1

1

3

3

1

 

(b) Fuel handling;

1

1

3

3

1

 

(c) Indication and warnings;

1

1

3

3

1

 

(d) Special systems;

1

3

 

(e) Balancing.

1

3

11.11 Hydraulic power (ATA 29)

 

 

 

 

 

 

(a) System description;

1

1

3

3

2

 

(b) System operation (1);

1

1

3

3

2

 

(c) System operation (2).

1

3

11.12 Ice and rain protection (ATA 30)

 

 

 

 

 

 

(a) Principles;

1

1

3

3

1

 

(b) De-icing;

1

1

3

3

1

 

(c) Anti-icing;

1

3

 

(d) Wipers;

1

1

3

3

1

 

(d) Tail protection.

1

3

11.13 Landing Gear (ATA 32)

 

 

 

 

 

 

(a) Description;

2

2

3

3

2

 

(b) System operation;

2

2

3

3

2

 

(c) Air-ground sensing;

2

3

 

(d) Tail protection.

2

2

3

3

2

11.14 Lights (ATA 33)

2

2

3

3

2

11.15 Oxygen (ATA 35)

1

1

3

3

2

11.16 Pneumatic/vacuum (ATA 36)

 

 

 

 

 

 

(a) Systems;

1

1

3

3

2

 

(b) Pumps.

1

1

3

3

2

11.17 Water/waste (ATA 38)

 

 

 

 

 

 

(a) Systems;

2

2

3

3

2

 

(b) Corrosion.

2

2

3

3

2

11.18 On-board maintenance systems (ATA 45)

1

2

11.19 Integrated Modular Avionics (ATA 42)

 

 

 

 

 

 

(a) Overall system description and theory;

1

2

 

(b) Typical system layouts.

1

2

11.20 Cabin systems (ATA 44)

1

2

11.21 Information systems (ATA 46)

1

2

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

Regulation (EU) 2023/989

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

A3

A4

B1.3

B1.4

12.1 Theory of flight — rotary wing aerodynamics

1

2

12.2 Flight control systems (ATA 67)

2

3

12.3 Blade tracking and vibration analysis (ATA 18)

1

3

12.4 Transmission

1

3

12.5 Airframe structures (ATA 51)

 

 

 

(a) General concept;

2

2

 

(b) Construction methods of the principal elements.

1

2

12.6 Air conditioning (ATA 21)

 

 

   12.6.1 Air supply

1

2

   12.6.2 Air conditioning

1

3

12.7 Instruments/avionic systems

 

 

   12.7.1 Instrument systems (ATA 31)

1

2

   12.7.2 Avionic systems

1

1

 

Fundamentals of system layouts and operation of:

Auto Flight (ATA 22);

Communications (ATA 23);

Navigation Systems (ATA 34).

12.8 Electrical Power (ATA 24)

1

3

12.9 Equipment and furnishings (ATA 25)

 

 

 

(a) Emergency equipment;
Seats, harnesses, and belts;
Lifting systems;

2

2

 

(b) Emergency flotation systems;
Cabin layout, cargo retention;
Equipment layout;
Cabin furnishing installation.

1

1

12.10 Fire Protection (ATA 26)

 

 

 

(a) Fire and smoke detection systems and Fire-extinguishing systems;

1

3

 

(b) Portable fire extinguishers.

1

1

12.11 Fuel Systems (ATA 28)

1

3

12.12 Hydraulic Power (ATA 29)

1

3

12.13 Ice and Rain Protection (ATA 30)

1

3

12.14 Landing Gear (ATA 32)

 

2

 

3

 

(a) System description and operation;

 

(b) Sensors.

2

3

12.15 Lights (ATA 33)

2

3

12.16 (Reserved)

2

3

12.17 Integrated Modular Avionics (ATA 42)

 

1

 

2

 

(a) Overall system description and theory

 

(b) Typical system layouts

1

2

12.18 On-board Maintenance Systems (ATA 45)

1

2

 

Central maintenance computers;
Data-loading system;

Electronic library system.

12.19 Information Systems (ATA 46)

1

2

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

Regulation (EU) 2023/989

C/N: Communication & Navigation; Ins.: Instruments; A/F: Autoflight; Sur.: Surveillance; A/S: Airframe & Systems

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

B2

 

B2L

Basic

B2L

C/N

B2L

Ins.

B2L

A/F

B2L

Sur.

B2L

A/S

13.1 Theory of Flight

 

 

 

 

 

 

 

 

(a) Aeroplane Aerodynamics and Flight Controls;

1

 

1

 

(b) Rotary Wing Aerodynamics.

1

1

13.2 Structures – General Concepts (ATA 51)

 

 

 

 

 

 

 

 

(a) General concept;

2

2

 

(b) Fundamentals of structural systems;

1

1

13.3 Autoflight (ATA 22)

 

3

 

 

 

 

 

 

 

(a) Fundamentals of automatic flight control;

3

 

(b) Autothrottle systems and automatic landing systems.

3

3

13.4 Communication/Navigation (ATA 23/34)

 

3

 

 

 

 

 

 

 

(a) Fundamentals of communication and navigation systems;

3

 

(b) Fundamentals of aircraft surveillance systems.

3

3

13.5 Electrical power (ATA 24)

3

3

13.6 Equipment and furnishings (ATA 25)

3

13.7 Flight Controls

 

 

 

 

 

 

 

 

(a) Primary and secondary flight controls (ATA 27);

2

2

 

(b) Actuation and protection;

2

2

 

(c) System operation;

3

3

 

(d) Rotorcraft flight controls (ATA 67).

2

2

13.8 Instruments (ATA 31)

3

3

13.9 Lights (ATA 33)

3

3

13.10 On-board maintenance systems (ATA 45)

3

13.11 Air conditioning and cabin pressurisation (ATA 21)

 

 

 

 

 

 

 

 

(a) Pressurisation;

3

3

 

(b) Air supply;

1

 

1

 

(c) Air conditioning;

3

3

 

(d) Safety and warning devices.

3

3

13.12 Fire protection (ATA 26)

 

 

 

 

 

 

 

 

(a) Fire and smoke detection system and fire-extinguishing systems;

3

3

 

(b) Portable fire extinguisher.

1

1

13.13 Fuel systems (ATA 28, ATA 47)

 

 

 

 

 

 

 

 

(a) System layout;

1

1

 

(b) Fuel handling;

2

2

 

(c) Indications and warnings;

3

3

 

(d) Special systems;

1

1

 

(e) Balancing

3

3

13.14 Hydraulic power (ATA 29)

 

 

 

 

 

 

 

 

(a) System layout;

1

1

 

(b) System operation (1);

3

3

 

(c) System operation (2);

3

3

13.15 Ice and rain protection (ATA 30)

 

 

 

 

 

 

 

 

(a) Principles;

2

2

 

(b) De-icing;

3

3

 

(c) Anti-icing;

2

2

 

(d) Wiper systems;

1

1

 

(e) Rain repellent

1

1

13.16 Landing gear (ATA 32)

 

 

 

 

 

 

 

 

(a) Description;

1

1

 

(b) System;

3

3

 

(c) Air-ground sensing.

3

3

13.17 Oxygen (ATA 35)

3

3

13.18 Pneumatic/vacuum (ATA 36)

2

 

2

13.19 Water/waste (ATA 38)

2

2

13.20 Integrated modular avionics (ATA 42)

 

 

 

 

 

 

 

 

(a) Overall system description and theory;

3

-

 

(b) Typical system layouts.

3

-

13.21 Cabin systems (ATA 44)

3

13.22 Information systems (ATA 46)

3

MODULE 14. PROPULSION

Regulation (EU) 2023/989

MODULE 14. PROPULSION

LEVEL

B2

B2L Instruments

B2L Airframe & Systems

14.1 Engines

 

 

(a) Turbine engines;

1

 

(b) Auxiliary power units (APUs);

1

 

(c) Piston engines;

1

 

(d) Electric and hybrid engines;

2

 

(e) Engine control.

2

14.2 Electric/electronic engine indication systems

2

14.3 Propeller systems

2

14.4 Starting and ignition systems

2

MODULE 15. GAS TURBINE ENGINE

Regulation (EU) 2023/989

MODULE 15. GAS TURBINE ENGINE

LEVEL

A1

 A3

B1.1 B1.3

15.1 Fundamentals

1

2

15.2 Engine performance

2

15.3 Inlet

2

2

15.4 Compressors

1

2

15.5 Combustion section

1

2

15.6 Turbine section

2

2

15.7 Exhaust

1

2

15.8 Bearings and seals

2

15.9 Lubricants and fuels

1

2

15.10 Lubrication systems

1

2

15.11 Fuel systems

1

2

15.12 Air systems

1

2

15.13 Starting and ignition systems

1

2

15.14 Engine indication systems

1

2

15.15 Alternate turbine constructions

1

15.16 Turboprop engines

1

2

15.17 Turboshaft engines

1

2

15.18 Auxiliary power units (APUs)

1

2

15.19 Power plant installation

1

2

15.20 Fire protection systems

1

2

15.21 Engine monitoring and ground operation

1

3

15.22 Engine storage and preservation

2

MODULE 16. PISTON ENGINE

Regulation (EU) 2023/989

MODULE 16. PISTON ENGINE

LEVEL

A2

A4

B1.2 B1.4 B3

16.1 Fundamentals

1

2

16.2 Engine performance

1

2

16.3 Engine construction

1

2

16.4 Engine fuel systems

 

 

   16.4.1 Carburettors

1

2

   16.4.2 Fuel injection systems

1

2

   16.4.3 Electronic engine control

1

2

16.5 Starting and ignition systems

1

2

16.6 Induction, exhaust and cooling systems

1

2

16.7 Supercharging/turbocharging

1

2

16.8 Lubricants and fuels

1

2

16.9 Lubrication systems

1

2

16.10 Engine indication systems

1

2

16.11 Power plant installation

1

2

16.12 Engine monitoring and ground operation

1

3

16.13 Engine storage and preservation

2

16.14 Alternative piston engine constructions

1

1

MODULE 17. PROPELLER

Regulation (EU) 2023/989

MODULE 17A. PROPELLER

LEVEL

A1

A2

B1.1 B1.2

B3

17.1 Fundamentals

1

2

17.2 Propeller construction

1

2

17.3 Propeller pitch control

1

2

17.4 Propeller synchronising

2

17.5 Propeller ice protection

1

2

17.6 Propeller maintenance

1

3

17.7 Propeller storage and preservation

1

2’

3. Basic training methods

Regulation (EU) 2023/989

An appropriate training method, or combination of methods, shall be determined for the entire course or for each of its modules or submodules, with regard to the scope and objectives of each training phase and taking into consideration the benefits and limitations of the available training methods.

Multimedia-based training (MBT) methods may be used in order to achieve the training objectives either in a physically or in a virtually controlled environment.

MODULARISATION

MODULE 1 — MATHEMATICS

 

 

MODULE 1 — MATHEMATICS

LEVEL

A1

A2

A3

A4

B1

B2

B2L

B3

1.1 Arithmetic

1

2

 

Arithmetical terms and signs, methods of multiplication and division, fractions and decimals, factors and multiples, weights, measures and conversion factors, ratio and proportion, averages and percentages, areas and volumes, squares, cubes, square and cube roots.

1.2 Algebra

 

 

 

(a) Evaluating simple algebraic expressions, addition, subtraction, multiplication and division, use of brackets, simple algebraic fractions;

1

2

 

(b) Linear equations and their solutions;

Indices and powers, negative and fractional indices;

Binary and other applicable numbering systems;

Simultaneous equations and second-degree equations with one unknown;

Logarithms.

1

1.3 Geometry

 

 

 

(a) Simple geometrical constructions;

1

 

(b) Graphical representation: nature and uses of graphs, graphs of equations/functions;

2

2

 

(c) Simple trigonometry: trigonometrical relationships, use of tables and rectangular and polar coordinates.

2

MODULE 2 — PHYSICS

MODULE 2 — PHYSICS

LEVEL

A1

A2

A3

A4

B3

B1

B2

B2L

 

2.1 Matter

1

2

 

 

 

 

Nature of matter: the chemical elements, structure of atoms, molecules;

Chemical compounds;

States: solid, liquid, and gaseous;

Changes between states.

2.2 Mechanics

 

 

 2.2.1 Statics

1

2

 

 

 

 

 

Forces, moments and couples, representation as vectors;

Centre of gravity;

Elements of theory of stress, strain, and elasticity: tension, compression, shear, and torsion;

Nature and properties of solid, fluid, and gas matter;

Pressure and buoyancy in liquids (barometers).

 2.2.2 Kinetics

1

2

 

 

 

 

 

Linear movement: uniform motion in a straight line, motion under constant acceleration (motion under gravity);

Rotational movement: uniform circular motion (centrifugal/centripetal forces);

Periodic motion: pendular movement;

Simple theory of vibration, harmonics, and resonance;

Velocity ratio, mechanical advantage, and efficiency.

 2.2.3 Dynamics

 

 

 

(a) Mass;

Force, inertia, work, power, energy (potential, kinetic and total energy), heat, efficiency;

1

2

 

(b) Momentum, conservation of momentum;

Impulse;

Gyroscopic principles;

Friction: nature and effects, coefficient of friction (rolling resistance).

1

2

 2.2.4 Fluid dynamics

 

 

 

(a) Specific gravity and density;

2

2

 

(b) Viscosity, fluid resistance, effects of streamlining;

Effects of compressibility on fluids;

Static, dynamic, and total pressure: Bernoulli’s Theorem, venturi.

1

2

2.3 Thermodynamics

 

 

 

(a) Temperature: thermometers and temperature scales (Celsius, Fahrenheit and Kelvin); definition of heat;

2

2

 

(b) Heat capacity, specific heat;

Heat transfer: convection, radiation and conduction;

Volumetric expansion;

First and second law of thermodynamics;

Gases: ideal gases laws; specific heat at constant volume and constant pressure, work done by expanding gas;

Isothermal, adiabatic expansion and compression, engine cycles, constant volume and constant pressure, refrigerators and heat pumps;

Latent heats of fusion and evaporation, thermal energy, heat of combustion.

1

2

2.4 Optics (Light)

2

 

 

 

Nature of light; speed of light;

Laws of reflection and refraction: reflection at plane surfaces, reflection by spherical mirrors, refraction, lenses;

Fibre optics.

2.5 Wave motion and sound

2

 

 

Wave motion: mechanical waves, sinusoidal wave motion, interference phenomena, standing waves;

Sound: speed of sound, production of sound, intensity, pitch and quality, Doppler effect.

MODULE 3 — ELECTRICS FUNDAMENTALS

 

 

MODULE 3 — ELECTRICS FUNDAMENTALS

LEVEL

A1

A2

A3

A4

B1

B2

B2L

B3

3.1 Electron theory

1

1

1

 

 

Structure and distribution of electrical charges within atoms, molecules, ions, and compounds;

Molecular structure of conductors, semiconductors, and insulators.

3.2 Static electricity and conduction

1

2

1

 

 

 

 

Static electricity and distribution of electrostatic charges;

Electrostatic laws of attraction and repulsion;

Units of charge, Coulomb’s law;

Conduction of electricity in solids, liquids, gases and in vacuum.

3.3 Electrical terminology

1

2

1

 

The following terms, their units and factors affecting them: potential difference, electromotive force, voltage, current, resistance, conductance, charge, conventional current flow, electron flow.

3.4 Generation of electricity

1

1

1

 

Production of electricity by the following methods: light, heat, friction, pressure, chemical reaction, magnetism, and motion.

3.5 Sources of DC electricity

1

2

2

 

 

 

 

 

Construction and basic chemical reaction of primary cells, secondary cells, lead acid cells, nickel cadmium cells, lithium cells, nickel cells and other alkaline cells;

Cells connected in series and in parallel;

Internal resistance and its effect on a battery;

Construction, materials, and operation of thermocouples;

Operation of photocells.

3.6 DC circuits

1

2

1

 

 

 

Ohm’s law, Kirchhoff’s voltage, and current laws;

Calculations using the above laws to find resistance, voltage, and current;

Significance of the internal resistance of a supply.

3.7 Resistance/Resistor

 

 

 

 

(a) Resistance

Specific resistance;

Calculation of total resistance using series, parallel and series–parallel combinations;

Operation and use of potentiometers and rheostats;

Operation of Wheatstone Bridge.

2

1

 

(b) Resistor

Positive and negative temperature coefficient conductance;

Resistor colour code, values and tolerances, preferred values, wattage ratings;

Resistors in series and in parallel;

Fixed resistors, stability, tolerance and limitations, methods of construction;

Variable resistors, thermistors, voltage-dependent resistors;

Construction of potentiometers and rheostats;

Construction of Wheatstone Bridge.

1

3.8 Power

2

1

 

 

 

 

Power, work, and energy (kinetic and potential);

Dissipation of power by a resistor;

Power formula;

Calculations involving power, work, and energy.

3.9 Capacitance/Capacitor

2

1

 

 

 

 

 

 

 

Operation and function of a capacitor;

Factors that affect the capacitance area of plates, distance between plates, number of plates, dielectric and dielectric constant, working voltage, voltage rating;

Capacitor types, construction, and function;

Capacitor colour-coding;

Calculations of capacitance and voltage in series and in parallel circuits;

Exponential charge and discharge of a capacitor, time constants;

Testing of capacitors.

3.10 Magnetism

 

 

 

 

(a) Theory of magnetism;

Properties of a magnet;

Action of a magnet suspended in the Earth’s magnetic field;

Magnetisation and demagnetisation;

Magnetic shielding;

Various types of magnetic material;

Electromagnet construction and principles of operation;

Handclasp rules to determine magnetic field around current-carrying conductor.

2

1

 

(b) Magnetomotive force, field strength, magnetic flux density, permeability, hysteresis loop, retentivity, coercive force reluctance, saturation point, eddy currents;

Precautions for care and storage of magnets.

2

1

3.11 Inductance/Inductor

2

1

 

 

 

 

 

 

 

 

 

 

 

Faraday’s law;

Action of inducing a voltage in a conductor that moves in a magnetic field;

Induction principles;

Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of change of flux, number of conductor turns;

Mutual induction;

The effect that the rates of change of primary current and mutual inductance have on induced voltage;

Factors that affect mutual inductance: number of turns in the coil, physical size of the coil, permeability of the coil, position of coils with respect to each other;

Lenz’s law and polarity determining rules;

Back EMF, self-induction;

Saturation point;

Principal uses of inductors.

3.12 DC motor/generator theory

2

1

 

Basic motor and generator theory;

Construction and purpose of components in a DC generator;

 

 

 

 

 

 

Operation of and factors that affect the output and direction of the current in DC generators;

Operation of and factors that affect the output power, torque, speed, and direction of rotation of DC motors;

Series-wound, shunt-wound and compound motors;

Starter generator construction.

3.13 AC theory

1

2

1

 

 

 

 

Sinusoidal waveform: phase, period, frequency, cycle;

Instantaneous, average, root mean square, peak, peak-to-peak current values and calculations of these values in relation to voltage, current and power;

Triangular/Square waves;

Single-phase/Three-phase principles.

3.14 Resistive (R), capacitive (C) and inductive (L) circuits

2

1

 

 

 

 

Phase the relationship of voltage and current in L, C and R circuits, parallel, series and series–parallel;

Power dissipation in L, C and R circuits;

Impedance, phase angle, power factor and current calculations;

True power, apparent power, and reactive power calculations.

3.15 Transformers

2

1

 

 

 

 

 

 

 

 

Transformer construction principles and operation;

Transformer losses and methods for overcoming them;

Transformer action under load and no-load conditions;

Power transfer, efficiency, polarity markings;

Line and phase voltages and currents;

Power in a three-phase system;

Primary and secondary current, voltage, turn ratio, power, efficiency;

Auto-transformers.

3.16 Filters

1

 

Operation, application, and uses of the following filters: low pass, high pass, band pass, band stop.

3.17 AC generators

2

1

 

 

 

 

 

Rotation of loop in a magnetic field and waveform produced;

Operation and construction of revolving armature and revolving field type AC generators;

Single-phase, two-phase, and three-phase alternators;

Three-phase star and delta connection advantages, and uses;

Permanent magnet generators.

3.18 AC motors

2

1

 

 

 

Construction, principles of operation and characteristics of: AC synchronous and induction motors both single-phase and polyphase;

Methods of speed control and direction of rotation;

Methods of producing a rotating field: capacitor, shaded or split pole.

MODULE 4 — ELECTRONICS FUNDAMENTALS

 

 

MODULE 4 — ELECTRONICS FUNDAMENTALS

LEVEL

A1

A2

A3

A4

B1

B3

B2

B2L

4.1 Semiconductors

 

 

 

 4.1.1 Diodes

 

 

 

 

(a) Description and characteristics

Diode symbols;

Diode characteristics and properties;

Diodes in series and in parallel;

Materials, electron configuration, electrical properties;

P and N type materials: effects of impurities on conduction, majority and minority characters;

P–N junction in a semiconductor, development of a potential across a P–N junction in unbiased, forward-biased and reverse-biased conditions;

Diode parameters: peak inverse voltage, maximum forward current, temperature, frequency, leakage current, power dissipation;

Main characteristics and use of silicon-controlled rectifiers (thyristors), light-emitting diodes (LEDs), photo-conductive diodes, rectifier diodes.

2

2

 

(b) Operation and function

Operation and function of diodes in the following circuits: clippers, clampers, full- and half-wave rectifiers, bridge rectifiers, voltage doublers and triplers;

Detailed operation and characteristics of the following devices: silicon-controlled rectifier (thyristor), light-emitting diode (LED), Schottky diode, photo-conductive diode, varactor diode, varistor, rectifier diodes, Zener diode.

Functional testing of diodes.

2

 4.1.2 Transistors

 

 

 

 

(a) Description and characteristics

Transistor symbols;

Component description and orientation;

Transistor characteristics and properties.

1

2

 

(b) Construction and operation

Construction and operation of PNP and NPN transistors;

Base, collector and emitter configurations;

Testing of transistors;

Basic appreciation of other transistor types, including types of FET and their uses;

Application of transistors: amplifier classes (A, B, C);

Simple circuits including bias, decoupling, feedback and stabilisation;

Multistage circuit principles: cascades, push–pull, oscillators, multivibrators, flip-flop circuits;

Operation and amplifier stages connecting methods: resistive, capacitive, direct, inverting, non-inverting and adding.

2

 4.1.3 Integrated circuits

 

 

 

 

(a) Description and operation of logic circuits and linear circuits/operational amplifiers;

1

2

 

(b) Introduction to the operation and function of an operational amplifier used as: an integrator, a differentiator, a voltage follower, a comparator;

Advantages and disadvantages of positive and negative feedback.

2

4.2 Printed circuit boards

1

2

 

Description and use of printed circuit boards.

4.3 Servomechanisms

 

 

 

 

(a) Principles

Understanding of the following principles: open- and closed-loop systems, servomechanism, feedback, follow-up, null, overshoot, damping, deadband, hunting, proximity switches, analogue transducers, synchro systems and components, digital tachometers and encoders, inductance, and capacitance transmitters;

1

2

 

(b) Construction operation and use of the following synchro-system components: resolvers, differential, control and torque, E and I transformers, inductance transmitters, capacitance transmitters, synchronous transmitters;

Construction, operation and use of servomechanism and PID controller;

Fault-finding of servo defects, reversal of synchro leads, hunting.

2

MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS

 

 

MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS

LEVEL

A1

A2

A3

A4

B3

B1

B2

B2L

5.1 Electronic instrument systems

1

1

1

1

 

Typical arrangements of systems and cockpit layout of electronic instrument systems.

 

 

 

 

5.2 Numbering systems

1

2

 

 

Numbering systems: binary, octal, and hexadecimal;

Demonstration of conversions between the decimal and binary systems, octal and hexadecimal systems and vice versa.

 

 

 

 

5.3 Data conversion

1

2

 

 

Analogue data, Digital data;

Operation and application of analogue-to-digital and digital-to-analogue converters, inputs and outputs, limitations of various types.

 

 

 

 

5.4 Data buses

2

2

 

 

Operation of data buses in aircraft systems, including knowledge of ARINC and other specifications.

Aircraft network/Ethernet.

 

 

 

 

5.5 Logic circuits

 

 

 

 

 

(a) Identification of common logic gate symbols, tables and equivalent circuits;

Applications used for aircraft systems, schematic diagrams.

2

2

 

(b) Interpretation of logic diagrams.

2

5.6 Basic computer structure

 

 

 

 

 

(a) Computer terminology (including bit, byte, software, hardware, CPU, IC, and various memory devices such as RAM, ROM, PROM);

Computer technology (as applied in aircraft systems).

1

1

2

2

 

(b) Computer operation, layout, and interface of the major components in a microcomputer, including their associated bus systems;

Information contained in single- and multi-address instruction words;

Memory-associated terms;

Operation of typical memory devices;

Operation, advantages, and disadvantages of the various data storage systems.

2

5.7 Microprocessors

2

 

 

Functions performed and overall operation of a microprocessor;

Basic operation of each of the following microprocessor elements: control and processing unit, clock, register, arithmetic logic unit.

 

 

 

 

5.8 Integrated circuits

2

 

Operation and use of encoders and decoders;

 

 

 

 

 

Function of encoder types.

5.9 Multiplexing

2

 

Operation, application and identification in logic diagrams of multiplexers and demultiplexers.

 

 

 

5.10 Fibre optics

1

2

 

 

 

 

 

 

Advantages and disadvantages of fibre optic data transmission over electrical wire propagation;

Fibre optic data bus;

Fibre-optic-related terms;

Terminations;

Couplers, control terminals, remote terminals;

Application of fibre optics in aircraft systems.

 

 

 

 

5.11 Electronic displays

1

1

2

2

 

Principles of operation of common types of displays used in modern aircraft, including cathode-ray tubes (CRTs), light-emitting diodes (LEDs) and liquid crystal displays (LCDs).

 

 

 

 

5.12 Electrostatic-sensitive devices

1

1

2

2

 

 

Special handling of components sensitive to electrostatic discharges;

Awareness of risks and possible damage, component, and personnel antistatic protection devices.

 

 

 

 

5.13 Software management control

1

2

2

 

Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programs.

 

 

 

 

5.14 Electromagnetic environment

1

2

2

 

Influence of the following phenomena on maintenance practices for electronic systems:

EMC — Electromagnetic Compatibility,

EMI — Electromagnetic Interference,

HIRF — High-Intensity Radiated Field,

Lightning / lightning protection.

 

 

 

 

5.15 Typical electronic/digital aircraft systems

1

1

1

1

 

General arrangement of typical electronic/digital aircraft systems and associated BITE (Built-In Test Equipment), such as:

(a) 

ACARS — ARINC Communication and Addressing and Reporting System,

FBW — Fly-by-Wire,

FMS — flight management system,

IRS — inertial reference system;

(b) 

ECAM — electronic centralised aircraft monitoring,

EICAS — engine indication and crew alerting system,

EFIS — electronic flight instrument system,

GNSS — global navigation satellite system,

TCAS — traffic alert collision avoidance system,

Integrated Modular Avionics,

Cabin Systems,

Information Systems.

 

 

 

 

MODULE 6 — MATERIALS AND HARDWARE

 

 

MODULE 6 — MATERIALS AND HARDWARE

LEVEL

A1

A2

A3

A4

B1

B3

B2

B2L

6.1 Aircraft materials — ferrous

 

 

 

 

(a) Characteristics, properties and identification of common alloy steels used in aircraft;

Heat treatment and application of alloy steels.

1

2

1

 

(b) Testing of ferrous materials for hardness, tensile strength, fatigue strength and impact resistance.

1

1

 

(c) Repair and inspection procedures for ferrous materials, structures, and airframes.

2

1

6.2 Aircraft materials — non-ferrous

 

 

 

 

(a) Characteristics, properties and identification of common non-ferrous materials used in aircraft;

Heat treatment and application of non-ferrous materials.

1

2

1

 

(b) Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance.

1

1

 

(c) Repair and inspection procedures for non-ferrous materials, structures, and airframes.

2

1

6.3 Aircraft materials — composite and non-metallic

 

 

 

 6.3.1 Composite and non-metallic materials other than wood and fabric

 

 

 

 

(a) Characteristics, properties and identification of common composite and non-metallic materials, other than wood, used in aircraft;

Sealant and bonding agents.

1

2

2

 

(b) Detection of defects/deterioration in composite and non-metallic materials.

1

2

 

(c) Repair of and inspection procedures for composite and non-metallic materials, structures, and airframes.

2

1

 6.3.2 Wooden structures

1

1

 

 

 

 

 

 

Construction methods of wooden airframe structures;

Characteristics, properties and types of wood and glue used in aeroplanes;

Preservation and maintenance of wooden structures;

Types of defects in wood material and wooden structures;

Detection of defects in wooden structures;

Repair of wooden structures.

 6.3.3 Fabric covering

1

 

 

 

 

Characteristics, properties and types of fabrics used in aeroplanes;

Inspection methods for fabrics;

Types of defects in fabrics;

Repair of fabric covering.

6.4 Corrosion

 

 

 

 

(a) Chemical fundamentals;

Formation by galvanic action process, microbiological contamination, mechanical stress.

1

1

1

 

(b) Types of corrosion and their identification;

Causes of corrosion;

Material types, and their susceptibility to corrosion.

2

3

2

6.5 Fasteners

 

 

 

 6.5.1 Screw threads

2

2

2

 

Screw nomenclature;

Thread forms, dimensions and tolerances for standard threads used in aircraft;

 

Measuring screw threads.

 6.5.2 Bolts, studs, and screws

2

2

2

 

 

 

 

 

Bolt types: specification, identification and marking of aircraft bolts, international standards;

Nuts: self-locking, anchor, standard types;

Machine screws: aircraft specifications;

Studs: types and uses, insertion, and removal;

Self-tapping screws, dowels.

 6.5.3 Locking devices

2

2

2

 

Tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quick-release fasteners, keys, circlips, cotter pins.

 6.5.4 Aircraft rivets

1

2

1

 

Types of solid and blind rivets: specifications and identification, heat treatment.

6.6 Pipes and unions

 

 

 

 

(a) Identification and types of rigid and flexible pipes and their connectors used in aircraft;

2

2

2

 

(b) Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system pipes.

2

2

1

6.7 Springs

2

1

 

Types of springs, materials, characteristics, and applications.

6.8 Bearings

1

2

2

 

 

Purpose of bearings, loads, material, construction;

Types of bearings and their application.

6.9 Transmissions

1

2

2

 

 

 

Gear types and their application;

Gear ratios, reduction and multiplication gear systems, driven and driving gears, idler gears, mesh patterns;

Belts and pulleys, chains and sprockets.

6.10 Control cables

1

2

1

 

 

 

 

 

Types of cables;

End fittings, turnbuckles and compensation devices;

Pulleys and cable system components;

Bowden cables;

Aircraft flexible control systems.

6.11 Electrical cables and connectors

1

2

2

 

 

 

 

Cable types, construction and characteristics;

High-tension and coaxial cables;

Crimping;

Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes.

MODULE 7 — MAINTENANCE PRACTICES

 

 

MODULE 7 — MAINTENANCE PRACTICES

LEVEL

A1

A2

A3

A4

B1

B3

B2

B2L

7.1 Safety precautions — aircraft and workshop

3

3

3

 

 

Aspects of safe working practices including precautions to be taken when working with electricity, gases (especially oxygen), oils, and chemicals.

Fuel tank safety and fuel tank entry procedures and precautions. Awareness and precautions regarding aircraft equipped with ballistic recovery systems. Also, instructions for the remedial action to be taken in the event of a fire or another accident with one or more of these hazards, including information on fire-extinguishing agents.

7.2 Workshop practices

3

3

3

 

 

 

Care of tools, control of tools, use of workshop materials;

Dimensions, allowances and tolerances, workmanship standards;

Calibration of tools and equipment, calibration standards.

7.3 Tools

3

3

3

 

 

 

 

 

Common hand-tool types;

Common power-tool types;

Operation and use of precision-measuring tools;

Lubrication equipment and methods;

Operation, function, and use of electrical general test equipment.

7.4 (Reserved)

 

 

 

 

 

7.5 Engineering drawings, diagrams, and standards

1

2

2

 

 

 

 

 

 

Drawing types and diagrams, their symbols, dimensions, tolerances and projections;

Identification of title block information;

Microfilm, microfiche, and computerised presentations;

Specification 100 of the Air Transport Association (ATA) of America;

Aeronautical and other applicable standards including ISO, AN, MS, NAS and MIL;

Wiring diagrams and schematic diagrams.

7.6 Fits and clearances

1

2

1

 

 

 

 

 

Drill sizes for bolt holes, classes of fits;

Common system for fits and clearances;

Schedule of fits and clearances for aircraft and engines;

Limits for bow, twist and wear;

Standard methods for checking shafts, bearings, and other parts.

7.7 Electrical wiring interconnection system (EWIS)

1

3

3

 

Continuity, insulation and bonding techniques and testing;

Use of crimp tools: hand and hydraulic operated;

Testing of crimp joints;

Connector pin removal and insertion;

Coaxial cables: testing and installation precautions;

Identification of wire types, their inspection criteria and damage tolerance;

Wiring protection techniques: cable looming and loom support, cable clamps, protective sleeving techniques including heat shrink wrapping, shielding;

High-Intensity Radiated Fields (HIRF) and protection principles;

Soldering of electrical wires, EWIS installations, inspection, repair, maintenance, and cleanliness standards.

7.8 Riveting

1

2

 

 

 

Riveted joints, rivet spacing and pitch;

Tools used for riveting and dimpling;

Inspection of riveted joints.

7.9 Pipes and hoses

1

2

 

 

 

Bending and belling/flaring aircraft pipes;

Inspection and testing of aircraft pipes and hoses;

Installation and clamping of pipes.

7.10 Springs

1

2

 

Inspection and testing of springs.

7.11 Bearings

1

2

 

 

 

Testing, cleaning and inspection of bearings;

Lubrication requirements for bearings;

Defects in bearings and their causes.

7.12 Transmissions

1

2

 

 

 

Inspection of gears, backlash;

Inspection of belts and pulleys, chains and sprockets;

Inspection of screw jacks, lever devices, push–pull rod systems.

7.13 Control cables

1

2

 

 

 

Swaging of end fittings;

Inspection and testing of control cables;

Bowden cables; aircraft flexible control systems.

7.14 Material handling

 

 

 

 7.14.1 Sheet metal

2

 

 

 

Marking out and calculation of bend allowance;

Sheet metal working, including bending and forming;

Inspection of sheet metal work.

 7.14.2 Composite and non-metallic

2

 

 

 

Bonding practices;

Environmental conditions;

Inspection methods.

7.14.3 Additive manufacturing

1

1

1

 

 

 

Common additive manufacturing techniques and their influence on the mechanical properties of the finished part;

Inspection of additive manufactured parts and common production failures.

7.15 (Reserved)

 

 

 

7.16 Aircraft weight and balance

 

 

 

 

(a) Calculation of centre-of-gravity / balance limits: use of relevant documents.

2

2

 

(b) Preparation of aircraft for weighing;

Aircraft weighing.

2

7.17 Aircraft handling and storage

2

2

2

 

 

 

 

 

 

 

Aircraft taxiing/towing and associated safety precautions;

Aircraft jacking, chocking, securing and associated safety precautions;

Aircraft storage methods;

Refuelling/defuelling procedures;

De-icing/anti-icing procedures;

Electrical, hydraulic, and pneumatic ground supplies;

Effects of environmental conditions on aircraft handling and operation.

7.18 Disassembly, inspection, repair, and assembly techniques

 

 

 

 

(a) Types of defects and visual inspection techniques;

Corrosion removal, assessment and reprotection;

2

3

3

 

(b) General repair methods, structural repair manual;

Ageing, fatigue, and corrosion control programmes;

2

 

(c) Non-destructive inspection techniques including penetrant, radiographic, eddy current, magnetic particle, ultrasonic and borescope inspections; including practical training in colour contrast penetrant inspection;

2

1

 

(d) Disassembly and reassembly techniques;

2

2

2

 

(e) Troubleshooting techniques.

2

2

7.19 Abnormal events

 

 

 

 

(a) Inspections following lightning strikes and HIRF penetration;

2

2

2

 

(b) Inspections following abnormal events such as heavy landings and flight through turbulence.

2

2

7.20 Maintenance procedures

1

2

2

 

 

 

 

 

 

 

 

Maintenance planning;

Modification procedures;

Stores procedures;

Certification/release procedures;

Interface with aircraft operation;

Maintenance Inspection / Quality Control / Quality Assurance;

Additional maintenance procedures;

Control of life-limited components.

7.21 Documentation and communication

1

2

2

 

 

Documentation: elements and criteria for writing work reports, troubleshooting reports, and shift handover instructions.

Communication: clear, comprehensive, and concise.

MODULE 8 — BASIC AERODYNAMICS

MODULE 8 — BASIC AERODYNAMICS

LEVEL

A1

A2

A3

A4

B3

B1

B2

B2L

8.1 Physics of the atmosphere

1

2

 

International Standard Atmosphere (ISA), and its application to aerodynamics.

8.2 Aerodynamics

1

2

 

 

 

 

 

 

Airflow around a body;

Boundary layer, laminar and turbulent flow, free stream flow, relative airflow, upwash and downwash, vortices, stagnation;

The terms: camber, chord, mean aerodynamic chord, profile (parasite) drag, induced drag, centre of pressure, angle of attack, wash-in and wash-out, fineness ratio, wing shape and aspect ratio;

Thrust, weight, aerodynamic resultant;

Generation of lift and drag angle of attack, lift coefficient, drag coefficient, polar curve, stall;

Aerofoil contamination including ice, snow, and frost.

8.3 Theory of flight

1

2

 

 

 

 

 

 

Relationship between lift, weight, thrust and drag;

Glide ratio;

Steady-state flights, performance;

Theory of the turn;

Influence of load factor: stall, flight envelope, and structural limitations;

Lift augmentation.

8.4 High-speed airflow

1

2

 

Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number, compressibility buffet, shock wave, aerodynamic heating, area rule;

Factors that affect airflow in engine intakes of high-speed aircraft;

Effects of sweepback on critical Mach number.

 

 

8.5 Flight stability and dynamics

1

2

 

Longitudinal, lateral, and directional stability (active and passive).

MODULE 9 — HUMAN FACTORS

MODULE 9 — HUMAN FACTORS

LEVEL

ALL

9.1 General

2

 

 

 

The need to take human factors into account when performing maintenance;

Incidents attributable to human factors/human error;

Murphy’s law.

9.2 Human performance and limitations

2

 

 

 

 

 

 

Vision;

Hearing;

Information processing;

Attention and perception;

Memory;

Claustrophobia and physical access.

9.3 Social psychology

1

 

 

 

 

 

 

Accountability and responsibility: individual and group;

Motivation and demotivation;

Peer pressure;

Cultural issues;

Teamwork;

Management, supervision, and leadership.

9.4 Factors that affect performance

2

 

 

 

 

 

 

Fitness/health;

Stress: domestic and work related;

Time pressure and deadlines;

Workload: overload, underload, and workload management;

Sleep and fatigue, shift work;

Alcohol, medication, drug abuse;

Lack of manpower.

9.5 Physical environment

1

 

 

 

 

 

Noise and fumes;

Illumination;

Climate and temperature;

Motion and vibration;

Working environment;

Situational awareness.

9.6 Tasks

1

 

 

 

 

Physical work;

Repetitive tasks, complacency;

Visual inspection;

Complex systems;

Critical maintenance tasks and error-capturing methods;

Technical documentation: access, use, and quality.

9.7 Communication

2

 

 

 

 

Within and between teams;

Work logging and recording;

Shift handover;

Keeping up to date, currency;

Dissemination of information.

9.8 Human error

2

 

Error models and theories;

 

Types of error in maintenance tasks;

Implications of errors (e.g. accidents);

Organisational errors;

Avoiding and managing errors.

9.9 Safety management

2

 

 

Risk management;

Occurrence reporting;

Safety culture

Just culture;

Identifying, avoiding, and reporting hazards;

Organisational human-factors programme: professionalism and integrity, error-provoking behaviour, reporting errors, disciplinary policy, error investigation, action to address problems, feedback, assertiveness;

Dealing with emergencies.

9.10 The ‘Dirty Dozen’ and risk-mitigation

2

 

 

The ‘Dirty Dozen’: the twelve most common human-factors errors in maintenance:

Lack of communication,

Lack of teamwork,

Lack of assertiveness,

Complacency,

Fatigue,

Stress,

Lack of knowledge,

Lack of resources,

Lack of awareness,

Distraction,

Pressure,

Norms.

Risk-mitigation methods.

MODULE 10 — AVIATION LEGISLATION

 

 

MODULE 10 — AVIATION LEGISLATION

LEVEL

A1

A2

A3

A4

B1

B2

B2L

B3

10.1 Regulatory framework

1

1

 

Role of:

 the International Civil Aviation Organization (ICAO);

 the European Commission (EC);

 the European Union Aviation Safety Agency (EASA);

 the European Union Member States and national aviation authorities;

 the bilateral agreements concluded by the European Commission;

 Regulation (EU) 2018/1139 (the Basic Regulation) and its implementing acts:

Regulations (EU) No 748/2012 (Initial Airworthiness) and (EU) No 1321/2014 (Continuing Airworthiness);

 the relationship between regulations (hard law) and AMC, GM and CSs (soft law);

 occurrence reporting according to Regulation (EU) No 376/2014;

 the relationship between the various annexes (parts) relating to Initial and

Continuing Airworthiness (such as Part 21, Part-M, Part-145, Part-66, Part-147, Part-T, Part-ML, Part-CAMO, and Part-CAO) and Regulations (EU) No 965/2012 (the Air Operations Regulation) and (EU) No 1178/2011 (the Air Crew Regulation).

10.2 Certifying staff — maintenance

2

2

 

Deep understanding of Part-66 maintenance licences with the associated privileges and authorisations, and how to exercise them properly for the different aircraft categories.

10.3 Approved maintenance organisations

2

2

 

General understanding of Part-145 and Part-CAO.

10.4 Independent certifying staff

3

 

Privileges, responsibilities, record-keeping, limitations, and oversight according to Part-M, Part-66 and Part-ML.

10.5 Air operations

1

1

 

General understanding of Regulation (EU) No 965/2012 (the Air Operations Regulation);

Differences between commercial and non-commercial air operations, and their influence on aircraft maintenance;

Air Operator Certificates (AOCs) and self-declaration authorisations;

Air operator responsibilities, in particular regarding continuing airworthiness and maintenance;

Specialised operations / specific approvals: ETOPS, CAT I/II/III, and BRNAV.

 

Minimum Equipment List (MEL) and Configuration Deviation List (CDL);

Aircraft placarding and markings;

Documents to be carried on board:

 Certificate of Airworthiness / Restricted Certificate of Airworthiness;

 Airworthiness Review Certificate;

 Permit to Fly;

 Certificate of Registration;

 Noise Certificate;

 Weight and Balance report;

 Radio Station Licence.

 

 

10.6 Certification of aircraft, parts, and appliances

2

2

 

Basic understanding of Part 21 and of the following EASA certification specifications:
CS-22, CS-23, CS-25, CS-27, CS-29, and CS-STAN.

 

 

10.7 Continuing airworthiness

2

2

 

General understanding of the Part 21 requirements on continuing airworthiness;

General understanding of Part-M, Part-ML and Part-CAMO;

Aircraft Maintenance Programme.

10.8 Oversight principles in continuing airworthiness

1

1

10.9 Maintenance and certification beyond current EU regulations (if not superseded by EU requirements)

1

 

Maintenance of European Union aircraft that are not within the scope of Regulation (EU) 2018/1139 (Annex I aircraft);

European military airworthiness requirement (EMAR) 66 licence;

Applicable national and international requirements for component maintenance, welding, painting, NDT, etc. (if not superseded by EU requirements).

 

 

10.10 Cybersecurity in aviation maintenance

Regulation on the introduction of organisation requirements for the management of information security risks related to aeronautical information systems used in civil aviation.

1

1

MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

A1

A2

B1.1

B1.2

B3

11.1 Theory of flight

 

 

 

 

 

(a)  Aeroplane aerodynamics and flight controls

1

 

1

2

2

1

 

 

 

 

 

 

 

Operation and effect of:

 roll control: ailerons and spoilers;

 pitch control: elevators, stabilators, variable incidence stabilisers and canards;

 yaw control, rudder limiters;

 elevons, ruddervators;

 high-lift devices, slots, slats, flaps, flaperons;

 drag-inducing devices, spoilers, lift dumpers, speed brakes;

 trim tabs, servo tabs, control surface bias.

(b)  Aeroplane: other aerodynamic devices

1

1

2

2

1

 

Operation and effect of:

 balance and antibalance (leading) tabs;

 spring tabs, mass balance, aerodynamic balance panels;

 mass balance, aerodynamic balance panels;

 effects of wing fences, saw tooth leading edges;

 boundary layer control using vortex generators, stall wedges or leading-edge devices.

 

 

 

 

 

11.2 Airframe structures (ATA 51)

 

 

 

 

 

 

 

(a) General concepts:

 Zonal and station identification systems;

 Electrical bonding;

 Lightning strike protection provisions.

2

2

2

2

2

(b) Airworthiness requirements for structural strength:

 Structural classification: primary, secondary, and tertiary;

 Fail-safe, safe-life, damage-tolerance concepts;

 Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;

 Drains and ventilation provisions;

 System installation provisions.

2

2

2

2

2

 

(c) Construction methods

 Stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, skinning, anticorrosive protection, wing, empennage and engine attachments;

 Structure assembly techniques: riveting, bolting, bonding;

 Methods of surface protection, such as chromating, anodising, painting;

 Surface cleaning;

 Airframe symmetry: methods of alignment and symmetry checks.

1

1

2

2

2

11.3 Airframe structures — aeroplanes

 

 

 

 

 

 11.3.1 Fuselage, doors, windows (ATA 52/53/56)

1

1

2

2

1

 

 

 

 

 

(a) Construction principles

 Construction and pressurisation sealing;

 Wing, stabiliser, pylon, and undercarriage attachments;

 Seat installation and cargo loading system;

 Doors and emergency exits: construction, mechanisms, operation and safety devices;

 Windows and windscreen construction and mechanisms.

 

(b)  Airborne towing devices (glider, banner, target).

1

1

1

1

1

 

(c)  Doors

 Doors and emergency exits: safety devices;

 Cargo loading system.

1

1

2

1

 11.3.2 Wings (ATA 57)

1

1

2

2

1

 

 

 

Construction;

Fuel storage;

Landing gear, pylon, control surface and high lift/drag attachments.

 11.3.3 Stabilisers (ATA 55)

1

1

2

2

1

 

 

Construction;

Control surface attachment.

 11.3.4 Flight control surfaces (ATA 55/57)

1

1

2

2

1

 

 

Construction and attachments;

Balancing — mass and aerodynamics.

 11.3.5 Nacelles/pylons (ATA 54)

1

1

2

2

1

 

Nacelles/Pylons:

— Construction,

— Firewalls,

— Engine mounts.

11.4 Air conditioning and cabin pressurisation (ATA 21)

 

 

 

 

 

(a) Pressurisation

Pressurisation systems;

Cabin pressure controllers, control, and safety valves;

Control and indication.

1

1

3

3

(b) Air supply

Sources of air supply including engine bleed, APU and ground cart;

Distribution systems.

1

-

3

-

(c) Air conditioning

Air-conditioning systems;

Air cycle and vapour cycle machines;

Flow, temperature and humidity control system;

Control and indication control valves.

1

3

-

(d) Safety and warning devices

Protection and warning devices.

1

1

3

3

(e) Heating and ventilation systems.

1

-

3

1

11.5 Instruments / avionics systems

 

 

 

 

 

 11.5.1 Instrument systems (ATA 31)

1

1

2

2

2

 

Pitot-static:

Airspeed indicators,

Vertical speed indicators,

Altimeters;

Gyroscopic:

Gyroscopic principles,

Artificial horizons,

Attitude directors,

Direction indicators,

Horizontal situation indicators (HSI),

Slip indicators, Turn indicators, Turn coordinators;

Compass systems: systems, direct reading, remote reading,

Stall-warning systems and angle-of-attack indicating systems,

Glass cockpit,

Indications of other aircraft systems.

 11.5.2 Avionics systems

1

 

1

1

1

1

 

Fundamentals of system layouts and operation of:

Autoflight (ATA 22);

Communication systems (ATA 23):

 Very High Frequency (VHF) communications,

 High Frequency (HF) communications,

 Satellite Communications (SATCOM),

 Controller–pilot data link communications (CPDLC),

 Audio systems,

 Emergency Locator Transmitters (ELTs),

 Cockpit Voice Recorder (CVR);

Navigation systems (ATA 34):

 Very high frequency omnidirectional range (VOR),

 Automatic direction finder (ADF),

 Instrument landing system (ILS),

 Microwave landing system (MLS),

 Flight director systems (FDSs), distance-measuring equipment (DME),

 Area navigation (RNAV) systems,

 Flight management systems (FMSs),

 Satellite navigation systems,

 Air traffic control transponder, secondary surveillance radar,

 Traffic alert and collision avoidance system (TCAS),

 Weather avoidance radar,

 Radio altimeter,

 Inertial navigation system (INS),

 ARINC (Aeronautical Radio Incorporated) communication and reporting.

Types and uses of avionics general test equipment.

11.6 Electrical power (ATA 24)

1

1

3

3

3

 

 Installation and operation of batteries;

 DC power generation;

 AC power generation;

 Emergency power generation;

 Voltage regulation;

 Power distribution;

 Inverters, transformers, rectifiers;

 Circuit protection;

 External/ground power.

11.7 Equipment and furnishings (ATA 25)

 

 

 

 

 

 

(a) Emergency equipment:

Emergency equipment requirements.

2

2

2

2

2

 

(b) Cabin and cargo layout:

 Seats, harnesses, and belts;

 Cabin layout;

 Equipment layout;

 Cabin furnishing installation;

 Galley installation;

 Cargo handling and retention equipment;

 Airstairs.

1

1

1

1

11.8 Fire protection (ATA 26)

 

 

 

 

 

 

(a) Fire and smoke detection system, and fire-extinguishing systems:

 Fire and smoke detection and warning systems;

 Fire-extinguishing systems;

 System tests.

1

1

1

1

 

(b) Portable fire extinguisher.

1

1

1

1

1

11.9 Flight controls (ATA 27)

 

 

 

 

 

 

(a) Primary and secondary flight controls:

 Primary controls: aileron, elevator, rudder, spoiler;

 Trim control, trim tabs;

 High-lift devices;

 System operation: manual;

 Gust locks and gust lock systems;

 Artificial feel, yaw damper, Mach trim, rudder limiter;

 Stall-warning systems.

1

1

3

3

2

 

(b) Actuation and protection:

 Active load control;

 Lift dump, speed brakes;

 Hydraulic, pneumatic systems;

 Stall-protection systems.

1

3

 

(c) System operation:

Electrical systems, fly-by-wire systems.

1

3

 

(d) Balancing and rigging.

1

1

3

3

2

11.10 Fuel systems (ATA 28, ATA 47)

 

 

 

 

 

 

(a) Systems:

 System layout;

 Fuel tanks;

 Supply systems.

1

1

3

3

1

 

(b) Fuel handling:

 Cross-feed and transfer;

 Refuelling and defuelling.

1

1

3

3

1

 

(c) Indication and warnings.

1

1

3

3

1

 

(d) Special systems:

 Dumping, venting, and draining;

 Inert gas systems.

1

3

 

(e) Balancing:

Longitudinal balance fuel systems.

1

3

11.11 Hydraulic power (ATA 29)

 

 

 

 

 

 

(a) System description:

System layout;

Hydraulic fluids;

Hydraulic reservoirs and accumulators;

Filters;

Power distribution.

1

1

3

3

2

 

(b) System operation (1):

Pressure generation: electric and mechanical;

Pressure control;

Indication and warning systems;

Servicing.

1

1

3

3

2

 

(c) System operation (2):

Pressure generation: pneumatic;

Emergency pressure generation;

Interface with other systems.

1

3

11.12 Ice and rain protection (ATA 30)

 

 

 

 

 

 

(a) Principles:

Ice formation, classification, and detection.

1

1

3

3

1

 

(b) De-icing:

De-icing systems: electrical, hot-air, pneumatic, chemical;

Probe and drain heating.

1

1

3

3

1

 

(c) Anti-icing:

Anti-icing systems: electrical, hot-air, chemical.

1

3

 

(d) Wipers:

Wiper systems.

1

1

3

3

1

 

(e) Rain-repellent systems.

1

3

11.13 Landing gear (ATA 32)

 

2

 

2

 

3

 

3

 

2

 

(a) Description:

Construction, shock absorbing;

Tyres.

 

(b) Systems:

Extension and retraction systems: normal and emergency;

Indications and warnings;

Wheels, brakes, antiskid, and autobraking;

Steering.

2

2

3

3

2

 

(c) Air–ground sensing.

2

3

 

(d) Tail protection:

Skids.

2

2

3

3

2

11.14 Lights (ATA 33)

2

2

3

3

2

 

 

 

External: navigation, anticollision, landing, taxiing, ice;

Internal: cabin, cockpit, cargo;

Emergency.

11.15 Oxygen (ATA 35)

1

1

3

3

2

 

 

 

 

System layout: cockpit, cabin;

Sources, storage, charging and distribution;

Supply regulation;

Indications and warnings.

11.16 Pneumatic / vacuum (ATA 36)

 

1

 

1

 

3

 

3

 

2

 

(a) Systems:

System layout;

Sources: engine / APU (Auxiliary Power Unit), compressors, reservoirs, ground supply;

Pressure control;

Distribution;

Indications and warnings;

Interface with other systems.

 

(b) Pumps:

Pressure and vacuum pumps.

1

1

3

3

2

11.17 Water / waste (ATA 38)

 

 

 

 

 

 

(a) Systems:

Water system layout, supply, distribution, servicing and draining;

Toilet system layout, flushing and servicing.

2

2

3

3

2

 

(b) Corrosion:

Corrosion aspects.

2

2

3

3

2

11.18 Onboard maintenance systems (ATA 45)

1

2

 

 

 

 

 

Central maintenance computers;

Data-loading system;

Electronic library system;

Printing systems;

Structure monitoring (damage-tolerance monitoring).

11.19 Integrated modular avionics (IMA) (ATA 42)

1

2

 

(a) Overall system description and theory:

Core system; network components;

Functions that may be typically integrated in the integrated modular avionics (IMA) modules are, among others:

 

 

Bleed management, air pressure control, air ventilation and control, avionics and cockpit ventilation control, temperature control, air traffic communication, avionics communication router, electrical load management, circuit breaker monitoring, electrical system BITE, fuel management, braking control, steering control, landing gear extension and retraction, tyre pressure indication, oleo pressure indication, brake temperature monitoring, etc.

 

(b) Typical system layout.

1

2

11.20 Cabin systems (ATA 44)

1

 

 

2

 

 

System architecture, operation, and control of systems for:

 passenger in-flight entertainment;

 communication within the aircraft (Cabin intercommunication data system (CIDS);

 communication between the aircraft cabin and ground stations;

 including voice, data, music, and video transmission.

CIDS interface between cockpit/cabin crew and cabin systems.

Data exchange between the different related line replaceable units (LRUs).

Flight attendant panels (FAPs).

Cabin network server (CNS) and interfaces with the following systems:

 Data/radio communication;

 Cabin core system (CCS);

 In-flight entertainment system (IFES);

 External communication system (ECS);

 Cabin mass memory system (CMMS);

 Cabin monitoring system (CMS);

 Miscellaneous cabin systems (MCSs); and

 Other systems.

Cabin network server (CNS) hosting functions:

 Access to predeparture/departure reports;

 Email/intranet/internet access; passenger database;

 In-flight entertainment system;

 External communication system;

 Cabin mass memory system;

 Cabin monitoring system;

 Miscellaneous cabin system.

11.21 Information systems (ATA 46)

1

2

 

 

 

 

 

 

 

System architecture, operation, and control of:

 Storage and electronic library;

 Updating;

 Retrieving of digital information;

 Air traffic and information management systems (ATIMS) and network server systems;

 Aircraft general information system;

 Flight deck information system;

 Maintenance information system;

 Passenger cabin information system;

 Miscellaneous information systems;

 Other linked systems.

MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

 

MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

A3

A4

B1.3

B1.4

12.1 Theory of flight — rotary wing aerodynamics

1

2

 

Terminology;

Effects of gyroscopic precession;

Torque reaction and directional control;

Dissymmetry of lift, blade tip stall;

Translating tendency and its correction;

Coriolis effect and compensation;

Vortex ring state, power setting, overpitching;

Auto-rotation;

Ground effect.

12.2 Flight control systems (ATA 67)

2

3

 

Cyclic control;

Collective control;

Swashplate;

Yaw control: antitorque control, tail rotor, bleed air;

Main-rotor head: design and operation features;

Blade dampers: function and construction;

Rotor blades: main- and tail-rotor blade construction and attachment;

Trim control, fixed and adjustable stabilisers;

System operation: manual, hydraulic, electrical, fly-by-wire;

Artificial feel;

Balancing and rigging.

12.3 Blade tracking and vibration analysis (ATA 18)

1

3

 

 

Rotor alignment;

Main-rotor and tail-rotor tracking;

Static and dynamic balancing;

Vibration types, and vibration reduction methods;

Ground resonance.

12.4 Transmission

1

3

 

 

 

Gear boxes, main and tail rotors;

Clutches, free wheel units and rotor brake;

Tail-rotor drive shafts, flexible couplings, bearings, vibration dampers and bearing hangers.

12.5 Airframe structures

 

 

 

(a) General concept

Airworthiness requirements for structural strength;

Structural classification: primary, secondary, tertiary;

Fail-safe, safe-life, damage-tolerance concepts;

Zonal and station identification systems;

Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;

Drains and ventilation provisions;

System installation provisions;

Lightning strike protection provisions.

2

2

 

(b) Construction methods for the principal elements

Stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, skinning and anticorrosive protection;

Pylon, stabiliser and undercarriage attachments;

Seat installation;

Doors: construction, mechanisms, operation, and safety devices;

Windows and windscreen construction;

Fuel storage;

Firewalls;

Engine mounts;

Structure assembly techniques: riveting, bolting, bonding;

Methods for surface protection, such as chromating, anodising, painting;

Surface cleaning;

Airframe symmetry: methods for alignment and symmetry checks.

1

2

12.6 Air conditioning (ATA 21)

 

 

 12.6.1 Air supply

1

2

 

Sources of air supply, including engine bleed and ground cart.

 12.6.2 Air conditioning

1

3

 

Air-conditioning systems;

Distribution systems;

Flow and temperature control systems;

Protection and warning devices.

12.7 Instruments / avionics systems

 

 

 12.7.1 Instrument systems (ATA 31)

1

2

 

Pitot-static: altimeter, airspeed indicator, vertical speed indicator;

Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator;

Compasses: direct reading, remote reading;

Vibration indicating systems / health and usage monitoring systems (HUMSs);

Glass cockpit;

Indications of other aircraft systems.

 12.7.2 Avionics systems

1

1

 

Fundamentals of system layouts and operation of:

Autoflight (ATA 22);

Communications (ATA 23):

 Very high frequency (VHF) communications,

 High-frequency (HF) communications,

 Satellite communications (SATCOM),

 Controller–pilot data link communications (CPDLC),

 Audio systems,

 Emergency locator transmitters (ELTs),

 Cockpit voice recorder (CVR);

Navigation systems (ATA 34):

 Very high frequency omnidirectional range (VOR),

 Automatic direction finding (ADF),

 Instrument landing system (ILS),

 Microwave landing system (MLS),

 Flight director systems (FDSs), distance-measuring equipment (DME),

 Area navigation (RNAV) systems,

 Flight management systems (FMSs),

 Satellite navigation systems,

 Inertial navigation system (INS),

 Air traffic control transponder, secondary surveillance radar,

 Traffic alert and collision avoidance system (TCAS),

 Weather avoidance radar,

 Radio altimeter,

 ARINC communication and reporting.

Types and uses of general test equipment for avionics.

12.8 Electric power (ATA 24)

1

3

 

Installation and operation of batteries;

DC power generation, AC power generation;

Emergency power generation;

Voltage regulation, circuit protection;

Power distribution;

Inverters, transformers, rectifiers;

External/Ground power.

12.9 Equipment and furnishings (ATA 25)

 

 

 

(a) Emergency equipment requirements;

Seats, harnesses, and belts;

Lifting systems.

2

2

 

(b) Emergency flotation systems;

Cabin layout, cargo retention;

Equipment layout;

Cabin furnishing installation.

1

1

12.10 Fire protection (ATA 26)

1

3

 

(a) Fire and smoke detection and warning systems;

Fire-extinguishing systems;

System tests.

 

(b) Portable fire extinguishers.

1

1

12.11 Fuel systems (ATA 28)

1

3

 

System layout;

Fuel tanks;

Supply systems;

Dumping, venting, and draining;

Cross-feed and transfer;

Indications and warnings;

Refuelling and defuelling.

12.12 Hydraulic power (ATA 29)

1

3

 

System layout;

Hydraulic fluids;

Hydraulic reservoirs and accumulators;

Pressure generation: electric, mechanical, pneumatic;

Emergency pressure generation;

Filters;

Pressure control;

Power distribution;

Indication and warning systems;

Interface with other systems;

Servicing.

12.13 Ice and rain protection (ATA 30)

1

3

 

Ice formation, classification, and detection;

Anti-icing and de-icing systems: electrical, hot-air, and chemical;

Rain repellent and removal;

Probe and drain heating;

Wiper system.

12.14 Landing gear (ATA 32)

 

2

 

3

 

(a) System description and operation:

Construction, shock absorbing;

Extension and retraction systems: normal and emergency;

Wheels, tyres, brakes;

Steering;

Skids, floats.

 

(b) Sensors:

Indications and warning;

Air–ground sensing.

2

3

12.15 Lights (ATA 33)

2

3

 

External: navigation, landing, taxiing;

Internal: cabin, cockpit, cargo;

Emergency.

12.16 (Reserved)

 

 

 

 

12.17 Integrated modular avionics (IMA) (ATA 42)

1

2

 

(a) Overall system description and theory

Functions that may be typically integrated in the integrated modular avionics (IMA) modules:

Bleed management, air pressure control, air ventilation and control, avionics and cockpit ventilation control, temperature control, air traffic communication, avionics communication router, electrical load management, circuit breaker monitoring, electrical system BITE, fuel management, steering control, landing gear extension and retraction, tyre pressure indication, oleo pressure indication, brake temperature monitoring, etc.;

Core System;

Network Components.

 

(b) Typical system layouts.

1

2

12.18 Onboard maintenance systems (ATA 45)

1

2

 

Central maintenance computers;

Data-loading system;

Electronic library system.

12.19 Information systems (ATA 46)

1

2

 

The units and components which furnish a means of storing, updating, and retrieving digital information traditionally provided on paper, microfilm or microfiche. They include units that are dedicated to the information storage and retrieval function, such as the electronic library mass storage and controller. They do not include units or components installed for other uses and shared with other systems, such as flight deck printer or general-use display.

Typical examples include air traffic and information management systems and network server systems.

Aircraft general information system.

Flight deck information system.

Maintenance information system.

Miscellaneous information system.

MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

C/N: Communication and Navigation; Ins.: Instruments; A/F: Autoflight; Sur.: Surveillance; A/S: Airframe and Systems

MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

B2

B2L Basic

B2L

C/N

B2L

Ins.

B2L

A/F

B2L

Sur.

B2L

A/S

13.1 Theory of flight

 

 

 

 

 

 

 

 

(a) Aeroplane aerodynamics and flight controls

Operation and effect of:

 roll control: ailerons and spoilers;

 pitch control: elevators, stabilators, variable incidence stabilisers and canards; and

 yaw control: rudder limiters;

 control using elevons, ruddervators;

 high-lift devices: slots, slats, flaps;

 drag-inducing devices: spoilers, lift dumpers, speed brakes;

 trim tabs, servo tabs, and control surface bias.

1

 

1

 

(b) Rotary wing aerodynamics

Terminology;

Operation and effect of cyclic, collective, and antitorque controls.

1

1

13.2 Structures — general concepts

 

 

 

 

 

 

 

 

(a) General concepts;

Zonal and station identification systems;

Electrical bonding;

Lightning strike protection provisions.

2

2

 

(b) Fundamentals of structural systems.

1

1

13.3 Autoflight (ATA 22)

 

 

 

 

 

 

 

 

(a) Fundamentals of automatic flight control:

 Working principles and current terminology;

 Command signal processing;

 Modes of operation: roll, pitch, and yaw channels;

 Yaw dampers;

 Stability augmentation system in helicopters;

 Automatic trim control;

 Autopilot navigation aids interface.

3

3

 

(b) Autothrottle systems and automatic landing   systems:

 Principles and categories;

 Modes of operation;

 Approach;

 Glideslope;

 Land, go-around;

 System monitors and failure conditions.

3

3

13.4 Communication/navigation (ATA 23/34)

 

 

 

 

 

 

 

 

(a) Fundamentals of communication and navigation systems:

 Radio wave propagation, antennas, transmission lines, communication, receiver, and transmitter;

Working principles of the following systems:

 Very high frequency (VHF) communications;

 High-frequency (HF) communications;

 Satellite communications (SATCOM);

 Controller–pilot data link communications (CPDLC);

 Audio systems;

 Emergency locator transmitters (ELTs);

 Cockpit voice recorder (CVR);

 Very high frequency omnidirectional range (VOR);

 Automatic direction finding (ADF);

 Instrument landing system (ILS);

 Flight director systems (FDSs), distance-measuring equipment (DME);

 Area navigation (RNAV) systems;

 Flight management systems (FMSs);

 Global navigation satellite systems (GNSSs), Global Positioning System (GPS), ground-based augmentation system (GBAS), satellite-based augmentation system (SBAS) such as the European geostationary navigation overlay service (EGNOS) and the wide area augmentation system (WAAS);

 Data link and two-way data link.

3

3

 

(b) Fundamentals of aircraft surveillance systems:

 Air traffic control transponder, secondary surveillance radar;

 Traffic alert and collision avoidance system (TCAS);

 Weather avoidance radar;

 Radio altimeter;

 Automatic dependent surveillance — broadcast (ADS-B) and its other associated services such as FIS-B, TIS-B and multilink;

 Inertial navigation system (INS);

 ARINC (Aeronautical Radio Incorporated) communication and reporting.

3

3

13.5 Electric power (ATA 24)

 

 

 

 

 

 

 

 

 Installation and operation of batteries;

 DC power generation;

 AC power generation;

 Emergency power generation;

 Voltage regulation;

 Power distribution;

 Inverters, transformers, rectifiers;

 Circuit protection;

 External/ground power.

3

3

13.6 Equipment and furnishings (ATA 25)

 

 

 

 

 

 

 

 

Electronic emergency equipment requirements.

3

13.7 Flight controls

 

 

 

 

 

 

 

 

(a) Primary and secondary flight controls (ATA 27):

 Primary controls: aileron, elevator, rudder, spoiler;

 Trim control: trim tabs;

 High-lift devices;

 System operation: manual;

 Gust locks and gust lock systems;

 Artificial feel, yaw damper, Mach trim, rudder limiter;

 Stall-warning systems.

2

2

 

(b) Actuation and protection:

 Active load control;

 Lift dump, speed brakes;

 Hydraulic, pneumatic systems;

 Stall-protection systems.

2

2

 

(c) System operation:

 System operation: electrical, fly-by-wire.

3

3

 

(d) Rotorcraft flight controls (ATA 67):

Rotorcraft controls: cyclic control, collective control, swashplate, yaw control.

2

2

13.8 Instruments (ATA 31)

3

3

 

 Classification;

 Atmosphere;

 Terminology;

 Pressure-measuring devices and systems;

 Pitot-static systems;

 Altimeters;

 Vertical speed indicators;

 Airspeed indicators;

 Machmeters;

 Altitude-reporting/-alerting systems;

 Air-data computers;

 Instrument pneumatic systems;

 Direct-reading pressure and temperature gauges;

 Temperature-indicating systems;

 Gyroscopic principles;

 Artificial horizons;

 Slip indicators;

 Directional gyros;

 Ground proximity warning systems (GPWSs);

 Compass systems;

 Flight data recording systems (FDRSs);

 Electronic flight instrument systems (EFISs) — typical system arrangements and cockpit layout;

 Instrument warning systems, including master warning systems and centralised warning panels;

 Stall-warning systems and angle-of-attack indicating systems;

 Vibration measurement and indication;

 Glass cockpit;

 Types and uses of general test equipment for avionics.

 

 

 

 

 

 

 

13.9 Lights (ATA 33)

 

 

 

 

 

 

 

 

External: navigation, anticollision, landing, taxiing, ice;

Internal: cabin, cockpit, cargo;

Emergency.

3

3

13.10 Onboard maintenance systems (ATA 45)

 

 

 

 

 

 

 

 

Central maintenance computers;

Data-loading system;

Electronic library system;

Printing system;

Structure monitoring system (damage-tolerance monitoring).

3

13.11 Air conditioning and cabin pressurisation (ATA 21)

 

 

 

 

 

 

 

(a) Pressurisation:

 Pressurisation systems;

 Cabin pressure controllers, control and safety valves;

 Control and indication.

3

3

(b) Air supply:

Sources of air supply including engine bleed, APU and ground cart;

Distribution systems.

1

1

(c) Air conditioning.

3

3

(d) Safety and warning devices.

3

3

13.12 Fire protection (ATA 26)

 

 

 

 

 

 

 

 

(a) Fire and smoke detection system and fire-extinguishing systems;

 Fire and smoke detection and warning systems;

 Fire-extinguishing systems;

 System tests.

3

3

 

(b) Portable fire extinguisher.

1

1

13.13 Fuel systems (ATA 28, ATA 47)

 

 

 

 

 

 

 

 

(a) System layout:

System layout;

Fuel tanks;

Supply systems.

1

1

 

(b) Fuel handling;

Cross-feed and transfer;

Refuelling and defuelling.

2

2

 

(c) Indications and warnings.

3

3

 

(d) Special systems:

Dumping, venting and draining;

Inert gas systems.

1

1

 

(e) Balancing:

Longitudinal balance fuel systems.

3

3

13.14 Hydraulic power (ATA 29)

 

 

 

 

 

 

 

 

(a) System layout:

System layout;

Hydraulic fluids;

Hydraulic reservoirs and accumulators;

Filters;

Power distribution.

1

1

 

(b) System operation (1):

Pressure generation: electric and mechanical;

Pressure control;

Indication and warning systems;

Servicing.

3

3

 

(c) System operation (2):

Pressure generation: pneumatic;

Emergency pressure generation;

Interface with other systems.

3

3

13.15 Ice and rain protection (ATA 30)

 

 

 

 

 

 

 

 

(a) Principles:

Ice formation, classification, and detection.

2

2

 

(b) De-icing:

De-icing systems: electrical, hot-air, pneumatic, and chemical;

Probe and drain heating.

3

3

 

(c) Anti-icing:

Anti-icing systems: electrical, hot-air, and chemical.

2

2

 

(d) Wiper systems.

1

1

 

(e) Rain repellent.

1

1

13.16 Landing gear (ATA 32)

 

 

 

 

 

 

 

 

(a) Description:

Construction, shock absorbing;

Tyres.

1

1

 

(b) Systems:

Extension and retraction systems: normal and emergency;

Indications and warnings;

Wheels, brakes, antiskid, and autobraking;

Steering.

3

3

 

(c) Air–ground sensing.

3

3

13.17 Oxygen (ATA 35)

 

 

 

 

 

 

 

 

System layout: cockpit, cabin;

Sources, storage, charging, and distribution;

Supply regulation;

Indications and warnings.

3

3

13.18 Pneumatic/vacuum (ATA 36)

 

 

 

 

 

 

 

 

 System layout;

2

2

 

 Sources: engine/APU, compressors, reservoirs, ground supply;

 

 Pressure control;

 

 Distribution;

 

 Indications and warnings;

 

 Interfaces with other systems.

13.19 Water/waste (ATA 38)

 

 

 

 

 

 

 

 

 Water system layout, supply, distribution, servicing, and draining;

 Toilet system layout, flushing and servicing.

2

2

13.20 Integrated modular avionics (IMA) (ATA 42)

3

 

(a) Overall system description and theory:

Core system;

Network components.

Note: Functions that may be typically integrated into the integrated modular avionics (IMA) modules are, among others:

 Bleed management;

 Air pressure control;

 Air ventilation and control;

 Avionics and cockpit ventilation control, temperature control;

 Air traffic communication;

 Avionics communication router;

 Electrical load management;

 Circuit breaker monitoring;

 Electrical system built-in test equipment (BITE);

 Fuel management;

 Braking control;

 Steering control;

 Landing gear extension and retraction;

 Tyre pressure indication;

 Oleo pressure indication;

 Brake temperature monitoring.

 

 

 

 

 

 

 

(b) Typical system layouts.

3

13.21 Cabin systems (ATA 44)

 

 

 

 

 

 

 

 

System architecture, operation and control of systems for:

 passenger in-flight entertainment;

 communication within the aircraft (cabin intercommunication data system (CIDS);

 communication between the aircraft cabin and ground stations,

including voice, data, music and video transmission.

CIDS interface between cockpit/cabin crew and cabin systems;

Data exchange between the different related line replaceable units (LRUs);

Flight attendant panels (FAPs).

CNS server and interfaces with the following systems:

 Data/radio communication system;

 Cabin core system (CCS);

 In-flight entertainment system (IFES);

 External communication system (ECS);

 Cabin mass memory system (CMMS);

 Cabin monitoring system (CMS);

 Miscellaneous cabin systems (MCSs).

The CNS may host functions such as:

 access to predeparture/departure reports;

 email/intranet/internet access;

 passenger database.

3

13.22 Information systems (ATA 46)

3

 

The units and components which furnish a means of storing, updating, and retrieving digital information traditionally provided on paper, microfilm or microfiche. They include units that are dedicated to the information storage and retrieval function, such as the electronic library mass storage and controller, but they do not include units or components installed for other uses and shared with other systems, such as flight deck printer or general-use display.

Typical examples include:

 air traffic and information management systems and network server systems;

 aircraft general information system;

 flight deck information system;

 maintenance information system;

 passenger cabin information system;

 miscellaneous information systems;

 other linked systems.

 

 

 

 

 

 

MODULE 14 — PROPULSION

 

 

MODULE 14 — PROPULSION

LEVEL

B2

B2L Instruments

B2L Airframe & Systems

14.1 Engines

 

 

(a) Constructional arrangement and operation of turbojet, turbofan, turboshaft, and turboprop engines.

1

 

(b)  Constructional arrangement and operation of auxiliary power units (APUs).

1

 

(c)  Constructional arrangement and operation of piston engines.

1

 

(d)  Constructional arrangement and operation of electric and hybrid engines, their electric energy storage and control systems.

2

 

(e) Electronic engine control and fuel-metering systems (full authority digital engine control (FADEC)).

2

14.2 Electric/electronic engine indication systems

2

 

 

 

 

 

 

 

 

 Exhaust gas temperature / interstage turbine temperature systems;

 Cylinder head temperature, engine coolant temperature, engine speed;

 Engine thrust indication: engine pressure ratio, engine turbine discharge pressure or jet pipe pressure systems;

 Vibration measurement systems;

 Oil pressure and temperature;

 Fuel pressure, temperature, and flow;

 Manifold pressure;

 Engine torque.

14.3 Propeller systems

2

 

 Propeller speed indication;

 Speed control and pitch change methods — electrical/electronic;

 Synchronising and synchrophasing equipment;

 Electrical anti-icing/de-icing equipment.

 

14.4 Starting and ignition systems

2

 

 

 

 Operation of engine start systems and components;

 Ignition systems and components;

 Maintenance safety requirements.

MODULE 15 — GAS-TURBINE ENGINE

MODULE 15 — GAS-TURBINE ENGINE

LEVEL

A1

A3

B1.1

B1.3

15.1 Fundamentals

1

2

 

 

 

 Potential energy, kinetic energy, Newton’s laws of motion, Brayton cycle;

 The relationship between force, work, power, energy, velocity, and acceleration;

 Constructional arrangement and operation of turbojet, turbofan, turboshaft, turboprop, and geared turbofan engines.

15.2 Engine performance

2

 

 

 

 

 

 Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption;

 Engine efficiencies;

 By-pass ratio and engine pressure ratio;

 Pressure, temperature, and velocity of the gas flow;

 Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations.

15.3 Inlet

2

2

 

 

 

 Compressor inlet ducts;

 Effects of various inlet configurations;

 Ice protection.

15.4 Compressors

1

2

 

 

 

 

 

 

 

 Axial and centrifugal types;

 Constructional features, operating principles, and applications;

 Fan balancing;

 Operation:

o Causes and effects of compressor stall and surge;

o Methods of air-flow control: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades;

o Compressor ratio.

15.5 Combustion section

1

2

 

Constructional features and principles of operation.

15.6 Turbine section

2

2

 

 

 

 

 Operation and characteristics of different turbine blade types;

 Blade-to-disk attachment;

 Nozzle guide vanes;

 Causes and effects of turbine blade stress and creep.

15.7 Exhaust

1

2

 

 

 

 

 Constructional features and principles of operation;

 Convergent, divergent, and variable area nozzles;

 Engine noise reduction;

 Thrust reversers.

15.8 Bearings and seals

2

 

Constructional features and principles of operation.

15.9 Lubricants and fuels

1

2

 

 

 

 Properties and specifications of standard, alternate, and drop-in fuel;

 Properties and specifications of lubricants;

 Fuel additives;

 Safety precautions.

15.10 Lubrication systems

1

2

 

System operation/layout and components.

15.11 Fuel systems

1

2

 

 

 Operation of engine control and fuel-metering systems, including electronic engine control (full authority digital engine control (FADEC)) and electronic power augmentation;

 System layout and components.

15.12 Air systems

1

2

 

Operation of engine air distribution and anti-icing control systems, including internal cooling and sealing, and external air services.

15.13 Starting and ignition systems

1

2

 

 

 

 Operation of engine start systems and components;

 Ignition systems and components;

 Maintenance safety requirements.

15.14 Engine indication systems

1

2

 

 

 

 

 

 

 

 

 Exhaust gas temperature / interstage turbine temperature;

 Engine thrust indication: engine pressure ratio, engine turbine discharge pressure or jet pipe pressure systems;

 Oil pressure and temperature;

 Fuel pressure and flow;

 Engine speed;

 Vibration measurement and indication;

 Torque;

 Power.

15.15 Alternate turbine constructions

1

 

 

 

 Geared turbofan (GTF);

 Variable fan blades;

 Open rotor/propfan;

 Hybrid turbine-electric concepts and electric power augmentation;

 Future trends and developments.

15.16 Turboprop engines

1

2

 

 

 

 

 Gas-coupled/free-turbine and gear-coupled turbines;

 Reduction gears;

 Integrated engine and propeller controls;

 Overspeed safety devices.

15.17 Turboshaft engines

1

2

 

Arrangements, drive systems, reduction gearing, couplings, control systems.

15.18 Auxiliary power units (APUs)

1

2

 

Purpose, operation, protective systems.

15.19 Power plant installation

1

2

 

Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains.

15.20 Fire protection systems

1

2

 

Operation of fire-detection and fire-extinguishing systems.

15.21 Engine monitoring and ground operation

1

3

 

 

 

 

 

 

 Procedures for starting and ground run-up;

 Interpretation of engine power output and parameters;

 Trend (including oil analysis, vibration and borescope) monitoring;

 Inspection of engine and components to criteria, tolerances and data specified by the engine manufacturer;

 Compressor washing/cleaning;

 Foreign object damage (FOD).

15.22 Engine storage and preservation

2

 

Preservation and depreservation for the engine and its accessories/systems.

MODULE 16 — PISTON ENGINE

MODULE 16 — PISTON ENGINE

LEVEL

A2

A4

B1.2

B1.4

B3

16.1 Fundamentals

1

2

 

 Mechanical, thermal, and volumetric efficiencies;

 Operating principles: 2-stroke, 4-stroke, Otto, diesel, and rotary (Wankel);

 Piston displacement and compression ratio;

 Engine configuration and firing order.

16.2 Engine performance

1

2

 

 Power calculation and measurement;

 Factors that affect engine power;

 Mixtures/leaning, pre-ignition.

16.3 Engine construction

1

2

 

 

 

 

 

 

 Crank case, crank shaft, cam shafts, sumps;

 Accessory gearbox;

 Cylinder and piston assemblies;

 Connecting rods, inlet and exhaust manifolds;

 Valve mechanisms;

 Propeller reduction gearboxes.

16.4 Engine fuel systems

 

 

 16.4.1 Carburettors

1

2

 

 

 Types, construction, and principles of operation;

 Icing and heating.

 16.4.2 Fuel injection systems

1

2

 

Types, construction, and principles of operation.

 16.4.3 Electronic engine control

1

2

 

 

 Operation of engine control and fuel-metering systems including electronic engine control (full authority digital engine control (FADEC));

 System layout and components.

16.5 Starting and ignition systems

1

2

 

 

 

 

 Starting systems, preheat systems;

 Magneto types, construction, and principles of operation;

 Ignition harnesses, spark plugs;

 Low- and high-tension systems.

16.6 Induction, exhaust, and cooling systems

1

2

 

 Construction and operation of induction systems, including alternate air systems;

 Exhaust systems, engine cooling systems — air and liquid.

16.7 Supercharging/turbocharging

1

2

 

 

 

 

 

 Principles and purpose of supercharging and its effects on engine parameters;

 Construction and operation of supercharging/turbocharging systems;

 System terminology;

 Control systems;

 System protection.

16.8 Lubricants and fuels

1

2

 

 

 

 Properties and specifications of standard, alternate, and drop-in fuel;

 Properties and specifications of lubricants;

 Fuel additives;

 Safety precautions.

16.9 Lubrication systems

1

2

 

System operation/layout and components.

16.10 Engine indication systems

1

2

 

 

 

 

 

 

 

 Engine speed;

 Cylinder head temperature;

 Coolant temperature;

 Oil pressure and temperature;

 Exhaust gas temperature;

 Fuel pressure and flow;

 Manifold pressure.

16.11 Power plant installation

1

2

 

Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains.

16.12 Engine monitoring and ground operation

1

3

 

 Procedures for starting and ground run-up;

 Interpretation of engine power output and parameters;

 Inspection of engine and components: criteria, tolerances, and data specified by the engine manufacturer.

16.13 Engine storage and preservation

2

 

Preservation and depreservation for the engine and its accessories/systems.

16.14 Alternate piston-engine constructions

1

1

 

Hybrid piston–electric concepts and electric power augmentation.

MODULE 17 — PROPELLER

MODULE 17 — PROPELLER

LEVEL

A1

A2

B1.1

B1.2

B3

17.1 Fundamentals

1

2

 

 Blade element theory;

 High/low blade angle, reverse angle, angle of attack, rotational speed;

 Propeller slip;

 Aerodynamic, centrifugal, and thrust forces;

 Torque;

 Relative airflow on blade angle of attack;

 Vibration and resonance.

17.2 Propeller construction

1

2

 

 

 

 

 Construction methods and materials used in wooden, composite and metal propellers;

 Blade station, blade face, blade shank, blade back / thrust face and hub assembly;

 Fixed pitch, controllable pitch, constant speeding propeller;

 Propeller/spinner installation.

17.3 Propeller pitch control

1

2

 

 

 

 Speed control and pitch change methods — mechanical and electrical/electronic;

 Feathering and reverse pitch;

 Overspeed protection.

17.4 Propeller synchronising

2

 

Synchronising and synchrophasing equipment.

17.5 Propeller ice protection

1

2

 

Fluid and electrical de-icing equipment.

17.6 Propeller maintenance

1

3

 

 

 

 

 

 Static and dynamic balancing;

 Blade tracking;

 Assessment of blade damage, erosion, corrosion, impact damage, delamination;

 Propeller treatment/repair schemes;

 Propeller engine running.

17.7 Propeller storage and preservation

1

2

 

Propeller preservation and depreservation.

Basic training methods

Training methods are categorised as follows: ‘instructor-centred training’, ‘student-centred training’, and ‘blended training’.

The actual training method and training tools should be adapted to suit the training subject and be chosen considering their intrinsic characteristics, such as but not limited to their efficiency and the pedagogical benefits of the training method/tool.

Basic training modules 7, 9, 11, 12, 13, 14, 15, 16 and 17 should not normally be taught solely through a student-centred method unless provisions are in place to verify the actual and progressive acquisition of knowledge, skills and attitude by the student.

1. General

Regulation (EU) 2023/989

1.1. All basic examinations shall be carried out using the multi-choice question format and essay questions as specified below. The incorrect alternatives shall seem equally plausible to anyone ignorant of the subject. All of the alternatives shall be clearly related to the question and of similar vocabulary, grammatical construction and length. In numerical questions, the incorrect answers shall correspond to procedural errors such as corrections applied in the wrong sense or incorrect unit conversions: they shall not be mere random numbers.

1.2. Each multi-choice question shall have three alternative answers of which only one shall be the correct answer and the candidate shall be allowed a time per module which is based upon a nominal average of 75 seconds per question.

1.3. Each essay question requires the preparation of a written answer and the candidate shall be allowed 20 minutes to answer each such question.

1.4. Suitable essay questions shall be drafted and evaluated using the knowledge syllabus in Appendix I Module 7.

1.5. Each question will have a model answer drafted for it, which will also include any known alternative answers that may be relevant for other subdivisions.

1.6. The model answer will also be broken down into a list of the important points known as Key Points.

1.7. The pass mark for each module and sub-module multi-choice part of the examination is 75 %.

1.8. The pass mark for each essay question is 75 % in that the candidates answer shall contain 75 % of the required key points addressed by the question and no significant error related to any required key point.

1.9. If either the multi-choice part only or the essay part only is failed, then it is only necessary to retake the multi-choice or essay part, as appropriate.

1.10. Penalty marking systems shall not be used to determine whether a candidate has passed.

1.11. An examination in a module may not be retaken earlier than 90 days following the date of a failed examination in that module, except in the case of a maintenance training organisation approved in accordance with Annex IV (Part-147) which delivers a course of retraining tailored to the failed subjects in the particular module; the failed module may be retaken after 30 days.

1.12. Basic knowledge examinations with a maximum allowed time of more than 90 or more than 180 minutes may be split in two or three partial exams respectively.

Each partial exam shall:

(a) be complementary to the other partial exam or exams taken by the candidate, ensuring that the combination of partial exams meets the examination requirements for the subject module;

(b) be of similar allowed time;

(c) be passed with 75 % or more of the questions answered correctly;

(d) contain a number of questions that is multiple of four;

(e) be listed on the same certificate of recognition issued after the last partial exam has been successfully passed. That certificate of recognition shall list the dates and the results of the partial exams – without averaging the results;

(f) be taken within the same organisation, following the normal examination provisions for retaking failed exams.

1.13. The maximum number of attempts for each examination is three in a 12-month period.

The applicant shall provide in a written statement to the approved maintenance training organisation or the competent authority to which they apply for an examination, the number, and dates of attempts during the 12 months preceding the examination, and the organisation or the competent authority where those attempts took place. The approved maintenance training organisation or the competent authority is responsible for checking the number of attempts within the applicable time frames.

1.14 While it is accepted that the subject matter of the questions may be the same, the questions used as part of the MBT learning programme shall not be used in examinations.

2. Number of questions per module

Regulation (EU) 2023/989

2.1. MODULE 1 – MATHEMATICS

Category A: 16 multiple-choice, no essay questions.

Time allowed: 20 minutes.

Category B1, B2, B2L and B3: 32 multiple-choice, no essay questions.

Time allowed: 40 minutes.

2.2. MODULE 2 – PHYSICS

Category A and B3: 32 multiple-choice, no essay questions.

Time allowed: 40 minutes.

Category B1, B2 and B2L: 52 multiple-choice, no essay questions.

Time allowed: 65 minutes.

2.3. MODULE 3 – ELECTRICAL FUNDAMENTALS

Category A: 20 multiple-choice, no essay questions.

Time allowed: 25 minutes.

Category B3: 24 multiple-choice, no essay questions.

Time allowed: 30 minutes.

Category B1, B2 and B2L: 52 multiple-choice, no essay questions.

Time allowed: 65 minutes.

2.4. MODULE 4 —ELECTRONICS FUNDAMENTALS

Category B1 and B3: 20 multiple-choice, no essay questions.

Time allowed: 25 minutes.

Category B2 and B2L: 40 multiple-choice, no essay questions.

Time allowed: 50 minutes.

2.5. MODULE 5 – DIGITAL TECHNIQUES/ELECTRONIC INSTRUMENT SYSTEMS

Category A and B3: 20 multiple-choice, no essay questions.

Time allowed: 25 minutes.

Category B1: 40 multiple-choice, no essay questions.

Time allowed: 50 minutes.

Category B2 and B2L: 72 multiple-choice, no essay questions.

Time allowed: 90 minutes.

2.6. MODULE 6 – MATERIALS AND HARDWARE

Category A: 52 multiple-choice, no essay questions.

Time allowed: 65 minutes.

Category B1 and B3: 80 multiple-choice, no essay questions.

Time allowed: 100 minutes.

Category B2 and B2L: 60 multiple-choice, no essay questions.

Time allowed: 75 minutes.

2.7. MODULE 7 – MAINTENANCE PRACTICES

Category A: 76 multiple-choice and 2 essay questions.

Time allowed: 95 minutes plus 40 minutes.

Category B1 and B3: 80 multiple-choice and 2 essay questions.

Time allowed: 100 minutes plus 40 minutes.

Category B2 and B2L: 60 multiple-choice and 2 essay questions.

Time allowed: 75 minutes plus 40 minutes.

2.8. MODULE 8 – BASIC AERODYNAMICS

Category A, B3, B1, B2 and B2L: 24 multiple-choice, no essay questions.

Time allowed: 30 minutes.

2.9. MODULE 9 – HUMAN FACTORS

Category A, B1, B3, B2 and B2L: 28 multiple-choice, no essay questions.

Time allowed: 35 minutes.

2.10. MODULE 10 – AVIATION LEGISLATION

Category A: 32 multiple-choice, no essay questions.

Time allowed: 40 minutes.

Category B1, B3, B2 and B2L: 44 multiple-choice, no essay questions.

Time allowed: 55 minutes.

2.11. MODULE 11 AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Category A1: 108 multiple-choice, no essay questions.

Time allowed: 135 minutes.

Category A2: 72 multiple-choice, no essay questions.

Time allowed: 90 minutes.

Category B1.1: 140 multiple-choice, no essay questions.

Time allowed: 175 minutes.

Category B1.2: 100 multiple-choice, no essay questions.

Time allowed: 125 minutes.

Category B3: 60 multiple-choice, no essay questions.

Time allowed: 75 minutes.

2.12. MODULE 12 – HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS:

Category A: 100 multiple-choice, no essay questions.

Time allowed: 125 minutes.

Category B1.3 and B1.4: 128 multiple-choice, no essay questions.

Time allowed: 160 minutes.

2.13. MODULE 13 – AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

Category B2: 188 multiple-choice, no essay questions.

Time allowed: 235 minutes.

Category B2L:

System rating

Number of multiple-choice questions

Time allowed (minutes)

Basic requirements

(Submodules 13.1, 13.2, 13.5 and 13.9)

32

40

COM/NAV

(Submodule 13.4(a))

24

30

INSTRUMENTS

(Submodule 13.8)

20

25

AUTOFLIGHT

(Submodules 13.3 and 13.7)

28

35

SURVEILLANCE

 (Submodule 13.4(b))

20

25

AIRFRAME SYSTEMS

(Submodules 13.11 to 13.19)

52

65

2.14. MODULE 14 — PROPULSION

Category B2 and B2L: 32 multiple-choice, no essay questions.

Time allowed: 40 minutes.

NOTE: The B2L examination for Module 14 is only applicable to the ‘Instruments’ and ‘Airframe Systems’ ratings.

2.15. MODULE 15 – GAS TURBINE ENGINE

Category A1 and A3: 60 multiple-choice, no essay questions.

Time allowed: 75 minutes.

Category B1.1 and B1.3: 92 multiple-choice, no essay questions.

Time allowed: 115 minutes.

2.16. MODULE 16 – PISTON ENGINE

Category A2 and A4: 52 multiple-choice, no essay questions.

Time allowed: 65 minutes.

Category B3, B1.2 and B1.4: 76 multiple-choice, no essay questions.

Time allowed: 95 minutes.

2.17. MODULE 17 – PROPELLER

Category A1 and A2: 20 multiple-choice, no essay questions.

Time allowed: 25 minutes.

Category B3, B1.1 and B1.2: 32 multiple-choice, no essay questions.

Time allowed: 40 minutes.

AMC1 Appendix II — Basic examination standard (except for category L licence)

ED Decision 2023/019/R

The tables below show the acceptable number of questions for the submodules. Justified deviations from these values are also acceptable, provided the sum of the questions complies with the total number of questions for a given module.

MODULE 1 — MATHEMATICS

 

 

MODULE 1 — MATHEMATICS

Nr of questions

A

B1

B2

B2L

B3

Total number for the module:

16

32

1.1 Arithmetic

6

6

1.2 Algebra:

 

 

 

(a) Simple algebraic expressions;

5

4

 

(b) Equations.

12

1.3 Geometry:

 

 

 

(a) Simple geometrical constructions;

3

 

(b) Graphical representation;

5

4

 

(c) Trigonometry.

3

MODULE 2 — PHYSICS

MODULE 2 — PHYSICS

Nr of questions

A

B3

B1

B2

B2L

Total number for the module:

32

52

2.1 Matter

4

5

2.2 Mechanics

 

 

 2.2.1 Statics

6

7

 2.2.2 Kinetics

6

7

 2.2.3 Dynamics:

 

 

 

(a) Mass, force, and energy;

4

5

 

(b) Momentum and conservation of momentum.

4

4

 2.2.4 Fluid dynamics:

 

 

 

(a) Gravity and density;

2

2

 

(b) Viscosity; compressibility on fluids; static, dynamic, and total pressure.

2

3

2.3 Thermodynamics:

 

 

 

(a) Temperature;

2

2

 

(b) Heat.

2

8

2.4 Optics (light)

5

2.5 Wave motion and sound

4

MODULE 3 — ELECTRICS FUNDAMENTALS

MODULE 3 — ELECTRICAL FUNDAMENTALS

Nr of questions

A

B1

B2

B2L

B3

Total number for the module:

20

52

24

3.1 Electron theory

2

2

2

3.2 Static electricity and conduction

3

 3

2

3.3 Electrical terminology

3

2

2

3.4 Generation of electricity

3

2

2

3.5 Sources of DC electricity

3

3

3

3.6 DC circuits

1

2

1

3.7 Resistance/resistor:

 

 

 

 

(a) Resistance;

3

1

 

(b) Resistors.

2

3.8 Power

3

1

3.9 Capacitance/capacitor

4

1

3.10 Magnetism:

 

 

 

 

(a) Theory of magnetism;

3

1

 

(b) Magnetomotive force.

1

1

3.11 Inductance/inductor

4

1

3.12 DC motor/generator theory

3

1

3.13 AC theory

5

3

1

3.14 Resistive (R), capacitive (C) and inductive (L) circuits

3

1

3.15 Transformers

3

1

3.16 Filters

1

3.17 AC generators

3

1

3.18 AC motors

2

1

MODULE 4 — ELECTRONICS FUNDAMENTALS

 

MODULE 4 — ELECTRONICS FUNDAMENTALS

Nr of questions

A

B1

B3

B2

B2L

Total number for the module:

20

40

4.1 Semiconductors

 

 

 

 4.1.1 Diodes:

 

 

 

 

(a) Description and characteristics;

8

8

 

(b) Operation and function.

7

 4.1.2 Transistors:

 

 

 

 

(a) Description and characteristics;

4

4

 

(b) Construction and operation.

7

 4.1.3 Integrated circuits:

 

 

 

 

(a) Basic description and operation;

3

2

 

(b) Description and operation.

4

4.2 Printed circuit boards

2

3

4.3 Servomechanisms:

 

 

 

 

(a) Principles;

3

2

 

(b) Construction, operation, and use.

3

MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS

 

MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS

Nr of questions

A

B3

B1

B2

B2L

Total number for the module:

20

20

40

72

5.1 Electronic instrument systems

4

4

4

4

5.2 Numbering systems

3

5

5.3 Data conversion

3

4

5.4 Data buses

3

5

5.5 Logic circuits:

 

 

 

 

 

(a) Identification and applications;

3

4

 

(b) Interpretation of logic diagrams.

4

5.6 Basic computer structure:

 

 

 

 

 

(a) Computer terminology and technology;

6

2

4

2

 

(b) Computer operation.

6

5.7 Microprocessors

4

5.8 Integrated circuits

5

5.9 Multiplexing

4

5.10 Fibre optics

3

3

5.11 Electronic displays

2

2

2

4

5.12 Electrostatic sensitive devices

6

6

4

5

5.13 Software management control

1

3

3

5.14 Electromagnetic environment

1

3

4

5.15 Typical electronic/digital aircraft systems

2

4

5

6

MODULE 6 — MATERIALS AND HARDWARE

 

MODULE 6 — MATERIALS AND HARDWARE

Nr of questions

A

B1

B3

B2

B2L

Total number for the module:

52

80

60

6.1 Aircraft materials — ferrous:

 

 

 

 

(a) Alloy steels used in aircraft;

3

3

3

 

(b) Testing of ferrous materials;

2

1

 

(c) Repair and inspection procedures.

2

1

6.2 Aircraft materials — non-ferrous:

 

 

 

 

(a) Characteristics;

3

4

3

 

(b) Testing of non-ferrous materials;

3

2

 

(c) Repair and inspection procedures.

2

1

6.3 Aircraft materials — composite and non-metallic

 

 

 

 6.3.1 Composite and non-metallic other than wood and fabric:

 

 

 

 

(a) Characteristics;

2

4

3

 

(b) Detection of defects;

2

4

 

(c) Repairs and inspection procedures.

2

2

 6.3.2 Wooden structures

3

4

 6.3.3 Fabric covering

4

6.4 Corrosion:

 

 

 

 

(a) Chemical fundamentals;

3

3

3

 

(b) Types of corrosion.

4

5

3

6.5 Fasteners

 

 

 

 6.5.1 Screw threads

4

4

3

 6.5.2 Bolts, studs, and screws

6

6

5

 6.5.3 Locking devices

2

2

2

 6.5.4 Aircraft rivets

2

3

2

6.6 Pipes and unions:

 

 

 

 

(a) Identification;

1

1

1

 

(b) Standard unions.

2

2

2

6.7 Springs

1

1

6.8 Bearings

2

4

3

6.9 Transmissions

3

4

4

6.10 Control cables

5

5

4

6.11 Electrical cables and connectors

5

6

11

MODULE 7 — MAINTENANCE PRACTICES

 

MODULE 7 — MAINTENANCE PRACTICES

Nr of questions

A

B1

B3

B2

B2L

Total number for the module:

76

80

60

7.1 Safety precautions — aircraft and workshop

4

4

4

7.2 Workshop practices

4

4

4

7.3 Tools

6

6

6

7.4 (Reserved)

7.5 Engineering drawings, diagrams, and standards

6

6

6

7.6 Fits and clearances

5

5

5

7.7 Electrical wiring interconnection system (EWIS)

4

4

8

7.8 Riveting

4

3

7.9 Pipes and hoses

4

3

7.10 Springs

1

1

7.11 Bearings

4

3

7.12 Transmissions

3

3

7.13 Control cables

4

3

7.14 Material handling

 

 

 

 7.14.1 Sheet metal

2

 7.14.2 Composite and non-metallic

2

 7.14.3 Additive manufacturing

2

4

2

7.15 (Reserved)

7.16 Aircraft weight and balance:

 

 

 

 

(a) Centre-of-gravity calculation;

2

2

 

(b) Aircraft weighing.

1

7.17 Aircraft handling and storage

7

5

6

7.18 Disassembly, inspection, repair, and assembly techniques:

 

 

 

 

(a) Types of defects and visual inspection techniques;

2

2

2

 

(b) General repair methods — structural repair manual;

2

 

(c) Non-destructive inspection techniques;

1

1

 

(d) Disassembly and reassembly techniques;

2

1

1

 

(e) Troubleshooting techniques.

1

1

7.19 Abnormal events:

 

 

 

 

(a) Inspections following lightning strikes and HIRF penetration;

2

1

2

 

(b) Inspections following abnormal events such as heavy landing and flight  through turbulence.

2

1

7.20 Maintenance procedures

6

6

6

7.21 Documentation and communication

4

4

4

MODULE 8 — BASIC AERODYNAMICS

MODULE 8 — BASIC AERODYNAMICS

Nr of questions

A

B3

B1

B2

B2L

Total number for the module:

24

24

8.1 Physics of the atmosphere

2

2

 

International Standard Atmosphere (ISA), application to aerodynamics.

8.2 Aerodynamics

9

9

8.3 Theory of flight

7

7

8.4 High-speed airflow

4

4

8.5 Flight stability and dynamics

2

2

MODULE 9 — HUMAN FACTORS

MODULE 9 — HUMAN FACTORS

Nr of questions

ALL

Total number for the module:

28

9.1 General

3

9.2 Human performance and limitations

3

9.3 Social psychology

2

9.4 Factors that affect human performance

3

9.5 Physical environment

2

9.6 Tasks

2

9.7 Communication

3

9.8 Human error

4

9.9 Safety management

2

9.10 The ‘Dirty Dozen’ and risk-mitigation

4

MODULE 10 — AVIATION LEGISLATION

 

 

MODULE 10 — AVIATION LEGISLATION

Nr of questions

A

B1

B2

B2L

B3

Total number for the module:

32

44

10.1 Regulatory framework

5

5

10.2 Certifying staff — maintenance

7

7

10.3 Approved maintenance organisations

6

6

10.4 Independent certifying staff

-

4

10.5 Air operations

4

4

10.6 Certification of aircraft, parts, and appliances

1

4

10.7 Continuing airworthiness

6

7

10.8 Oversight principles in continuing airworthiness

2

3

10.9 Maintenance and certification beyond the current EU regulations
(if not superseded by EU requirements)

3

10.10 Cybersecurity in aviation maintenance

1

1

MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

Nr of questions

A1

A2

B1.1

B1.2

B3

Total number for the module:

108

72

140

100

60

11.1 Theory of flight:

 

 

 

 

 

 (a) Aeroplane aerodynamics and flight controls;

2

2

2

2

2

 (b) Aeroplane, other aerodynamic devices.

2

2

2

2

2

11.2 Airframe structures (ATA 51):

 

 

 

 

 

 (a) General concepts;

 (b) Airworthiness requirements for structural strength;

3

3

4

3

2

3

3

3

3

1

 (c) Construction methods.

1

1

3

2

1

11.3 Airframe structures — aeroplanes

 

 

 

 

 

 11.3.1 Fuselage, doors, windows (ATA 52/53/56):

1

1

2

2

2

 (a) Construction principles;

 (b) Airborne towing devices;

1

1

1

1

1

 (c) Doors.

1

1

1

1

-

 11.3.2 Wings (ATA 57)

2

2

3

3

2

 11.3.3 Stabilisers (ATA 55)

1

1

2

2

1

 11.3.4 Flight control surfaces (ATA 55/57)

1

1

2

2

1

 11.3.5 Nacelles/pylons (ATA 54)

1

1

2

2

1

11.4 Air conditioning and cabin pressurisation (ATA 21):

 

 

 

 

 

 (a) Pressurisation;

2

2

3

1

 (b) Air supply;

3

3

 (c) Air conditioning;

3

3

 (d) Safety and warning devices;

2

1

2

2

 (e) Heating and ventilation system.

1

2

1

11.5 Instruments / avionics systems

 

 

 

 

 

 11.5.1 Instrument systems (ATA 31)

2

2

4

4

3

 11.5.2 Avionics systems

3

2

5

4

4

 

Fundamentals of system layouts and operation of:

 Autoflight (ATA 22);

 Communications (ATA 23);

 Navigation systems (ATA 34).

11.6 Electrical power (ATA 24)

4

3

5

5

4

11.7 Equipment and furnishings (ATA 25)

 

 

 

 

 

 

(a) Emergency equipment;

4

2

4

3

2

 

(b) Cabin and cargo layout.

3

3

3

3

-

11.8 Fire protection (ATA 26)

 

 

 

 

 

 

(a) Fire and smoke detection system and fire-extinguishing systems;

3

2

4

3

 

(b) Portable fire extinguisher.

1

1

1

1

1

11.9 Flight controls (ATA 27)

3

2

4

4

3

 

(a) Primary and secondary flight controls;

 

(b) Actuation and protection;

3

3

 

(c) System operation;

3

3

 

(d) Balancing and rigging.

1

1

3

3

2

11.10 Fuel systems (ATA 28/47)

2

2

3

3

2

 

(a) Systems layout;

 

(b) Fuel handling;

2

2

2

2

1

 

(c) Indications and warnings;

1

1

2

2

1

 

(d) Special systems;

1

1

 

(e) Balancing.

2

2

11.11 Hydraulic power (ATA 29)

1

1

3

3

2

 

(a) System description;

 

(b) System operation (1);

1

1

3

2

1

 

(c) System operation (2).

2

2

11.12 Ice and rain protection (ATA 30)

1

1

2

2

1

 

(a) Principles;

 

(b) De-icing;

1

1

2

2

1

 

(c) Anti-icing;

1

2

 

(d) Wipers;

1

1

2

2

1

 

(e) Rain-repellent systems.

2

2

11.13 Landing gear (ATA 32)

3

3

4

3

1

 

(a) Description;

 

(b) System operation;

3

3

4

2

1

 

(c) Air–ground sensing;

1

1

 

(d) Tail protection.

1

1

1

1

1

11.14 Lights (ATA 33)

2

2

3

3

2

11.15 Oxygen (ATA 35)

3

3

4

4

3

11.16 Pneumatic/vacuum (ATA 36)

 

 

 

 

 

 (a) Systems;

3

3

3

3

2

 (b) Pumps.

3

3

3

3

2

11.17 Water/waste (ATA 38)

 

 

 

 

 

 (a) Systems;

2

2

2

2

1

 (b) Corrosion.

1

1

1

1

1

11.18 Onboard maintenance systems (ATA 45)

3

3

11.19 Integrated modular avionics (IMA) (ATA 42)

 

 

 

 

 

 (a) Overall system description and theory;

1

1

 (b) Typical system layouts.

1

1

11.20 Cabin systems (ATA 44)

2

2

11.21 Information systems (ATA 46)

2

2

MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

Nr of questions

A3

A4

B1.3

B1.4

Total number for the module:

100

128

12.1 Theory of flight — rotary wing aerodynamics

6

9

12.2 Flight control systems (ATA 67)

9

9

12.3 Blade tracking and vibration analysis (ATA 18)

6

9

12.4 Transmission

3

6

12.5 Airframe structures (ATA 51)

 

 

 

(a) General concept;

5

6

 

(b) Construction methods of the principal elements.

5

7

12.6 Air conditioning (ATA 21)

 12.6.1 Air supply

1

2

 12.6.2 Air conditioning

3

5

12.7 Instruments / avionics systems

 

 

 12.7.1 Instrument systems (ATA 31)

6

9

 12.7.2 Avionics systems

5

7

 

Fundamentals of system layouts and operation of:

 Autoflight (ATA 22);

 Communications (ATA 23);

 Navigation systems (ATA 34).

12.8 Electrical power (ATA 24)

8

10

12.9 Equipment and furnishings (ATA 25)

 

 

 

(a) Emergency equipment:

Seats, harnesses, and belts;

Lifting systems.

2

3

 

(b) Emergency flotation systems:

Cabin layout, cargo retention;

Equipment layout;

Cabin furnishing installation.

3

3

12.10 Fire protection (ATA 26)

3

4

 

(a) Fire and smoke detection systems and fire-extinguishing systems;

 

(b) Portable fire extinguishers.

1

1

12.11 Fuel systems (ATA 28)

7

8

12.12 Hydraulic power (ATA 29)

8

8

12.13 Ice and rain protection (ATA 30)

4

4

12.14 Landing gear (ATA 32)

 

 

 

(a) System description and operation;

3

4

 

(b) Sensors.

3

3

12.15 Lights (ATA 33)

3

4

12.16 (Reserved)

 

 

12.17 Integrated modular avionics (IMA) (ATA 42)

 

 

 

(a) Overall system description and theory;

1

1

 

(b) Typical system layouts.

1

1

12.18 Onboard maintenance systems (ATA 45)

2

3

 

Central maintenance computers;

Data-loading system;

Electronic library system.

12.19 Information systems (ATA 46)

2

2

MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

C/N: Communication and Navigation; Ins.: instruments; A/F: Autoflight; Sur.: Surveillance; A/S: Airframe and Systems

MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

Nr of questions

B2

B2L Basic

B2L

C/N

B2L

Ins.

B2L

A/F

B2L

Sur.

B2L

A/S

Total number for the module:

188

32

24

20

28

20

50

13.1 Theory of flight

 

 

 

 

 

 

 

 

(a) Aeroplane aerodynamics and flight controls;

3

3

 

(b) Rotary wing aerodynamics.

1

1

13.2 Structures — general concepts (ATA 51)

 

 

 

 

 

 

 

 

(a) General concepts;

4

4

 

(b) Fundamentals of structural systems.

4

4

13.3 Autoflight (ATA 22)

 

 

 

 

 

 

 

 

(a) Fundamentals of automatic flight control;

16

8

 

(b) Autothrottle systems and automatic landing systems.

8

8

13.4 Communication/navigation (ATA 23/34)

 

 

 

 

 

 

 

 

(a) Fundamentals of communication and navigation systems;

24

24

 

(b) Fundamentals of aircraft surveillance systems.

3

20

13.5 Electrical power (ATA 24)

13

13

13.6 Equipment and furnishings (ATA 25)

5

13.7 Flight controls

 

 

 

 

 

 

 

 

(a) Primary and secondary flight controls (ATA 27);

4

3

 

(b) Actuation and protection;

4

3

 

(c) System operation;

2

3

 

(d) Rotorcraft flight controls (ATA 67).

2

3

13.8 Instruments (ATA 31)

20

20

13.9 Lights (ATA 33)

7

7

13.10 Onboard maintenance systems (ATA 45)

5

13.11 Air conditioning and cabin pressurisation (ATA 21)

 

 

 

 

 

 

 

 (a) Pressurisation;

2

2

 (b) Air supply;

2

2

 (c) Air conditioning;

2

2

 (d) Safety and warning devices.

2

2

13.12 Fire protection (ATA 26)

 

 

 

 

 

 

 

 

(a) Fire and smoke detection system and fire-extinguishing systems;

2

2

 

(b) Portable fire extinguisher.

1

1

13.13 Fuel systems (ATA 28, ATA 47)

 

 

 

 

 

 

 

 

(a) System layout;

2

2

 

(b) Fuel handling;

2

2

 

(c) Indications and warnings;

2

2

 

(d) Special systems;

2

2

 

(e) Balancing.

1

1

13.14 Hydraulic power (ATA 29)

 

 

 

 

 

 

 

 

(a) System layout;

1

1

 

(b) System operation (1);

5

4

 

(c) System operation (2).

5

4

13.15 Ice and rain protection (ATA 30)

 

 

 

 

 

 

 

 

(a) Principles;

1

1

 

(b) De-icing;

2

2

 

(c) Anti-icing;

1

1

 

(d) Wiper systems;

1

1

 

(e) Rain repellent.

1

1

13.16 Landing gear (ATA 32)

 

 

 

 

 

 

 

 

(a) Description;

1

1

 

(b) System;

3

3

 

(c) Air–ground sensing.

3

3

13.17 Oxygen (ATA 35)

2

13.18 Pneumatic/vacuum (ATA 36)

6

6

13.19 Water/waste (ATA 38)

2

2

13.20 Integrated modular avionics (IMA) (ATA 42)

 

 

 

 

 

 

 

 (a) Overall system description and theory;

2

 (b) Typical system layouts.

1

13.21 Cabin systems (ATA 44)

3

13.22 Information systems (ATA 46)

3

MODULE 14 — PROPULSION

 

 

MODULE 14 — PROPULSION

Nr of questions

B2

B2L Instruments

B2L Airframe and Systems

Total number for the module:

32

14.1 Engines

 

 

(a) Turbine engines;

3

 

(b) Auxiliary power units (APUs);

4

 

(c) Piston engines;

2

 

(d) Electric and hybrid engines;

4

 

(e) Engine control.

3

14.2 Electric/electronic engine indication systems

10

14.3 Propeller systems

2

14.4 Starting and ignition systems

4

MODULE 15 — GAS-TURBINE ENGINE

MODULE 15 — GAS-TURBINE ENGINE

Nr of questions

A1

A3

B1.1

B1.3

Total number for the module:

60

92

15.1 Fundamentals

4

4

15.2 Engine performance

6

15.3 Inlet

3

4

15.4 Compressors

5

7

15.5 Combustion section

3

3

15.6 Turbine section

5

5

15.7 Exhaust

4

4

15.8 Bearings and seals

3

15.9 Lubricants and fuels

3

4

15.10 Lubrication systems

3

4

15.11 Fuel systems

4

5

15.12 Air systems

3

3

15.13 Starting and ignition systems

3

4

15.14 Engine indication systems

5

7

15.15 Alternate turbine constructions

2

15.16 Turboprop engines

3

5

15.17 Turboshaft engines

2

3

15.18 Auxiliary power units (APUs)

2

3

15.19 Power plant installation

2

3

15.20 Fire protection systems

2

3

15.21 Engine monitoring and ground operation

4

7

15.22 Engine storage and preservation

3

MODULE 16 — PISTON ENGINE

 

 

MODULE 16 — PISTON ENGINE

Nr of questions

A2

A4

B1.2

B1.4

B3

Total number for the module:

52

76

16.1 Fundamentals of piston engines

5

5

16.2 Engine performance

3

5

16.3 Engine construction

7

8

16.4 Engine fuel systems

 16.4.1 Carburettors

3

4

 16.4.2 Fuel injection systems

2

4

 16.4.3 Electronic engine control

2

4

16.5 Starting and ignition systems

5

5

16.6 Induction, exhaust, and cooling systems

3

4

16.7 Supercharging/turbocharging

4

6

16.8 Lubricants and fuels

2

5

16.9 Lubrication systems

3

4

16.10 Engine indication systems

6

7

16.11 Power plant installation

3

3

16.12 Engine monitoring and ground operation

3

5

16.13 Engine storage and preservation

3

16.14 Alternative piston-engine constructions

1

4

MODULE 17 — PROPELLER

 

 

MODULE 17 — PROPELLER

Nr of questions

A1

A2

B1.1

B1.2

B3

Total number for the module:

20

32

17.1 Fundamentals of propellers

5

8

17.2 Propeller construction

4

5

17.3 Propeller pitch control

4

6

17.4 Propeller synchronising

2

17.5 Propeller ice protection

2

3

17.6 Propeller maintenance

3

6

17.7 Propeller storage and preservation

2

2

1. General

Regulation (EU) 2023/989

Aircraft type training shall consist of theoretical training and examination, and, except for the category C ratings, practical training and assessment.

(a) Theoretical training and examination shall comply with the following requirements:

(i) Shall be conducted by a maintenance training organisation appropriately approved in accordance with Annex IV (Part-147) or, when conducted by other organisations, as directly approved by the competent authority.

(ii) Shall comply with the standard set out in point 3.1 of this Appendix and, if existing, the elements defined in the operational suitability data (OSD) established in accordance with Regulation (EU) No 748/2012.

(iii) In the case of a category C person qualified by holding an academic degree as specified in point 66.A.30(a)(5), the first relevant aircraft type theoretical training shall be at the category B1 or B2 level.

(iv) Shall have been started and completed within the 3 years preceding the application for a type rating endorsement.

(b) Practical training and assessment shall comply with the following requirements:

(i) Shall be conducted by a maintenance training organisation appropriately approved in accordance with Annex IV (Part-147) or, when conducted by other organisations, as directly approved by the competent authority.

(ii) Shall comply with the standard set out in point 3.2 of this Appendix and, if existing, the elements defined in the OSD established in accordance with Regulation (EU) No 748/2012.

(iii) Shall include a representative cross section of maintenance activities relevant to the aircraft type.

(iv) Shall include demonstrations using equipment, components, maintenance simulation training devices (MSTDs), maintenance training devices (MTDs), or real aircraft.

(v) Shall have been started and completed within the 3 years preceding the application for a type rating endorsement.

(c) Differences training

(i) Differences training is the training required to cover the training differences between:

(a) two different aircraft type ratings of the same manufacturer as determined by the Agency; or

(b) two different licence categories in respect of the same aircraft type rating.

(ii) Differences training has to be defined on a case-to-case basis taking into account the requirements contained in this Appendix III in respect of both theoretical and practical elements of type rating training.

(iii) A type rating shall only be endorsed on a licence after differences training when the applicant also complies with one of the following conditions:

               having already endorsed on the licence the aircraft type rating from which the differences are being identified, or

               having completed the type training requirements for the aircraft from which the differences are being identified.

(iv) the differences training shall have been started and completed within 3 years preceding the application for the new type rating in the same category (case (a)) or in another category (case (b)).

2. Aircraft type training levels

Regulation (EU) No 1321/2014

The three levels listed below define the objectives, the depth of training and the level of knowledge that the training is intended to achieve.

               Level 1: A brief overview of the airframe, systems and powerplant as outlined in the Systems Description Section of the Aircraft Maintenance Manual/Instructions for Continued Airworthiness.

Course objectives: Upon completion of Level 1 training, the student will be able to:

(a) provide a simple description of the whole subject, using common words and examples, using typical terms and identify safety precautions related to the airframe, its systems and powerplant;

(b) identify aircraft manuals, maintenance practices important to the airframe, its systems and powerplant;

(c) define the general layout of the aircraft's major systems;

(d) define the general layout and characteristics of the powerplant;

(e) identify special tooling and test equipment used with the aircraft.

               Level 2: Basic system overview of controls, indicators, principal components, including their location and purpose, servicing and minor troubleshooting. General knowledge of the theoretical and practical aspects of the subject.

Course objectives: In addition to the information contained in the Level 1 training, at the completion of Level 2 training, the student will be able to:

(a) understand the theoretical fundamentals; apply knowledge in a practical manner using detailed procedures;

(b) recall the safety precautions to be observed when working on or near the aircraft, powerplant and systems;

(c) describe systems and aircraft handling particularly access, power availability and sources;

(d) identify the locations of the principal components;

(e) explain the normal functioning of each major system, including terminology and nomenclature;

(f) perform the procedures for servicing associated with the aircraft for the following systems: Fuel, Power Plants, Hydraulics, Landing Gear, Water/Waste, and Oxygen;

(g) demonstrate proficiency in use of crew reports and on-board reporting systems (minor troubleshooting) and determine aircraft airworthiness per the MEL/CDL;

(h) demonstrate the use, interpretation and application of appropriate documentation including instructions for continued airworthiness, maintenance manual, illustrated parts catalogue, etc.

               Level 3: Detailed description, operation, component location, removal/installation and bite and troubleshooting procedures to maintenance manual level.

Course objectives: In addition to the information contained in Level 1 and Level 2 training, at the completion of Level 3 training, the student will be able to:

(a) demonstrate a theoretical knowledge of aircraft systems and structures and interrelationships with other systems, provide a detailed description of the subject using theoretical fundamentals and specific examples and to interpret results from various sources and measurements and apply corrective action where appropriate;

(b) perform system, powerplant, component and functional checks as specified in the aircraft maintenance manual;

(c) demonstrate the use, interpret and apply appropriate documentation including structural repair manual, troubleshooting manual, etc.;

(d) correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level;

(e) describe procedures for replacement of components unique to aircraft type.

3. Aircraft type training standard

Regulation (EU) 2023/989

Although aircraft type training includes both theoretical and practical elements, courses can be approved for the theoretical element, the practical element or for a combination of both.

An appropriate training method, or combination of training methods, shall be determined for the entire course or for each of its parts with regard to the scope and objectives of each training phase and taking into consideration the benefits and limitations of the available training methods.

Multimedia-based training (MBT) methods may be used in order to achieve the training objectives either in a physically or in a virtually controlled environment.

3.1. Theoretical element

Regulation (EU) 2023/989

(a) Objective:

On completion of a theoretical training course the student shall be able to demonstrate, to the levels identified in the Appendix III syllabus, the detailed theoretical knowledge of the aircraft’s applicable systems, structure, operations, maintenance, repair, and troubleshooting in accordance with maintenance data. The student shall be able to demonstrate the use of manuals and approved procedures, including the knowledge of relevant inspections and limitations.

(b) Level of training:

Training levels are those levels defined in point 2 above.

After the first type course for category C certifying staff all subsequent courses need only be to level 1.

During a level 3 theoretical training, level 1 and 2 training material may be used to teach the full scope of the chapter if required. However, during the training the majority of the course material and training time shall be at the higher level.

(c)  Duration:

The theoretical training minimum tuition hours are contained in the following table:

Category

Hours

Aeroplanes with a maximum take-off mass above 30000 kg:

B1.1

150

B1.2

120

B2

100

C

30

Aeroplanes with a maximum take-off mass equal or less than 30000 kg and above 5700 kg:

B1.1

120

B1.2

100

B2

100

C

25

Aeroplanes with a maximum take-off mass of 5700 kg and below33 For non-pressurised piston engine aeroplanes below 2 000 kg MTOM, the minimum duration can be reduced by 50 %.

B1.1

80

B1.2

60

B2

60

C

15

Helicopters34 For helicopters in Group 2 (as defined in point 66.A.5), the minimum duration can be reduced by 30 %.

B1.3

120

B1.4

100

B2

100

C

25

For the purpose of the table above, a tuition hour means 60 minutes of teaching and exclude any breaks, examination, revision, preparation and aircraft visit.

These hours apply only to theoretical courses for complete aircraft/engine combinations according to the type rating as defined by the Agency.

(d) Justification of course duration:

Training courses carried out in a maintenance training organisation approved in accordance with Annex IV (Part-147) and courses directly approved by the competent authority shall justify their hour duration and the coverage of the full syllabus by a training needs analysis based on:

               the design of the aircraft type, its maintenance needs and the types of operation,

               detailed analysis of applicable chapters — see contents table in point 3.1(e) below,

               detailed competency analysis showing that the objectives as stated in point 3.1(a) above are fully met.

Where the training needs analysis shows that more hours are needed, course lengths shall be longer than the minimum specified in the table.

Similarly, tuition hours of differences courses or other training course combinations (such as combined B1/B2 courses), and in cases of theoretical type training courses below the figures given in point 3.1(c) above, these shall be justified to the competent authority by the training needs analysis as described above.

In addition, the course must describe and justify the following:

               The minimum physical and/or virtual classroom attendance required of the trainee, in order to meet the objectives of the course.

               The maximum number of hours of physical and/or virtual classroom training per day, taking into account pedagogical and human factors principles.

If the minimum attendance required is not met, the certificate of recognition shall not be issued. Additional training may be provided by the training organisation in order to meet the minimum attendance time.

(e) Content:

As a minimum, the elements in the Syllabus below that are specific to the aircraft type shall be covered. Additional elements introduced due to type variations, technological changes, etc. shall also be included.

The training syllabus shall be focused on mechanical and electrical aspects for B1 personnel, and electrical and avionic aspects for B2.

If it exists, the minimum syllabus of the operational suitability data (OSD), established in accordance with Regulation (EU) No 748/2012, shall be included.

Level

Chapters

Aeroplanes turbine

Aeroplanes piston

Helicopters turbine

Helicopters piston

Avionics

Licence category

B1

C

B1

C

B1

C

B1

C

B2

Introduction module:

 

 

 

 

 

 

 

 

 

05 Time limits/maintenance checks

1

1

1

1

1

1

1

1

1

06 Dimensions/Areas (MTOM, etc.)

1

1

1

1

1

1

1

1

1

07 Lifting and Shoring

1

1

1

1

1

1

1

1

1

08 Levelling and weighing

1

1

1

1

1

1

1

1

1

09 Towing and taxiing

1

1

1

1

1

1

1

1

1

10 Parking/mooring, Storing and Return to Service

1

1

1

1

1

1

1

1

1

11 Placards and Markings

1

1

1

1

1

1

1

1

1

12 Servicing

1

1

1

1

1

1

1

1

1

20 Standard practices — only type particular

1

1

1

1

1

1

1

1

1

Helicopters

 

 

 

 

 

 

 

 

 

18 Vibration and Noise Analysis (Blade tracking)

3

1

3

1

60 Standard Practices Rotor

3

1

3

1

62 Rotors

3

1

3

1

1

62A Rotors — Monitoring and indicating

3

1

3

1

3

63 Rotor Drives

3

1

3

1

1

63A Rotor Drives — Monitoring and indicating

3

1

3

1

3

64 Tail Rotor

3

1

3

1

1

64A Tail rotor — Monitoring and indicating

3

1

3

1

3

65 Tail Rotor Drive

3

1

3

1

1

65A Tail Rotor Drive — Monitoring and indicating

3

1

3

1

3

66 Folding Blades/Pylon

3

1

3

1

67 Rotors Flight Control

3

1

3

1

53 Airframe Structure (Helicopter)

3

1

3

1

25 Emergency Flotation Equipment

3

1

3

1

1

Airframe structures

 

 

 

 

 

 

 

 

 

51 Standard practices and structures (damage classification, assessment and repair)

3

1

3

1

1

53 Fuselage

3

1

3

1

1

54 Nacelles/Pylons

3

1

3

1

1

55 Stabilisers

3

1

3

1

1

56 Windows

3

1

3

1

1

57 Wings

3

1

3

1

1

52 Doors

3

1

3

1

1

Zonal and Station Identification Systems.

1

1

1

1

1

1

1

1

1

Airframe systems:

 

 

 

 

 

 

 

 

 

21 Air Conditioning

3

1

3

1

3

1

3

1

3

21A Air Supply

3

1

3

1

3

1

3

1

2

21B Pressurisation

3

1

3

1

3

1

3

1

3

21C Safety and Warning Devices

3

1

3

1

3

1

3

1

3

22 Autoflight

2

1

2

1

2

1

2

1

3

23 Communications

2

1

2

1

2

1

2

1

3

24 Electrical Power

3

1

3

1

3

1

3

1

3

25 Equipment and Furnishings

3

1

3

1

3

1

3

1

1

25A Electronic Equipment including emergency equipment

1

1

1

1

1

1

1

1

3

26 Fire Protection

3

1

3

1

3

1

3

1

3

27 Flight Controls

3

1

3

1

3

1

3

1

2

27A Sys. Operation: Electrical/Fly-by-Wire

3

1

3

28 Fuel Systems

3

1

3

1

3

1

3

1

2

28A Fuel Systems — Monitoring and indicating

3

1

3

1

3

1

3

1

3

29 Hydraulic Power

3

1

3

1

3

1

3

1

2

29A Hydraulic Power — Monitoring and indicating

3

1

3

1

3

1

3

1

3

30 Ice and Rain Protection

3

1

3

1

3

1

3

1

3

31 Indicating/Recording Systems

3

1

3

1

3

1

3

1

3

31A Instrument Systems

3

1

3

1

3

1

3

1

3

32 Landing Gear

3

1

3

1

3

1

3

1

2

32A Landing Gear — Monitoring and indicating

3

1

3

1

3

1

3

1

3

33 Lights

3

1

3

1

3

1

3

1

3

34 Navigation

2

1

2

1

2

1

2

1

3

35 Oxygen

3

1

3

1

2

36 Pneumatic

3

1

3

1

3

1

3

1

2

36A Pneumatic — Monitoring and indicating

3

1

3

1

3

1

3

1

3

37 Vacuum

3

1

3

1

3

1

3

1

2

38 Water/Waste

3

1

3

1

2

41 Water Ballast

3

1

3

1

1

42 Integrated modular avionics

2

1

2

1

2

1

2

1

3

44 Cabin Systems

2

1

2

1

2

1

2

1

3

45 On-Board Maintenance System (or covered in 31)

3

1

3

1

3

1

3

46 Information Systems

2

1

2

1

2

1

2

1

3

47 Nitrogen generation system

3

1

3

1

2

50 Cargo and Accessory Compartments

3

1

3

1

3

1

3

1

1

55/57 Flight control surfaces (All)

3

1

3

1

1

Turbine Engine

 

 

 

 

 

 

 

 

 

70 Standard Practices — Engines,

3

1

3

1

1

70A constructional arrangement and operation (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems).

3

1

3

1

1

70B Engine Performance

3

1

3

1

1

71 Powerplant

3

1

3

1

1

72 Engine Turbine/Turbo Prop/Ducted Fan/Unducted fan

3

1

3

1

1

73 Engine Fuel and Control

3

1

3

1

1

75 Air

3

1

3

1

1

76 Engine controls

3

1

3

1

1

78 Exhaust

3

1

3

1

1

79 Oil

3

1

3

1

1

80 Starting

3

1

3

1

1

82 Water Injections

3

1

3

1

1

83 Accessory Gear Boxes

3

1

3

1

1

84 Propulsion Augmentation

3

1

3

1

1

73A FADEC

3

1

3

1

3

74 Ignition

3

1

3

1

3

77 Engine Indicating Systems

3

1

3

1

3

49 Auxiliary Power Units (APUs)

3

1

2

Piston Engine

 

 

 

 

 

 

 

 

 

70 Standard Practices — Engines

3

1

3

1

1

70A Constructional arrangement and operation (Installation, Carburettors, Fuel injection systems, Induction, Exhaust and Cooling Systems, Supercharging/Turbochargin, Lubrication Systems).

3

1

3

1

1

70B Engine Performance

3

1

3

1

1

71 Powerplant

3

1

3

1

1

73 Engine Fuel and Control

3

1

3

1

1

76 Engine Control

3

1

3

1

1

79 Oil

3

1

3

1

1

80 Starting

3

1

3

1

1

81 Turbines

3

1

3

1

1

82 Water Injections

3

1

3

1

1

83 Accessory Gear Boxes

3

1

3

1

1

84 Propulsion Augmentation

3

1

3

1

1

73A FADEC

3

1

3

1

3

74 Ignition

3

1

3

1

3

77 Engine Indication Systems

3

1

3

1

3

Propellers

 

 

 

 

 

 

 

 

 

60A Standard Practices — Propeller

3

1

3

1

1

61 Propellers/Propulsion

3

1

3

1

1

61A Propeller Construction

3

1

3

1

61B Propeller Pitch Control

3

1

3

1

61C Propeller Synchronising

3

1

3

1

1

61D Propeller Electronic control

2

1

2

1

3

61E Propeller Ice Protection

3

1

3

1

61F Propeller Maintenance

3

1

3

1

1

3.2. Practical element

Regulation (EU) 2023/989

(a) Objective:

The objective of practical training is to gain the required competence in performing safe maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging and functional checks. It includes the awareness of the use of all technical literature and documentation for the aircraft, the use of specialist/special tooling and test equipment for performing removal and replacement of components and modules unique to type, including any on-wing maintenance activity.

(b) Content:

At least 50 % of the crossed items in the table below, which are relevant to the particular aircraft type, shall be completed as part of the practical training.

Tasks crossed represent subjects that are important for practical training purposes to ensure that the operation, function, installation and safety significance of key maintenance tasks is adequately addressed; particularly where these cannot be fully explained by theoretical training alone. Although the list details the minimum practical training subjects, other items may be added where applicable to the particular aircraft type.

Tasks to be completed shall be representative of the aircraft and systems both in complexity and in the technical input required to complete that task. While relatively simple tasks may be included, other more complex tasks shall also be incorporated and undertaken as appropriate to the aircraft type.

If it exists, the minimum list of practical tasks of the operational suitability data (OSD), established in accordance with Regulation (EU) No 748/2012, shall be part of the practical elements to be selected.

Glossary of the table: LOC: Location; FOT: Functional/Operational Test; SGH: Service and Ground Handling; R/I: Removal/Installation; MEL: Minimum Equipment List; TS: TroubleShooting.

Chapters

 

B1/B2

B1

B2

LOC

FOT

SGH

R/I

MEL

TS

FOT

SGH

R/I

MEL

TS

Introduction module:

 

 

 

 

 

 

 

 

 

 

 

5 Time limits/maintenance checks

X/X

6 Dimensions/Areas (MTOM, etc.)

X/X

7 Lifting and Shoring

X/X

8 Levelling and weighing

X/X

X

X

9 Towing and taxiing

X/X

X

X

10 Parking/mooring, Storing and Return to Service

X/X

X

X

11 Placards and Markings

X/X

12 Servicing

X/X

X

X

20 Standard practices — only type particular

X/X

X

X

Helicopters:

 

 

 

 

 

 

 

 

 

 

 

18 Vibration and Noise Analysis (Blade tracking)

X/—

X

60 Standard Practices Rotor — only type specific

X/X

X

X

62 Rotors

X/—

X

X

X

62A Rotors — Monitoring and indicating

X/X

X

X

X

X

X

X

X

63 Rotor Drives

X/—

X

X

63A Rotor Drives — Monitoring and indicating

X/X

X

X

X

X

X

X

64 Tail Rotor

X/—

X

X

64A Tail rotor -Monitoring and indicating

X/X

X

X

X

X

X

X

65 Tail Rotor Drive

X/—

X

X

65A Tail Rotor Drive — Monitoring and indicating

X/X

X

X

X

X

X

X

66 Folding Blades/Pylon

X/—

X

X

X

67 Rotors Flight Control

X/—

X

X

X

X

53 Airframe Structure (Helicopter)

Note: covered under Airframe structures

 

 

 

 

 

 

 

 

 

 

 

25 Emergency Flotation Equipment

X/X

X

X

X

X

X

X

X

Airframe structures:

 

 

 

 

 

 

 

 

 

 

 

51 Standard Practices and Structures (damage classification, assessment and repair)

 

 

 

 

 

 

 

 

 

 

 

53 Fuselage

X/—

X

54 Nacelles/Pylons

X/—

55 Stabilisers

X/—

56 Windows

X/—

X

57 Wings

X/—

52 Doors

X/X

X

X

X

Airframe systems:

 

 

 

 

 

 

 

 

 

 

 

21 Air Conditioning

X/X

X

X

X

X

X

X

X

X

21A Air Supply

X/X

X

X

21B Pressurisation

X/X

X

X

X

X

X

X

21C Safety and warning Devices

X/X

X

X

22 Autoflight

X/X

X

X

X

X

X

X

23 Communications

X/X

X

X

X

X

X

X

X

24 Electrical Power

X/X

X

X

X

X

X

X

X

X

X

X

25 Equipment and Furnishings

X/X

X

X

X

X

X

X

25A Electronic Equipment including emergency equipment

X/X

X

X

X

X

X

X

26 Fire Protection

X/X

X

X

X

X

X

X

X

X

X

X

27 Flight Controls

X/X

X

X

X

X

X

X

27A Sys. Operation: Electrical/Fly-by-Wire

X/X

X

X

X

X

X

X

X

28 Fuel Systems

X/X

X

X

X

X

X

X

X

X

28A Fuel Systems — Monitoring and indicating

X/X

X

X

X

X

29 Hydraulic Power

X/X

X

X

X

X

X

X

X

X

29A Hydraulic Power — Monitoring and indicating

X/X

X

X

X

X

X

X

X

X

30 Ice and Rain Protection

X/X

X

X

X

X

X

X

X

X

31 Indicating/Recording Systems

X/X

X

X

X

X

X

X

X

X

X

X

31A Instrument Systems

X/X

X

X

X

X

X

X

X

X

X

X

32 Landing Gear

X/X

X

X

X

X

X

X

X

X

X

32A Landing Gear — Monitoring and indicating

X/X

X

X

X

X

X

X

X

X

33 Lights

X/X

X

X

X

X

X

X

X

34 Navigation

X/X

X

X

X

X

X

X

X

35 Oxygen

X/—

X

X

X

X

X

36 Pneumatic

X/—

X

X

X

X

X

X

X

X

36A Pneumatic — Monitoring and indicating

X/X

X

X

X

X

X

X

X

X

X

X

37 Vacuum

X/—

X

X

X

X

38 Water/Waste

X/—

X

X

X

X

41 Water Ballast

X/—

42 Integrated modular avionics

X/X

X

X

X

X

X

44 Cabin Systems

X/X

X

X

X

X

X

45 On-Board Maintenance System (or covered in 31)

X/X

X

X

X

X

X

X

X

X

X

X

46 Information Systems

X/X

X

X

X

X

47 Nitrogen generation system

X/X

X

X

X

X

X

X

X

50 Cargo and Accessory Compartments

X/X

X

55/57 Flight control surfaces

X/—

X

Turbine/Piston Engine Module:

 

 

 

 

 

 

 

 

 

 

 

70 Standard Practices — Engines — only type particular

X

X

70A Constructional arrangement and operation (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X

Turbine engines:

 

 

 

 

 

 

 

 

 

 

 

70B Engine Performance

X

71 Power Plant

X/—

X

X

X

72 Engine Turbine/Turbo Prop/Ducted Fan/ Unducted fan

X/—

73 Engine Fuel and Control

X/X

X

73A FADEC Systems

X/X

X

X

X

X

X

X

X

X

74 Ignition

X/X

X

X

75 Air

X/—

X

X

76 Engine Controls

X/—

X

X

77 Engine Indicating

X/X

X

X

X

X

X

X

78 Exhaust

X/—

X

X

79 Oil

X/—

X

X

80 Starting

X/—

X

X

X

82 Water Injection

X/—

X

83 Accessory Gearboxes

X/—

X

84 Propulsion Augmentation

X/—

X

Auxiliary Power Units (APUs):

 

 

 

 

 

 

 

 

 

 

 

49 Auxiliary Power Units (APUs)

X/—

X

X

X

Piston Engines:

 

 

 

 

 

 

 

 

 

 

 

70 Standard Practices — Engines — only type particular

X

X

70A Constructional arrangement and operation (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X

70B Engine Performance

X

71 Power Plant

X/—

X

X

X

73 Engine Fuel and Control

X/X

X

73A FADEC Systems

X/X

X

X

X

X

X

X

X

X

X

74 Ignition

X/X

X

X

76 Engine Controls

X/—

X

X

77 Engine Indicating

X/X

X

X

X

X

X

X

78 Exhaust

X/—

X

X

X

79 Oil

X/—

X

X

80 Starting

X/—

X

X

X

81 Turbines

X/—

X

X

X

X

82 Water Injection

X/—

X

83 Accessory Gearboxes

X/—

X

X

84 Propulsion Augmentation

X/—

X

Propellers:

 

 

 

 

 

 

 

 

 

 

 

60A Standard Practices — Propeller

X

61 Propellers/ Propulsion

X/X

X

X

X

X

61A Propeller Construction

X/X

X

61B Propeller Pitch Control

X/—

X

X

X

X

61C Propeller Synchronising

X/—

X

X

X

61D Propeller Electronic control

X/X

X

X

X

X

X

X

X

X

X

X

61E Propeller Ice Protection

X/—

X

X

X

X

61F Propeller Maintenance

X/X

X

X

X

X

X

X

X

X

X

X

4.1. Theoretical element examination standard

Regulation (EU) 2023/989

After the theoretical portion of the aircraft type training has been completed, a written examination shall be performed, which shall comply with the following:

(a) Format of the examination is of the multi-choice type. Each multi-choice question shall have 3 alternative answers of which only one shall be the correct answer. The total time is based on the total number of questions and the time for answering is based upon a nominal average of 90 seconds per question.

(b) The incorrect alternatives shall seem equally plausible to anyone ignorant of the subject. All the alternatives shall be clearly related to the question and of similar vocabulary, grammatical construction and length.

(c) In numerical questions, the incorrect answers shall correspond to procedural errors such as the use of incorrect sense (+ versus -) or incorrect measurement units. They shall not be mere random numbers.

(d) The level of examination for each chapter35For the purpose of this point 4, a ‘chapter’ means each one of the rows preceded by a number in the table contained in point 3.1(e). shall be the one defined in point 2 ‘Aircraft type training levels’. However, the use of a limited number of questions at a lower level is acceptable.

(e) The examination shall be of the closed book type. No reference material is permitted. An exception will be made for the case of examining a B1 or B2 candidate's ability to interpret technical documents.

(f)  The number of questions shall be at least one question per hour of training. The number of questions for each chapter and level shall be proportionate to:

               the effective training hours spent on teaching at that chapter and level; or

               in case of student-centred methods, the anticipated average time to complete the training; and

               the learning objectives as given by the training needs analysis.

The competent authority shall assess the number and the level of the questions when approving the course.

(g) The minimum examination pass mark is 75 %. When the type training examination is split in several examinations, each examination shall be passed with at least a 75 % mark. In order to be possible to achieve exactly a 75 % pass mark, the number of questions in the examination shall be a multiple of 4.

(h) Penalty marking (negative points for failed questions) is not to be used.

(i)  End of module phase examinations cannot be used as part of the final examination unless they contain the correct number and level of questions required.

(j) Whilst it is accepted that the subject matter of the questions may be the same, the questions used as part of the MBT learning programme shall not be used in course or phase examinations.

4.2. Practical element assessment standard

Regulation (EU) No 1321/2014

After the practical element of the aircraft type training has been completed, an assessment must be performed, which must comply with the following:

(a) The assessment shall be performed by designated assessors appropriately qualified.

(b) The assessment shall evaluate the knowledge and skills of the trainee.

5. Type evaluation standard for Group 2 and Group 3 aircraft

Regulation (EU) 2023/989

Type evaluation relative to aircraft of Group 2 or Group 3 shall be conducted by training organisations appropriately approved in accordance with Annex IV (Part-147) or by the competent authority.

The evaluation shall consist of practical assessment and oral examination and comply with the following requirements:

(a) The practical assessment shall determine the candidate’s competence to perform maintenance tasks applicable to the particular aircraft type.

(b) The oral examination shall be on a sample of chapters drawn from point 3. ‘Aircraft type training standard’, at the indicated level in point 3.1.(e).

(c) Both oral examinations and practical assessments shall ensure that the following objectives are met:

1. properly discuss with confidence the aircraft type and its systems;

2. ensure safe performance of maintenance, inspections, and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example, troubleshooting, repairs, adjustments, replacements, rigging and functional checks such as engine run, etc., if required;.

3. correctly use all technical literature and documentation for the aircraft;

4. correctly use specialist/special tooling and test equipment, perform removal and replacement of components and modules unique to type, including any on-wing maintenance activity.

(d) The following conditions apply to the type evaluation:

1. The maximum number of attempts for each examination is three in a 12-month period. A waiting period of 30 days is required after the first failed attempt within one set, and a waiting period of 60 days is required after the second failed attempt.

The applicant shall confirm in writing to the maintenance training organisation or the competent authority to which they apply for an examination, the number, and dates of attempts during the last 12-month period and the maintenance training organisation or the competent authority where these attempts took place. The maintenance training organisation or the competent authority is responsible for checking the number of attempts within the applicable time frames.

2. The type evaluation shall be passed, and the required practical experience shall be completed within the 3 years preceding the application for the rating endorsement on the aircraft maintenance licence.

3. Type evaluation shall be performed with at least one examiner present. The examiner(s) shall not have been involved in the applicant’s training.

(e) A written and signed report shall be prepared and made available to the candidate by the examiner(s) to explain why the candidate has passed or failed.

6. On-the-job training (OJT)

Regulation (EU) 2023/989

6.1 General

The OJT is the training that the applicant is given on a particular aircraft type in a real workplace, having the possibility to learn maintenance best practices and correct release-to-service procedures. The OJT shall comply with the following requirements:

(a) The list of the OJT tasks and programme shall be accepted by the competent authority which has issued the maintenance licence before starting the OJT training.

(b) The OJT shall be conducted at one or more maintenance organisations appropriately approved according to this Regulation for the maintenance of that aircraft type. One of those organisations shall control the OJT.

(c) The applicant shall have a category A, B or L5 licence before undergoing the OJT or have finished the theoretical type training and cumulated at least 50 % of the basic experience requirement (point 66.A.30) as regards the category of aircraft he or she is trained for.

(d) The applicant shall start and complete the OJT within 3 years preceding the application for the first type rating endorsement. At least 50 % of the OJT tasks shall take place after the related aircraft theoretical type training has been completed.

(e) The applicant shall undergo the OJT under the mentorship of a qualified mentor or mentors, on a one-to-one supervision basis, during which the mentors verify the technical knowledge, the skills, and responsibilities of a typical certifying staff. During the OJT, the mentors transmit also knowledge and experience to the applicant, providing the necessary advice, support, and guidance.

(f) Each task shall be signed off by the applicant and refer to an actual job card/work sheet, etc. The mentors shall verify and countersign off the tasks performed during the OJT, because they shall assume the responsibility for the tasks at support staff or certifying staff level, as applicable, depending on the release-to-service procedure.

(g) At the satisfactory completion of the OJT programme, the mentors shall issue a recommendation for the final assessment of the applicant to be conducted by designated assessors.

6.2 OJT content and OJT logbook

The OJT shall include a series of activities and tasks representative of the aircraft type rating, systems, and licence category applied for and may cover more than one licence category.

The OJT shall be documented in an OJT logbook reporting the following:

(a) name of the applicant;

(b) date of birth of the applicant;

(c) the approved maintenance organisation(s) where the OJT was carried out;

(d) aircraft rating and licence categories applied for;

(e) list of tasks, including:

(i) task description;

(ii) reference to job card/work order/aircraft tech log, etc.;

(iii) location of task completion;

(iv) date of task completion;

(v) aircraft registration(s).

(f) names of the mentors (including licence number, if applicable);

(g) a signed recommendation of the mentors for the successive final assessment of the applicant.

6.3 Final assessment of the applicant

The final assessment of the applicant may only be performed once the OJT logbook has been completed and the mentors have signed the related recommendation.

The designated assessor(s) conducting the final assessment shall notify the date of the assessment to the licensing authority well in advance to allow a possible participation of the same authority.

The objective of the final assessment is to verify that the applicant has sufficient technical knowledge as well as the appropriate skills and attitude and that he or she is competent to work independently as type-rated certifying staff on a particular aircraft type.

The final assessment shall have a minimum duration of one working day.

(a) The assessment shall sample:

(1) the general technical knowledge required for the particular licence category;

(2) the aircraft-type-specific knowledge and skills for the particular licence category;

(3) the understanding of the licence privileges relevant to the aircraft and to the licence category;

(4) the appropriate behaviour and safety attitude of the applicant in relation to the maintenance environment.

(b) The assessment shall be recorded in a report containing the following information:

(1) identification data of the applicant;

(2) identification data of the assessor(s);

(3) date and time frame of the assessment;

(4) content of the assessment;

(5) result of the assessment: Passed or Failed.

(6) signature of the assessor(s), the candidate and, if applicable, the independent observer(s).

(c) A failed assessment may be retaken after 3 months or, if additional training has been received and a new recommendation by the mentors has been made, earlier than 3 months if agreed by the assessor(s). After three failed attempts, the complete OJT shall be repeated.

6.4 Requirements for mentors and assessors

Mentors and assessors are maintenance staff with the following qualifications:

(i) Mentors:

               hold a valid aircraft maintenance licence (AML) issued in accordance with this Annex or a valid and fully compliant with ICAO Annex 1 AML in accordance with Appendix IV to Annex II (Part-145), which is acceptable to the competent authority;

               have been holding, for at least 1 year, an AML in the same category, when compared to the one for which the OJT is being mentored, that is endorsed with a type rating appropriate to exercise the privileges on the related aircraft;

               have the necessary release or sign-off privileges in the maintenance organisation where the OJT is performed;

               have experience in training other people (such as being apprenticeship instructors, instructors in accordance with Annex IV (Part-147), having received train-the-trainer courses or having any other comparable national qualification, or having a training to do so that is acceptable to the competent authority).

(ii) Assessors of the final assessment:

               hold a valid AML issued in accordance with this Annex or a valid and fully compliant with ICAO Annex 1 AML in accordance with Appendix IV to Annex II (Part-145), which is acceptable to the competent authority;

               have been holding, for at least 3 years, an AML in the same category, when compared to the one for which the OJT is being assessed, endorsed with the same or similar aircraft type rating;

               have experience and/or have received training in assessing others (such as being apprenticeship instructors, examiners in accordance with Annex IV (Part-147), having received train-the-trainer courses, or having any other comparable national qualification, or having a training to do so that is acceptable to the competent authority);

               shall not have been involved as a mentor of the applicant in the OJT; when the assessor has taken part in the OJT performance, then an independent observer shall be present during the OJT assessment.

6.5 OJT documentation and records

The satisfactory accomplishment of the OJT shall be attested to the applicant with the final assessment report and the OJT logbook.

The OJT documentation shall be provided to the competent authority to support the application for the issue or change of the licence as laid down in Section B, Subpart B, of this Annex.

Records of the OJT documentation shall be kept by the maintenance organisation where the OJT is conducted, in accordance with the procedures agreed with the competent authority of the maintenance organisation.

AMC to Appendix III to Part-66 ‘Aircraft Type Training and Examination Standard. On-the-Job Training’

ED Decision 2015/029/R

Aircraft Type Training and On-the-Job Training

The theoretical and practical training providers, as well as the OJT provider, may contract the services of a language translator in the case where training is imparted to students not conversant in the language of the training material. Nevertheless, it remains essential that the students understand all the relevant maintenance documentation.

During the performance of examinations and assessments, the assistance of the translator should be limited to the translation of the questions, but should not provide clarifications or help in relation to those questions.

AMC1 Appendix III Aircraft type training and type evaluation standard — on-the-job training (OJT) Section 1

ED Decision 2023/019/R

Aircraft Type Training

1. Aircraft type training may be sub-divided in airframe and/or powerplant and/or avionics/electrical systems type training courses.

               Airframe type training course means a type training course including all relevant aircraft structure and electrical and mechanical systems excluding the powerplant.

               Powerplant type training course means a type training course on the bare engine, including the build-up to a quick engine change unit.

               The interface of the engine/airframe systems should be addressed by either airframe or powerplant type training course. In some cases, such as for general aviation, it may be more appropriate to cover the interface during the airframe course due to the large variety of aircraft that can have the same engine type installed.

               Avionics/electrical systems type training course means type training on avionics and electrical systems covered by but not necessarily limited to ATA (Air Transport Association) Chapters 22, 23, 24, 25, 27, 31, 33, 34, 42, 44, 45, 46, 73 and 77 or equivalent.

2. Practical training may be performed either following or integrated with the theoretical elements. However, it should not be performed before theoretical training.

3. The content of the theoretical and practical training should:

               address the different parts of the aircraft which are representative of the structure, the systems/components installed and the cabin; and

               include training on the use of technical manuals, maintenance procedures and the interface with the operation of the aircraft.

Therefore it should be based on the following elements:

               Type design including relevant type design variants, new technology and techniques;

               Feedback from in-service difficulties, occurrence reporting, etc;

               Significant applicable airworthiness directives and service bulletins;

               Known human factor issues associated with the particular aircraft type;

               Use of common and specific documentation, (when applicable, such as MMEL, AMM, MPD, TSM, SRM, WD, AFM, tool handbook), philosophy of the troubleshooting, etc.;

               Knowledge of the maintenance on-board reporting systems and ETOPS maintenance conditions where applicable;

               Use of special tooling and test equipment and specific maintenance practises including critical safety items and safety precautions;

               Significant and critical tasks/aspects from the MMEL, CDL, Fuel Tank Safety (FTS), airworthiness limitation items (ALI) including Critical Design Configuration Control Limitations (CDCCL), CMR and all ICA documentation such as MRB, MPD, SRM, AMM, etc., when applicable.

               Maintenance actions and procedures to be followed as a consequence of specific certification requirements, such as, but not limited to, RVSM (Reduced Vertical Separation Minimum) and NVIS (Night Vision Imaging Systems);

               Knowledge of relevant inspections and limitations as applicable to the effects of environmental factors or operational procedures such as cold and hot climates, wind, moisture, sand, de-icing / anti-icing, etc.

The type training does not necessarily need to include all possible customer options corresponding to the type rating described in the Appendix I to AMC to Part-66.

4. Limited avionic system training should be included in the category B1 type training as the B1 privileges include work on avionics systems requiring simple tests to prove their serviceability.

5. Electrical systems should be included in both categories of B1 and B2 type training.

6. The theoretical and practical training should be complementary and may be:

               integrated or split;

               supported by the use of training aids, such as trainers, virtual aircraft, aircraft components, maintenance simulation training devices (MSTDs) and maintenance training devices (MTDs).

7. The integration and usage of MSTDs and MTDs, as defined in AMC 147.A.30(a), in maintenance type training (theoretical and/or practical) should consider the following:

                The use of actual aircraft components should be allowed for any MSTD or MTD, even if the components are in a non-airworthy condition.

                The complexity and degree of simulation for an MSTD may vary and should support type training elements that address a component, a system or the entire aircraft. Based on its characteristics and capabilities, the MSTD may be:

                a training device capable of providing, for the respective component or system, the representation of aircraft location, access and layout, and for servicing with an acceptable level of accuracy and limited simulation; or

                a training device capable of providing, for the respective component or system, the representation of aircraft location, access and layout with sufficient accuracy and with interactive simulation for servicing, and the applicable maintenance data for operational (O) and functional (F) test elements including built-in test (BIT) initiation and monitoring from outside the cockpit; such representation should have the capability to accommodate some troubleshooting scenarios; or

                a training device capable of providing, for the respective component or system, the representation of onboard (flight deck/cockpit or cabin) indication and controls with an acceptable level of accuracy and limited interactive simulation; or

                a training device capable of providing, for the respective component or system, the representation of onboard (flight deck/cockpit or cabin) indication and controls with sufficient accuracy and with interactive simulation for servicing, and the applicable maintenance data for operational (O) and functional (F) test elements including built-in test (BIT) initiation and monitoring; such representation should have the capability to accommodate some troubleshooting scenarios; or

                any combination of the above.

                Flight simulation training devices (FSTDs) may be used as MSTDs whenever their characteristics and capabilities are considered appropriate for, and supportive of, the delivery of the respective maintenance training element(s).

                An MTD is any training device other than an MSTD used for maintenance training and/or examination and/or assessment.

AMC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III to Part-66 ‘Aircraft Type Training and Examination Standard. On-the-Job Training’

ED Decision 2015/029/R

Practical Element of the Aircraft Type Training

1. The practical training may include instruction in a classroom or in simulators but part of the practical training should be conducted in a real maintenance or manufacturer environment.

2. The tasks should be selected because of their frequency, complexity, variety, safety, criticality, novelty, etc. The selected tasks should cover all the chapters described in the table contained in paragraph 3.2 of Appendix III to Part-66.

3. The duration of the practical training should ensure that the content of training required by paragraph 3.2 of Appendix III to Part-66 is completed.

Nevertheless, for aeroplanes with a MTOM equal or above 30000kg, the duration for the practical element of a type rating training course should not be less than two weeks unless a shorter duration meeting the objectives of the training and taking into account pedagogical aspects (maximum duration per day) is justified to the competent authority.

4. The organisation providing the practical element of the type training should provide trainees a schedule or plan indicating the list of tasks to be performed under instruction or supervision. A record of the tasks completed should be entered into a logbook which should be designed such that each task or group of tasks may be countersigned by the designated assessor. The logbook format and its use should be clearly defined.

5. In paragraph 4.2 of Appendix III to Part-66, the term ‘designated assessors appropriately qualified’ means that the assessors should demonstrate training and experience on the assessment process being undertaken and be authorised to do so by the organisation.

Further guidance about the assessment and the designated assessors is provided in Appendix III to AMC to Part-66.

6. The practical element (for powerplant and avionic systems) of the Type Rating Training may be subcontracted by the approved Part-147 organisation under its quality system according to the provisions of 147.A.145(d)3 and the corresponding Guidance Material.

AMC to Paragraph 1(c) of Appendix III to Part-66 ‘Aircraft Type Training and Examination Standard. On-the-Job Training’

ED Decision 2015/029/R

Differences Training

Approved difference training is not required for different variants within the same aircraft type rating (as specified in Appendix I to AMC to Part-66) for the purpose of type rating endorsement on the aircraft maintenance licence.

However, this does not necessarily mean that no training is required before a certifying staff authorisation can be issued by the maintenance organisation (refer to AMC 66.A.20(b)3).

DIFFERENCES TRAINING

If the holder of a B1 and B2 licence, without any type rating, successfully completes a combined type training course (B1 + B2) followed by an OJT tailored only to B1 tasks, they can obtain only the type-rating endorsement that is applicable to the B1 subcategory.

Within the next 3 years from the completion of the combined training course, endorsement of the aircraft type for the B2 category is possible after carrying out an OJT programme limited to the tasks relevant to the B2 category only.

When instead, the aircraft type endorsement would be requested after more than 3 years, the applicant would be required to also pass a differences type training course (from B1 to B2) plus the OJT programme limited to the tasks relevant to the B2 category only. All common theoretical and practical elements, and OJT tasks, already demonstrated as B1, shall be considered fulfilled.

AIRCRAFT TYPE TRAINING STANDARD

Training methods are categorised as ‘instructor-centred’, ‘student-centred’ and ‘blended training’.

The actual training method and the training tools should be adapted to suit the training subject and be chosen considering their intrinsic characteristics, such as but not limited to their efficiency and the pedagogical benefits of the method/tool.

A complex or critical subject should not normally be taught solely through a student-centred method unless provisions are in place to verify the actual and progressive acquisition of knowledge of the student.

Complex and critical areas should be identified by the training needs analysis (TNA). The complexity and criticality of the areas could differ on a case-by-case basis (that is, areas proven to be critical by organisations’ ‘in-service events’, occurrence reporting, human factors, safety, etc.), but should in any case cover the maintenance areas with special emphasis (MASE) identified by the type-certificate holder (TCH) in its operational suitability data (OSD).

AMC1 Appendix III Aircraft type training and type evaluation – on-the-job training (OJT) Section 3.1(d)

ED Decision 2023/019/R

Training needs analysis (TNA) for the theoretical element of the aircraft type training

1. The minimum duration for the theoretical element of the type rating training course, as described in Appendix III to Part-66, has been determined based on:

               generic categories of aircraft and minimum standard equipment fit

               the estimated average duration of standard courses imparted in Europe

2. The purpose of the Training Needs Analysis (TNA) is to adapt and justify the duration of the course for a specific aircraft type. This means that the TNA is the main driver for determining the duration of the course, regardless of whether it is above or below the minimum duration described in Appendix III to Part-66.

In the particular case of type training courses approved on the basis of the requirements valid before Regulation (EU) No 1149/2011 was applicable (1 August 2012) and having a duration for the theoretical element equal to or above the minimum duration contained in paragraph 3.1(c) of Appendix III to Part-66, it is acceptable that the TNA only covers the differences introduced by Regulation (EU) No 1149/2011 in paragraph 3.1(e) ‘Content’ and the criteria introduced in paragraph 3.1(d) ‘Justification of course duration’ related to the minimum attendance and the maximum number of training hours per day. This TNA may result in a change in the duration of the theoretical element.

3. The content and the duration deriving from this TNA may be supported by an analysis from the Type Certificate holder.

4. In order to approve the reduction of such minimum duration, the competent authority should perform an assessment on a case-by-case basis, and the assessment should be appropriate to the aircraft type and to the training methods and tools proposed.

For example:

(a) While it would be exceptional for a theoretical course for a large transport category aircraft, such as an A330 or a B777, to be below the minimum duration shown, it would not necessarily be exceptional in the case of a business aircraft, such as a Learjet 45 or similar. The TNA for a business aircraft course could demonstrate that a course of a shorter duration satisfies the applicable requirements.

(b) The use of an MSTD (i.e. flat panel trainer) comprising aircraft-type-specific software may result in the duration of the training being reduced due to a more effective transfer of knowledge.

(c) The use of multimedia-based training (MBT), or blending the training methods, may improve the efficiency of the training and, consequently, contribute to the reduction of the overall time needed to achieve the learning objectives.

5. When developing the TNA, the following should be considered:

(a) The TNA should include an analysis identifying all the areas and elements where there is a need for training as well as the associated learning objectives, considering the design philosophy of the aircraft type, the operational environment, the type of operations and the operational experience. This analysis should be written in a manner which provides a reasonable understanding of which areas and elements constitute the course in order to meet the learning objectives.

(b) As a minimum, the Training Need Analysis (TNA) should take into account all the applicable elements contained in paragraph 3.1 of Part-66 Appendix III and associated AMCs.

(c) The TNA should set-up the course content considering the Appendix III objectives for each level of training and the prescribed topics in the theoretical element table contained in paragraph 3.1 of Part-66 Appendix III.

(d) For each chapter described in the theoretical element table contained in paragraph 3.1 of Part-66 Appendix III, the corresponding training time should be recorded.

(e) Typical documents to be used in order to identify the areas and elements where there is a need for training typically include, among others, the Aircraft Maintenance Manual, MRB report, CMRs, airworthiness limitations, Troubleshooting Manual, Structural Repair Manual, Illustrated Parts Catalogue, Airworthiness Directives and Service Bulletins.

(f) During the analysis of these documents:

               Consideration should be given to the following typical activities:

               Activation/reactivation;

               Removal/Installation;

               Testing;

               Servicing;

               Inspection, check and repairs;

               Troubleshooting / diagnosis.

               For the purpose of identifying the specific elements constituting the training course, it is acceptable to use a filtering method based on criteria such as:

               Frequency of the task;

               Human factor issues associated to the task;

               Difficulty of the task;

               Criticality and safety impact of the task;

               In-service experience;

               Novel or unusual design features (not covered by Part-66 Appendix I);

               Similarities with other aircraft types;

               Special tests and tools/equipment.

               It is acceptable to follow an approach based on:

               Tasks or groups of tasks, or

               Systems or subsystems or components

(g) The TNA should:

               Identify the learning objectives for each task, group of tasks, system, subsystem or component;

               Associate the identified tasks to be trained to the regulatory requirements (table in Paragraph 3.1 of Appendix III to Part-66);

               Organise the training into modules in a logical sequence (adequate combination of chapters as defined in Appendix III of Part-66);

               Determine the sequence of learning (within a lesson and for the whole syllabus);

               Identify the scope of information and level of detail with regard the minimum standard to which the topics of the TNA should be taught according to the set-up objectives.

               Address the following:

               Description of each system/component including the structure (where applicable);

               System/component operation taking into account:

(a) Complexity of the system (e.g. the need of further break down into subsystems, etc.);

(b) Design specifics which may require more detailed presentation or may contribute to maintenance errors;

(c) Normal and emergency functioning;

(d) Troubleshooting;

(e) Interpretation of indications and malfunctions;

(f) Use of maintenance publications;

(g) Identification of special tools and equipment required for servicing and maintaining the aircraft;

(h) Maintenance Practices;

(i) Routine inspections, functional or operational tests, rigging/adjustment, etc.

               Describe the following:

               The instructional methods and training tools and their blended application in order to ensure the effectiveness of the training.

               The maintenance training documentation/material to be delivered to the student.

               Facilitated discussions, questioning session, additional practice-oriented training, etc.

               The homework, if developed, i.e. to support the achievement of the learning objectives while using asynchronous distance-learning or self-learning methods.

               The training provider’s resources available to the learner.

(h) It is acceptable to differentiate between subjects which have to be led by an instructor and subjects which may be delivered through interactive simulation training devices and/or covered by self-paced elements. The overall time of the course will be allocated accordingly.

(i) The maximum number of training hours per day for the theoretical element of type training should not be more than 6 hours. A training hour means 60 minutes of tuition excluding any breaks, examination, revision, preparation and aircraft visit. In exceptional cases, the competent authority may allow deviation from this standard when it is properly justified that the proposed number of hours follows pedagogical and human factors principles. These principles are especially important in those cases where:

               Theoretical and practical training are performed at the same time;

               Training and normal maintenance duty/apprenticeship are performed at the same time.

(j) The minimum participation time in order for the trainee to meet the objectives of the course should not be less than 90 % of the tuition hours, or 95 % completion of the content in case of student-centred methods in a theoretical training course. Additional training may be provided by the training organisation in order to meet the minimum participation time. If the minimum participation defined for the course is not met, a certificate of recognition should not be issued.

(k) The TNA is a living process and should be reviewed/updated based on operation feedback, maintenance occurrences, airworthiness directives, major service bulletins impacting maintenance activities or requiring new competencies for mechanics, alert service bulletins, feedback from trainees or customer satisfaction, evolution of the maintenance documentation such as MRBs, MPDs, MMs, etc. The frequency at which the TNA should be reviewed/updated is left to the discretion of the organisation conducting the course.

NOTE: The examination is not part of the TNA. However, it should be prepared in accordance with the learning objectives described in the TNA.

AMC1 Appendix III Aircraft type training and type evaluation standard — on-the-job training (OJT) Section 4.1

ED Decision 2023/019/R

Type training examination and assessment standard

4.1 Theoretical element examination standard

Examinations may be computer or paper based, or a combination of both. Refer to point 147.A.135.

AMC to Section 5 of Appendix III to Part-66 ‘Aircraft Type Training and Examination Standard. On-the-Job Training’

ED Decision 2015/029/R

Type Examination Standard

This Section 5 ‘Type Examination Standard’ does not apply to the examination performed as part of type training. This Section only applies to those cases where type examination is performed as a substitute for type training.

AMC1 Appendix III Aircraft type training and type evaluation standard — on-the-job training (OJT) Section 6

ED Decision 2023/019/R

On-the-job training (OJT)

General

‘Maintenance organisations appropriately approved according to this Regulation for the maintenance of that aircraft type’ means Part-145 or Part-CAO approved maintenance organisations (AMO) that hold an ‘A’ rating for such aircraft.

The OJT may be split in several parts and carried out at different AMOs, also combining line and base facilities from the same or different organisations. The organisation at which the final assessment is carried out, should control and coordinate the OJT activities and have the responsibility for the entire OJT programme.

The procedures for the OJT should be included in the Exposition Manual of the approved maintenance organisation.

‘Skills and responsibilities of a typical certifying staff’ include but are not limited to:

                understanding the importance of professional integrity, behaviour and having an appropriate attitude towards safety;

                understanding the conditions for ensuring the continuing airworthiness of aircraft and components;

                the ability to identify and rectify existing and potential unsafe conditions;

                the ability to prioritise tasks, coordinate with a team, and report discrepancies;

                the ability to determine the required qualifications for the performance of maintenance tasks;

                the ability to confirm the proper accomplishment of maintenance tasks;

                the ability to compile and control completed work cards;

                knowledge of safety risks linked to a particular working environment;

                understanding of human performance and limitations;

                understanding of the AMO’s (where the OJT is performed) privileges and limitations;

                understanding of the AMO’s personnel authorisations and limitations;

                being familiar with the AMO’s documents/forms (work packages, work orders, work cards, etc.);

                being familiar with AMO’s release-to-service procedures: use of the aircraft technical logbook (ATLB), deferral of items and dispatch under MEL/CDL;

                access, use and control of the required tools and equipment;

                access, use and control of the required ICAs (AMM, TSM, SRM, etc.).

OJT content and OJT logbook

If the aircraft manufacturer has defined the OJT tasks during the type certification of a particular aircraft type (e.g. the operational suitability data (OSD) has been approved for a particular aircraft type), those tasks should be selected. In particular, the analysis performed for the maintenance areas of specific emphasis (MASE), as defined in point 430 of CS-MCSD, helps the organisation identify the more appropriate tasks.

Where no such data exists, the task list in Appendix II to the AMC to Annex III (Part-66) serves as the basis to develop an OJT programme including the applicable tasks for a particular aircraft type, based typically on the AMM. The tasks may be selected from the table in Appendix II in order to cover a broader representative sample of both simple and complex tasks on the particular aircraft type in order to reach a balanced distribution of the tasks between line and base maintenance. The tasks should be selected among those that are applicable to the aircraft type and the licence (sub)category applied for; for example, the selection could exclude location tasks (LOC) and tasks that can be considered under the category A licence privileges (seat covers, boilers, wheels, etc.).

A minimum number of tasks, as described in point 2 ‘List of tasks for OJT’ of Appendix II, of each of the following categories should be performed: INS/inspections, FOT/functional or operational, SGH/servicing, R/I removal and installation, MEL, and T/S troubleshooting. The licensing authority may accept that a limited number of tasks is not performed as long as the relevant cross section of the tasks as regards quality, quantity and complexity is still assured.

A task may be performed on the analogous system installed on a different aircraft type when the systems are similar in terms of design architecture, technology, and functionality. This can be the case, for example, for tasks performed on engines or landing gear of aircraft of the same manufacturer. Such task should be clearly identified and recorded.

Certain maintenance tasks could be performed on non-airworthy aircraft that still maintain functionality of systems to the extent that the maintenance tasks can be completely performed without any deviation from the maintenance instructions. Tasks circumscribed to system components may be performed at the workshop. This can be the case, for example, for avionics functional tests. Such scenarios should be limited to specific tasks that may not occur often in the maintenance of operational aircraft.

The use of MSTDs and MTDs for OJT should be restricted to a minimum.

When an existing licence is changed to include an additional category with a type rating, a different OJT from the category held to the new one may be permissible. In those cases, only tasks corresponding to the differences between the two categories should be performed.

The OJT may be partly performed on aircraft whose maintenance is not subject to Regulation (EU) 2018/1139 (for example, aircraft subject to the FAA regulatory framework or training helicopters used by the military) provided that the maintenance is subject to the same procedures and manuals.

A minimum of maintenance activity on aircraft that are subject to Regulation (EU) 2018/1139 is, however, required in order to gain sufficient insight into the European civil aviation regulatory framework and into release-to-service procedures. The acceptance of the OJT is up to the licensing authority.

The organisation that has control over the OJT should provide candidates with a schedule or plan which indicates the list of tasks to be performed under supervision. A record of the completed tasks is to be entered into a logbook whose design and format should be such that each task or group of tasks is countersigned by the corresponding mentor(s).

Regarding day-to-day supervision of the OJT programme in the approved maintenance organisation and the role of the mentor(s), the following should be considered:

               It is sufficient for the completion of the individual OJT tasks to be confirmed by the direct mentor(s), without the direct evaluation of the assessor being necessary.

               During the day-to-day OJT performance, the aim of the supervision is for mentors to oversee the whole process, including task completion, use of manuals, adherence to procedures, observance of safety measures, warnings, cautions and recommendations, and demonstration of appropriate behaviour in the maintenance environment.

               The mentor(s) should personally observe the work being performed to ensure its safe completion, and should be readily available for consultation if needed during the OJT.

               The mentor(s) should sign the tasks and release the maintenance tasks as the candidate is still not qualified to do so.

               The mentor(s) should be designated by the approved maintenance organisation to supervise.

For training in release-to-service procedures, following the completion of the performance of a specific task chosen by the mentor, the candidate should prepare a document with simulated release to service which has to be marked as ‘for training purposes only’ (e.g. ATL page, maintenance task card, CRS). If both the task and the simulated release to service have been performed to the satisfaction of the mentor, the task may be countersigned in the OJT task list by the mentor. A physical or electronic copy of the document with simulated release should be added to the syllabus.

Tasks which are usually performed with more than one person may be performed by more than one candidate under the supervision of one mentor. During the performance of the tasks, the mentor is limited to overseeing three candidates at the same time, given that the candidates can be properly seen ‘at a glance’ from the mentor’s position. Those tasks should be marked as ‘group tasks’ when applying for the approval. All other tasks should be a one-to-one mentorship. In such cases, all the candidates involved should be noted on the work order.

At the end of the performance of the OJT, a compliance report shall be made which verifies and documents the correct and complete performance and the recommendation of the mentor(s) for the following assessment. The mentor(s) may deny a recommendation if the candidate has not demonstrated the knowledge, skills, behaviour and/or ethics required from certifying staff.

Final assessment of the applicant

The OJT assessment should consist of a theoretical part and a practical part.

The theoretical part comprises the regulatory framework, safety procedures, knowledge of aircraft and its systems, maintenance procedures, and other typical certifying staff activities such as:

               the review and acceptance of work orders;

               shift-handover procedures and team coordination;

               communication and interaction with the flight crew;

               dispatch with unserviceable items;

               clear aircraft logbook entries and reporting notes;

               checks before release to service.

The practical part should include maintenance tasks on the aircraft (e.g. rem./inst., TS, R/I, FOT, MEL dispatch). The assessor may decide to simulate some aspects of the maintenance tasks.

The aircraft type on which the OJT is performed needs to be available for the assessment together with access to the required maintenance data, equipment, and tools. A training aircraft may be acceptable. It is good practice to assess the practical skills on the aircraft in question while the assessment of knowledge may be performed either on the aircraft or in theory.

Further guidance about the designated assessors is provided in the AMC to Appendix III to Part-66.

If an independent observer is required for the OJT, they shall be selected by the maintenance organisation among the maintenance personnel that have not taken part in the OJT performance but do have an adequate understanding of the OJT procedures.

Appendix IV Experience and basic knowledge modules or partial modules required for extending an aircraft maintenance licence under Annex III (Part-66)

Regulation (EU) 2023/989

A. Experience requirements

Table A below shows the experience requirements, in months, for adding a new category or subcategory to a licence granted in accordance with Annex III (Part-66).

The experience requirements can be reduced by 50 % if the applicant has completed an approved Part147 basic training course relevant to a particular subcategory.

Table A

To: From:

A1

A2

A3

A4

B1.1

B1.2

B1.3

B1.4

B2

B2L

B3

L1

L2

L3

L4

L5

A1

6

6

6

24

6

24

12

24

12

6

12

12

12

12

24

A2

6

6

6

24

6

24

12

24

12

6

12

12

12

12

24

A3

6

6

6

24

12

24

6

24

12

12

12

12

12

12

24

A4

6

6

6

24

12

24

6

24

12

12

12

12

12

12

24

B1.1

6

6

6

6

6

6

12

12

6

6

6

12

12

12

B1.2

6

6

6

24

24

6

24

12

12

12

12

B1.3

6

6

6

6

6

6

12

12

6

6

6

12

12

12

B1.4

6

6

6

24

6

24

24

12

6

6

6

12

12

12

B2

6

6

6

6

12

12

12

12

12

6

6

12

12

24

B2L

6

6

6

6

12

12

12

12

12

12

6

6

12

12

24

B3

6

6

6

24

6

24

12

24

12

12

12

12

L1

24

24

24

24

36

24

36

24

36

24

24

6 *36

12 *

12 *

24 *

L2

24

12

24

24

36

12

36

24

36

24

12

12 *

12 *

24 *

L3

30

30

30

30

48

30

48

30

48

30

30

12 *

12 *

6 *

24 *

L4

30

30

30

30

48

30

48

30

48

30

30

12 *

12 *

24 *

L5

24

24

24

24

36

24

36

24

36

24

24

12 *

12 *

12 *

B. Basic knowledge modules or partial modules required

The purpose of this table is to outline the examinations required to add a new basic category/subcategory to an AML granted in accordance with this Annex.

The syllabi prepared in accordance with Appendix I and Appendix VII require different levels of knowledge for different licence categories within a module; therefore, there are additional examinations applicable to certain modules for licence holders wishing to extend an AML granted in accordance with this Annex to include another category/subcategory and an analysis of the module shall be conducted to determine the subjects missing or passed at a lower level.

Table B

To From

A1

A2

A3

A4

B1.1

B1.2

B1.3

B1.4

B2

B2L

B3

L1C

L1

L2C

L2

L3H

L3G

L4H

L4G

L5

A1

None

16.

12.

12, 16.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 2, 8, 9.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 9.

A2

11, 15.

None

12, 15.

12.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 2, 8, 9.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 9.

A3

11, 17.

11, 16,

17.

None

16.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 2, 8, 9.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 9.

A4

11, 15,

17.

11, 17.

15.

None

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 9.

All except 2, 8, 9.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 2L.

All except 9.

B1.1

None

16.

12.

12, 16.

None

16.

12.

12, 16.

4, 5,

13,14

4, 5,

13SQ,

14SQ

16.

12L.

12L.

8L**,

12L.

8L**,

12L.

9L.

10L.

9L,

11L.

10L,

11L.

8L**,

10L,11, 12L.

B1.2

11,15.

None

12, 15.

12.

11, 15.

None

12, 15.

12.

4, 5,

13, 14

4, 5,

13SQ.

14SQ

None

12L.

12L.

8L*,

12L.

8L*,

12L.

9L.

10L.

9L,

11L.

10L,

11L.

8L*,

10L,11,12L.

B1.3

11, 17.

11, 16,

17.

None

16.

11, 17.

11, 16,

17.

None

16.

4, 5, 13, 14

4, 5,

13SQ.

14SQ

11, 16,

17.

7L,12L.

7L,12L.

7L,

8L**,

12L.

7L,

8L**,

12L.

9L.

10L.

9L,

11L.

10L,

11L.

8L**, 10L,11, 12L.

B1.4

11, 15,

17.

11, 17.

15.

None

11, 15,

17.

11, 17.

15.

None

4, 5, 13, 14

4, 5,

13SQ.

14SQ

11, 17.

7L,12L.

7L,12L.

7L,8L*, 12L.

7L,8L*, 12L.

9L.

10L.

9L,11L.

10L,

11L.

8L*, 10L,

11, 12L.

B2

6, 7,

11, 15,

17.

6, 7,

11, 16,

17.

6, 7,

12, 15.

6, 7,

12, 16.

6, 7,

11, 15,

17.

6, 7, 11,

16, 17.

6, 7, 12,

15.

6, 7, 12,

16.

None

None

6, 7, 11,

16, 17.

5L, 7L.

4L, 5L,

6L,7L.

5L,7L,

8L.

4L,5L,

6L,7L,

8L.

9L.

10L.

9L,

11L.

10L,

11L.

6, 7, 11 or 12, 15 or 16, 17, 8L, 10L

B2L

6, 7,

11, 15,

17.

6, 7,

11, 16,

17.

6, 7,

12, 15.

6, 7,

12, 16.

6, 7,

11, 15,

17.

6, 7, 11, 16, 17.

6, 7, 12, 15.

6, 7, 12, 16.

13SQ,

14SQ.

None

6, 7, 11, 16, 17.

5L, 7L,

12LSQ.

4L, 5L,

6L, 7L,

12LSQ.

5L, 7L,

8L,

12LSQ.

4L, 5L,

6L, 7L,

8L,

12LSQ.

9L.

10L.

9L,

11L.

10L,

11L.

6, 7, 11 or

12, 15 or 16, 17, 8L, 10L

B3

11, 15.

11

12,

15.

12.

2,3,5,

8, 11, 15.

2,3,5,8, 11.

2,3,5,8, 12, 15.

2,3,5,8, 12.

2,3,4,

5, 8, 13,

14.

2,3,4,

5, 8,

13SQ.

None

12L.

12L.

8L*,

12L.

8L*,

12L.

9L.

10L.

9L,

11L.

10L,

11L.

2,3,5,8, 11 or 12, 8L*, 10L, 11L, 12L.

To From

A1

A2

A3

A4

B1.1

B1.2

B1.3

B1.4

B2

B2L

B3

L1C

L1

L2C

L2

L3H

L3G

L4H

L4G

L1C

All

All

All

All

All

All

All

All

All

All

All

None

4L, 6L.

8L.

4L, 6L,

8L.

9L.

10L.

8L,9L,

11L.

8L, 10L,

11L.

L1

All

All

All

All

All

All

All

All

All

All

All

None

None

8L.

8L.

9L.

10L.

8L,9L,

11L.

8L,10L,

11L.

L2C

All

All

All

All

All

All

All

All

All

All

All

None

4L,6L.

None

4L, 6L.

9L.

10L.

9L,11L.

10L, 11L.

L2

All

All

All

All

All

All

All

All

All

All

All

None

None

None

None

9L.

10L.

9L,11L.

10L, 11L.

L3H

All

All

All

All

All

All

All

All

All

All

All

5L,7L.

4L,5L,

6L,7L.

5L,7L,

8L.

4L,5L,

6L,7L,

8L.

None

10L.

8L,11L.

8L,10L,

11L.

L3G

All

All

All

All

All

All

All

All

All

All

All

5L,7L.

4L,5L,

6L,7L.

5L,7L,

8L.

4L,5L,

6L,7L,

8L.

9L.

None

8L,9L,

11L.

8L,11L.

L4H

All

All

All

All

All

All

All

All

All

All

All

5L,7L.

4L,5L,

6L,7L.

5L,7L.

4L,5L,

6L,7L.

None

10L.

None

10L.

L4G

All

All

All

All

All

All

All

All

All

All

All

5L,7L.

4L,5L,

6L,7L.

5L,7L.

4L,5L,

6L,7L.

9L.

None

9L.

None

SQ = it depends on system qualification

*:  excluding the subjects related to piston engines

**: excluding the subjects related to turbine engines;

Appendix V — Application Form — EASA Form 19

Regulation (EU) 2021/700

1. This Appendix contains an example of the form used for applying for the aircraft maintenance licence referred to in Annex III (Part-66).

2. The competent authority of the Member State may modify the EASA Form 19 only to include additional information necessary to support the case where the national requirements permit or require the aircraft maintenance licence issued in accordance with Annex III (Part-66) to be used outside the requirements of this Regulation.

APPLICATION FOR INITIAL/AMENDMENT/RENEWAL OF PART-66 AIRCRAFT MAINTENANCE LICENCE (AML)

EASA FORM 19

APPLICANT’S DETAILS:

Name: ………………………………………………………………………………………………………………………………………………………

Address: ……………………………………………………………………………………………………………………………………………………

Tel: ……………………………………………………………………….. E-mail: …………………………………………………………………….

Nationality: …………………………………………………………... Date and Place of Birth: ………………………………………….

PART-66 AML DETAILS (if applicable):

Licence No: …………………………………………………………………. Date of Issue: …………………………………………………….

EMPLOYER’S DETAILS:

Name: ………………………………………………………………………………………………………………………………………………………

Address: ……………………………………………………………………………………………………………………………………………………

………………………………………………………………………………………………………………………………………………………………….

Maintenance Organisation Approval Reference: ………………………………………………………………………………………

Tel: …………………………………………………………………………….. Fax: ……………………………………………………………………

APPLICATION FOR: (Tick relevant boxes)

Initial AML 

Amendment of AML 

Renewal of AML  

(Sub)categories

Aeroplane Turbine

Aeroplane Piston

Helicopter Turbine

Helicopter Piston

A

B1

B2

 

 

 

 

B2L

 

 

 

 

B3

 

 

 

 

C

 

 

 

 

L (see below)

Avionics

 

 

See system ratings below

 

Piston engine non-pressurised aeroplanes of MTOM of 2t and below

 

 

Complex motor-powered aircraft

 

 

 

Aircraft other than complex motor-powered aircraft

 

 

 

System ratings for B2L licence:

1.  autoflight

2.  instruments

3.  com/nav

4.  surveillance

5.  airframe systems

 

 

 

 

L-licence subcategories:

L1C: Composite sailplanes

L1: Sailplanes

L2C: Composite powered sailplanes and composite ELA1 aeroplanes

L2: Powered sailplanes and ELA1 aeroplanes

L3H: Hot-air balloons

L3G: Gas balloons

L4H: Gas balloons

L4H: Hot-air airships

L4G: ELA2 gas airships

L5: Gas airship other than ELA2

 

 

Type endorsements/Rating endorsement/Limitation removal (if applicable): …………………………………………………………………………………………………………………………………………………………………….

 

I wish to apply for initial/amendment of/renewal of Part-66 AML, as indicated, and confirm that the information contained in this form was correct at the time of application.

I herewith confirm that:

1. I am not holding any Part-66 AML issued in another Member State;

2. I have not applied for any Part-66 AML in another Member State; and

3. I never had a Part-66 AML issued in another Member State which was revoked or suspended in any other Member State.

I also understand that any incorrect information could disqualify me from holding a Part-66 AML.

Signed: …………………………………………………………………. Name: ……………………………………………………………………….

Date: ………………………………………………………………………………………………………………………………………………………….

I wish to claim the following credits (if applicable):

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

Experience credits for Part-147 training

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

Examination credits for equivalent exam certificates 

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

…………………………………………………………………………………………………………………………………………………………………….

Please enclose all relevant certificates

Recommendation (if applicable): It is hereby certified that the applicant has met the relevant Part-66 maintenance knowledge and experience requirements and it is recommended that the competent authority grants or endorses the Part-66 AML.

 

Signed: ..............................................................  Name: ..................................................................................

Position: ...........................................................   Date: ....................................................................................

EASA Form 19 Issue 5

Appendix VI — Aircraft Maintenance Licence referred to in Annex III (Part-66) — EASA Form 26

Regulation (EU) 2023/989

1. An example of the aircraft maintenance licence referred to in Annex III (Part-66) can be found on the following pages.

2. The document shall be printed in the standardised form shown but may be reduced in size to allow it being generated by computer. When the size is reduced, care shall be taken to ensure that sufficient space is available in those places where official seals or stamps are required. Computer-generated documents need not have all the boxes incorporated when any such box remains blank, so long as the document can clearly be recognised as an aircraft maintenance licence issued in accordance with Annex III (Part-66).

3. The document may be filled in either in English or the official language of the Member State of the competent authority. In the latter case, a second copy in English shall be attached to the document for any licence holder who needs to use the licence outside that Member State to ensure understanding for the purpose of mutual recognition.

4. Each licence holder shall have a unique licence holder number, established on the basis of a national identifier and an alpha-numeric designator.

5. The document may have the pages in a different order to the one of this example and needs not have some or any divider lines as long as the information contained is positioned in such a manner that each page lay-out can clearly be identified with the format of the example of the aircraft maintenance licence contained herein.

6. The document shall be prepared by the competent authority. However, it may also be prepared by any maintenance organisation approved in accordance with Annex II (Part-145), where the competent authority agrees to this and the preparation takes place in accordance with a procedure laid down in the maintenance organisation exposition referred to in point 145.A.70 of Annex II (Part-145). In all cases, the competent authority shall issue the document.

7. The preparation of any change to an existing aircraft maintenance licence shall be carried out by the competent authority. However, it may also be prepared by any maintenance organisation approved in accordance with Annex II (Part-145), where the competent authority agrees to this and the preparation takes place in accordance with a procedure laid down in the maintenance organisation exposition referred to in point 145.A.70 of Annex II (Part-145). In all cases, the competent authority shall change the document.

8. The holder of the aircraft maintenance licence shall keep it in good condition and shall ensure that no unauthorised entries are made. Failure to comply with this rule may invalidate the license or lead to the holder not being permitted to hold any certification privilege. It may also result in prosecution under national law.

9. The aircraft maintenance licence issued in accordance with Annex III (Part-66) shall be recognised in all Member States and it is not required to exchange the document when working in another Member State.

10. The Annex to EASA Form 26 is optional and may only be used to include national privileges, where such privileges are covered by national law outside the scope of Annex III (Part-66).

11. With regard to the aircraft type rating page of the aircraft maintenance licence, the competent authority may decide not to issue this page until the first aircraft type rating needs to be endorsed and may need to issue more than one aircraft type rating page depending on the number of type ratings to be listed.

12. Notwithstanding point 11, each page issued shall be in the format of this example and contain the specified information for that page.

13. The aircraft maintenance licence shall clearly indicate that the limitations are exclusions from the certification privileges. If there are no limitations applicable, the LIMITATIONS page shall state ‘No limitations’.

14. Where a pre-printer format is used for issuing the aircraft maintenance licence, any category, subcategory or type rating box which does not contain a rating entry shall be marked to show that the rating is not held.

 

I.

EUROPEAN UNION (*)

[STATE]

[AUTHORITY NAME & LOGO]

 

II.

Part-66

AIRCRAFT MAINTENANCE

LICENCE

 

III.

Licence No. [MEMBER STATE

CODE].66.[XXXX]

 

 

IVa. Full name of holder:

IVb. Date and place of birth:

V. Address of holder:

VI. Nationality of holder:

VII. Signature of holder:

 

 

EASA FORM 26 Issue 6

 

III. Licence No:

 

VIII. CONDITIONS:

 

This licence shall be signed by the holder and be accompanied by an identity document containing a photograph of the licence holder.

Endorsement of any categories on the page(s) entitled 'Part-66 CATEGORIES' only, does not permit the holder to issue a certificate of release to service for an aircraft.

This licence, when endorsed with an aircraft rating, meets the intent of ICAO Annex 1.

The privileges of this licence holder are prescribed by Regulation (EU) No 1321/2014 and, in particular, Annex III (Part-66) thereto.

This licence remains valid until the date specified on the limitation page unless previously suspended or revoked.

The privileges of this licence may not be exercised unless in the preceding two-year period, the holder had either six months of maintenance experience in accordance with the privileges granted by the licence, or met the provisions for the issue of the appropriate privileges.

 

IX. Part-66 CATEGORIES

 

VALIDITY

A

B1

B2

B2L

B3

L

C

 

Aeroplanes Turbine

 

 

    n/a

n/a

n/a

n/a

 

Aeroplanes Piston

 

 

    n/a

n/a

n/a

n/a

 

Helicopters Turbine

 

 

    n/a

n/a

n/a

n/a

 

Helicopters Piston

 

 

    n/a

n/a

n/a

n/a

 

Avionics

n/a

n/a

 

 

n/a

n/a

n/a

 

Complex motor-powered aircraft

n/a

n/a

    n/a

n/a

n/a

 

 

Aircraft other than complex motor-powered aircraft

n/a

n/a

    n/a

n/a

n/a

 

 

Sailplanes, powered sailplanes, ELA1 aeroplanes, balloons and airships

n/a

n/a

    n/a

n/a

 

n/a

 

Piston engine non pressurised aeroplanes of 2 000 kg MTOM and below

n/a

n/a

    n/a

 

n/a

n/a

 

 

X. Signature of issuing officer & date:

 

XI. Seal or stamp of issuing authority:

III. Licence No:

 

III. Licence No:

XII. PART-66 RATINGS

 

 

XIII. PART-66 LIMITATIONS

Aircraft Rating/ System ratings

Category/Subcategory

Stamp & Date

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Licence valid until:

III. Licence No:

 

III. Licence No:

Annex to EASA FORM 26

XIV. NATIONAL PRIVILEGES outside the scope of Part-66, in accordance with [National Legislation] (Valid only in [Member State])

 

 

 

 

 

 

 

 

 

 

 

 

 

INTENTIONALLY LEFT BLANK

 

 

Official Stamp & Date

 

III. Licence No:

EASA Form 26 Issue 5

Appendix VII — Basic knowledge requirements for category L aircraft maintenance licence

Regulation (EU) 2023/989

The definitions of the different levels of knowledge required in this Appendix are the same as those set out in point 1 of Appendix I.

1. Modularisation

The modules required for each aircraft licence subcategory/category shall be in accordance with the following matrix. Where applicable, the subject modules are indicated by an ‘X’, while ‘n/a’ means that the subject module is not applicable nor required.

The basic knowledge requirement for L5 shall be the same as for any B1 subcategory (as indicated in Appendix I) plus other modules as shown in the matrix.

 

Licence subcategories

 

Composite sailplanes

Sailplanes

Composite powered sailplanes and composite ELA1 aeroplanes

Powered sailplanes and ELA1 aeroplanes

Hot-air balloons

 

Gas balloons

Hot-air airships

ELA2 gas airships

Gas airships above ELA2

Subject modules

L1C

L1

L2C

L2

L3H

L3G

L4H

L4G

L5

1L ‘Basic knowledge’

X

X

X

X

X

X

X

X

n/a

2L ‘Human factors’

X

X

X

X

X

X

X

X

n/a

3L ‘Aviation legislation’

X

X

X

X

X

X

X

X

n/a

4L ‘Wooden and/or metal-tube structure covered with fabric’

n/a

X

n/a

X

n/a

n/a

n/a

n/a

n/a

5L ‘Composite structure’

X

X

X

X

n/a

n/a

n/a

n/a

n/a

6L ‘Metallic structure’

n/a

X

n/a

X

n/a

n/a

n/a

n/a

n/a

7L ‘Airframe – general, mechanical and electrical systems’

X

X

X

X

n/a

n/a

n/a

n/a

n/a

8L ‘Power plant’

n/a

n/a

X

X

n/a

n/a

X

X

X (37Only applicable propulsion subjects of Module 8L are required; these depend on the B1 subcategory the applicant comes from.)

9L ‘Balloons – hot-air balloons’

n/a

n/a

n/a

n/a

X

n/a

X

n/a

n/a

10L ‘Balloons – gas (free/tethered)  balloons’

n/a

n/a

n/a

n/a

n/a

X

n/a

X

X

11L ‘Airships – hot-air/gas AIRSHIPS’

n/a

n/a

n/a

n/a

n/a

n/a

X

X

X

12L ‘Radio Com/ELT/Transponder/ Instruments’

X

X

X

X

n/a

n/a

X

X

X

MODULE 1L – BASIC KNOWLEDGE

MODULE 1L – BASIC KNOWLEDGE

Level

1L.1 Mathematics

 Arithmetic

 Algebra

 Geometry

 

1

1L.2 Physics

 Matter

 Mechanics

 Temperature

 

1

1L.3 Electrics

— AC and DC circuits

1

1L.4 Aerodynamics/aerostatics

1

1L.5 Workplace safety and environmental protection

2

MODULE 2L – HUMAN FACTORS

MODULE 2L – HUMAN FACTORS

Level

2L.1 General

1

2L.2 Human performance and limitations

1

2L.3 Social psychology

1

2L.4 Factors that affect performance

1

2L.5 Physical environment

1

2L.6 The ‘Dirty Dozen’ and risk mitigation

2

MODULE 3L – AVIATION LEGISLATION

MODULE 3L – AVIATION LEGISLATION

Level

3L.1 Regulatory framework

1

3L.2 Continuing airworthiness regulations

1

3L.3 Repairs and modifications (Part-ML)

2

3L.4 Maintenance data (Part-ML)

2

3L.5 Licence privileges and how to exercise them properly (Part-66, Part-ML)

2

MODULE 4L – WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

MODULE 4L – WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

Level

4L.1 Airframe wooden/combination of metal tube and fabric

2

4L.2 Materials

2

4L.3 Identifying damages and defects

3

4L.4 Standard repair and maintenance procedures

3

MODULE 5L – COMPOSITE STRUCTURE

MODULE 5L – COMPOSITE STRUCTURE

Level

5L.1 Airframe fibre-reinforced plastic (FRP)

2

5L.2 Materials

2

5L.3 Identifying damages and defects

3

5L.4 Standard repair and maintenance procedures

3

MODULE 6L – METALLIC STRUCTURE

MODULE 6L – METALLIC STRUCTURE

Level

6L.1 Metallic airframe

2

6L.2 Materials

2

6L.3 Identifying damages and defects

3

6L.4 Standard repair and maintenance procedures

3

MODULE 7L – AIRFRAME – GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

MODULE 7L – AIRFRAME – GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

Level

7L.1 Theory of flight – gliders and aeroplanes

1

7L.2 Airframe structure – gliders and aeroplanes

1

7L.3 Air conditioning (ATA 21)

1

7L.4 Electrical power, cables and connectors (ATA 24)

2

7L.5 Equipment and furnishing (ATA 25)

2

7L.6 Fire protection and other safety systems (ATA 26)

2

7L.7 Flight controls (ATA 27)

3

7L.8 Fuel system (ATA 28)

2

7L.9 Hydraulic power (ATA 29)

2

7L.10 Ice and rain protection (ATA 30)

1

7L.11 Landing gear (ATA 32)

2

7L.12 Lights (ATA 33)

2

7L.13 Oxygen (ATA 35)

2

7L.14 Pneumatic/vacuum (ATA 36)

2

7L.15 Water ballast (ATA 41)

2

7L.16 Fasteners

2

7L.17 Pipes, hoses and connectors

2

7L.18 Springs

2

7L.19 Bearings

2

7L.20 Transmissions

2

7L.21 Control cables

2

7L.22 Fits and clearances

2

7L.23 Aircraft weight and balance

2

7L.24 Workshop practices and tools

2

7L.25 Disassembly, inspection, repair and assembly techniques

2

7L.26 Abnormal events

2

7L.27 Maintenance procedures

2

MODULE 8L – POWER PLANT

MODULE 8L – POWER PLANT

Piston

Turbine

Electrical

Level

8L.1 General engine fundamentals

X

X

X

2

8L.2 Piston engine fundamentals and performance

X

 

 

2

8L.3 Piston engine construction

X

 

 

2

8L.4 Piston engine fuel system (non-electronic)

X

 

 

2

8L.5 Starting and ignition system

X

 

 

2

8L.6 Air intake, exhaust and cooling system

X

 

 

2

8L.7 Supercharging/turbocharging

X

 

 

2

8L.8 Lubrication systems of piston engines

X

 

 

2

8L.9 Engine indication systems

X

X

X

2

8L.10 Electric aircraft engines

 

 

X

2

8L.11 Turbine engine fundamentals and performance

 

X

 

2

8L.12 Inlet and compressor

 

X

 

2

8L.13 Combustion chamber, starting and ignition system

 

X

 

2

8L.14 Turbine section and exhaust

 

X

 

2

8L.15 Other turbine engine components and systems

 

X

 

2

8L.16 Turbine engine inspections and ground operation

 

X

 

2

8L.17 Propeller

X

X

X

2

8L.18 Full authority digital engine control (FADEC)

X

X

X

2

8L.19 Lubricants and fuels

X

X

X

2

8L.20 Engine and propeller installation

X

X

X

2

8L.21 Engine monitoring and ground operation

X

X

X

2

8L.22 Engine/propeller storage and preservation

X

X

X

2

MODULE 9L – BALLOONS – HOT-AIR BALLOONS

MODULE 9L – BALLOONS – HOT-AIR BALLOONS

Level

9L.1  Theory of flight – hot-air balloons

1

9L.2 General airframe of hot-air balloons

2

9L.3 Envelope

3

9L.4 Heater system/burner

3

9L.5 Basket and basket suspension (including alternative devices)

3

9L.6 Instruments

2

9L.7 Equipment

2

9L.8 Hot-air balloon handling and storage

2

9L.9 Disassembly, inspection, repair and assembly techniques

3

MODULES 10L – BALLOONS – GAS (FREE/TETHERED) BALLOONS

MODULES 10L – BALLOONS – GAS (FREE/TETHERED) BALLOONS

Level

10L.1 Theory of flight – gas balloons

1

10L.2 General airframe of gas balloons

2

10L.3 Envelope

3

10L.4 Netting

3

10L.5 Valves, parachutes and other related systems

3

10L.6 Load ring

3

10L.7 Basket (including alternative devices)

3

10L.8 Ropes and lines

3

10L.9 Instruments

2

10L.10 Tethered gas balloon (TGB) systems

3

10L.11 Equipment

2

10L.12 Gas balloon handling and storage

2

10L.13 Disassembly, inspection, repair and assembly techniques

3

MODULES 11L – AIRSHIPS – HOT-AIR/GAS AIRSHIPS

MODULES 11L – AIRSHIPS – HOT-AIR/GAS AIRSHIPS

Level

11L.1 Theory of flight and control of airships

2

11L.2 Airship airframe structure – general concepts

2

11L.3 Airship envelope

2

11L.4 Gondola

3

11L.5 Airship flight control (ATA 27/55)

3

11L.6 Electrical power (ATA 24)

3

11L.7 Lights (ATA 33)

2

11L.8 Ice and rain protection

3

11L.9 Fuel systems (ATA 28)

2

11L.10 Engine and propellers in airships

2

11L.11 Airship handling and storage

2

11L.12 Disassembly, inspection, repair and assembly techniques

2

MODULE 12L – RADIO COM/ELT/TRANSPONDER/INSTRUMENTS

MODULE 12L – RADIO COM/ELT/TRANSPONDER/INSTRUMENTS

Level

12L.1 Radio Com/ELT

2

12L.2 Transponder and FLARM

2

12L.3 Instruments

2

12L.4 Avionics general test equipment

1

AMC1 Appendix VII Basic knowledge requirements for category L aircraft maintenance licence

ED Decision 2023/019/R

MODULE 1L — BASIC KNOWLEDGE

MODULE 1L — BASIC KNOWLEDGE

Level

1L.1 Mathematics

Arithmetic:

 Arithmetical terms and signs;

 Methods of multiplication and division;

 Fractions and decimals;

 Factors and multiples;

 Weights, measures, and conversion factors;

 Ratio and proportion;

 Averages and percentages;

 Areas and volumes, squares, cubes.

Algebra:

 Evaluating simple algebraic expressions: addition, subtraction, multiplication, and division;

 Use of brackets;

 Simple algebraic fractions.

Geometry:

 Simple geometrical constructions;

 Graphical representation: nature and uses of graphs.

1

1L.2 Physics

Matter:

 Nature of matter: the chemical elements;

 Chemical compounds;

 States: solid, liquid, gaseous;

 Changes between states.

Mechanics:

 Forces, moments and couples, and representation as vectors;

 Centre of gravity;

 Tension, compression, shear, and torsion;

 Nature and properties of solids, fluids, and gases.

Temperature:

 Thermometers and temperature scales: Celsius, Fahrenheit, and Kelvin;

 Definition.

1

1L.3 Electrics

AC and DC circuits:

 Ohm’s law, Kirchhoff’s voltage, and current laws;

 Significance of the internal resistance of a supply;

 Resistance/resistor;

 Resistor colour code, values and tolerances, preferred values, wattage ratings;

 Resistors in series and in parallel.

1

1L.4 Aerodynamics/aerostatics

International Standard Atmosphere (ISA), application to aerodynamics and aerostatics.

1

1L.5 Workplace safety and environmental protection

                Safe working practices and precautions when working with electricity, gases (especially oxygen), oils, and chemicals;

 Labelling, storage and disposal of hazardous (to workplace safety and environment)  materials;

 Remedial action in the event of a fire or another accident with one or more hazards,  including knowledge of fire-extinguishing agents.

2

MODULE 2L — HUMAN FACTORS

MODULE 2L — HUMAN FACTORS

Level

2L.1 General

 The need to take human factors into account in the maintenance domain;

 Incidents attributable to human factors/human error;

 Murphy’s law.

1

2L.2 Human performance and limitations

Vision, hearing, information processing, attention and perception, memory.

1

2L.3 Social psychology

Responsibility, motivation, peer pressure, teamwork.

1

2L.4 Factors that affect performance

Fitness, physical and mental health, stress, sleep, fatigue, alcohol, medication, drug abuse.

1

2L.5 Physical environment

Working environment (climate, noise, illumination).

1

2L.6  The ‘Dirty Dozen’ and risk-mitigation

The ‘Dirty Dozen’:

 lack of communication

 lack of teamwork

 lack of assertiveness

 complacency

 fatigue

 stress

 lack of knowledge

 lack of resources

 lack of awareness

 distraction

 pressure

 norms.

Risk-mitigation methods.

2

MODULE 3L — AVIATION LEGISLATION

MODULE 3L — AVIATION LEGISLATION

Level

3L.1 Regulatory framework

                Role of the European Commission (EC), the European Union Aviation Safety Agency (EASA) and national aviation authorities (NAAs);

                Scope and limitations of the regulatory framework.

1

3L.2  Continuing airworthiness regulations

 General understanding of the applicable parts of Part-66;

 General understanding of the applicable parts of Part-ML;

 General understanding of the applicable parts of Part-CAO;

 General understanding of Part-M, Part-CAMO and Part-145.

1

3L.3 Repairs and modifications (Part-ML)

 Approval of changes (repairs and modifications);

 Standard changes and standard repairs.

2

3L.4 Maintenance data (Part-ML)

 Airworthiness directives (ADs), safety information bulletins (SIBs);

 Service bulletins (SBs), instructions for Continuing Airworthiness (ICAs) (AMM, IPC, etc.),  aircraft flight manual (AFM), maintenance records, maintenance programmes.

2

3L.5  Licence privileges and how to exercise them properly (Part-66, Part-ML)

Conditions for release to service:

 in a maintenance organisation;

 as independent certifying staff;

 release-to-service procedures.

2

MODULE 4L — WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

MODULE 4L — WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

Level

4L.1 Airframe wooden/combination of metal tube and fabric

 

                General construction principles for wooden structures covered with fabric, metal-tube structures covered with fabric, and combination of wooden and metal-tube structures;

                Wood as a technical material (heartwood, sapwood, grain, etc.);

                Wood defects (types, acceptable/ not acceptable);

                Different woodcuts (tangential cuts, radial cuts, etc.) and their properties (tangential cuts, radial cuts, etc.);

                Metal tubing (mechanical and stress properties of metal tubes);

                Types of welding and welding joints;

                General characteristics of aircraft coverings;

                General characteristics of paint;

 Transmission of loads in and between structures.

2

4L.2 Materials

 

                Types of wood (solid wood, laminated wood, plywood, wood composites), suitable wood materials and their properties (spruce, firs, etc.), wood defects (acceptable / not acceptable), stability, deterioration (temperature, humidity, ageing, etc.);

                Types of covering and technologies (natural and synthetic polymers), deterioration;

                Types of glues, adhesives, paints and other associated materials;

                Types of metal-tubing material (steel, light alloy tubes, etc.);

                Welding seams, fittings, screws and bolts (material and properties);

                Proper storage of those materials;

 Plastics (overview and understanding of their properties).

2

4L.3 Identifying damages and defects

 

                Inspection procedures;

                Damage identification in wooden structures (heavy landing, rot, glue failure, fungi, shrinkage, stress damage, cracks, fatigue, etc.);

                Damage identification in metal-tube structures (hard landing, stress, corrosion, fatigue, dents, cracks, fatigue, etc.);

                Damage identification in welded seams;

                Damage identification in fabric coverings (tears, strains, UV damage, hard landing, etc.).

3

4L.4  Standard repair and maintenance procedures

 

                Repair and conservation of wooden aircraft structures: wing rib, wing spar, bolt and brushing holes, patches (fabric, splayed, surface, plug, scarf);

                Repair and reapplication of fabric on aircraft (fabric, tape, lacing, threads, seams, fabric protection, stitching, knots, fasteners, finishing tape, rings and grommets, dope);

                Repair and corrosion protection/prevention methods for metal-tube aircraft structures (welding, patch plates, reinforcement tubes, sleeves, etc.);

                Repair, removal and application of paint and dope on airframes in wooden / combination of metal tube and fabric (surface preparation, application and finish).

3

MODULE 5L — COMPOSITE STRUCTURE

MODULE 5L — COMPOSITE STRUCTURE

Level

5L.1 Airframe fibre-reinforced plastic (FRP)

 

                General construction principles of airframes in FRP and its properties;

                Characteristics of laminated structures (matrix and fibres);

                Fibre (fibre orientation, strength characteristics, isotropic, anisotropic, filament, strands, tows, yarns, rovings, impreg and prepreg);

                Fabric weave styles (plain weave, twill weave, atlas weave, unidirectional) and non-woven material (stitched and knotted) and their characteristics;

                Matrix (thermosetting, thermoplastic, curing stages);

                Characteristics of sandwich structures and their supporting cores (honeycombs, foams, wooden cores, pseudo-cores);

                General characteristics of accelerators and additives/modifiers;

                Transmission of loads in and between structures.

2

5L.2 Materials

 

                Types of fibres (fibreglass, E-glass, aramid, carbon/graphite, boron, ceramic, lightning protection fibre);

                Types of matrices (different types, properties and application);

                Types of resin filler materials (fumed silica, glass powder, hollow glass, phenolic and plastic microballoons, cotton, flox, colour pigments, fire retardants);

                Types of sandwich structure core materials (honeycombs: aramid paper, kraft paper, thermoplastic, aluminium, fibreglass, carbon; foams: polystyrene, phenolic, polyurethane, polypropylene, PVC, polymethacylimide; balsa wood);

                Behaviour, interaction, and technological aspects of composites made of those materials;

                Storage and handling of those materials.

2

5L.3  Identifying damages and defects

 

                Inspection procedures (visual inspection, tapping, NDT testing, etc.);

                Types of manufacturing defects and damages and their causes (fibre breakage, matrix imperfections, delamination, debonding, improper drilling, environmental degradation, impact damage, fatigue, erosion, corrosion, UV damage, hard landing, stress, etc.).

3

5L.4 Standard repair and maintenance procedures

 

                Repairs of aircraft structures: wing, rib, wing spar, aerofoil, bolt and brushing holes, patches, sandwich core and faceplate repairs, bolted and bonded repairs;

                Proper construction and repair fittings, and load-bearing points for composites and composite sandwich structures;

                Creation and use of repair moulds from the airframe or intact parts (types, procedures, coatings, etc.);

                Proper procedure for the mixing of resins, fibre layering and curing of composites;

                Bonding metals and other materials;

                Composite painting and finish.

3

MODULE 6L — METALLIC STRUCTURE

MODULE 6L — METALLIC STRUCTURE

Level

6L.1 Metallic airframe

 

                General construction principles for metal-structure airframes;

                General knowledge of the properties of metal as a technical material (classification; physical, mechanical and electrical properties; manufacturing properties; chemical properties);

                General knowledge of the properties of pure metals and alloys;

                Metal grain structure of pure metals and alloys and its impact on behaviour (grain boundaries; corrosion; hardening; annealing; differences between forged, machined and cast metals);

                Stresses in structural members (tension, compression, torsion, shearing, bearing, bending);

                Types of corrosion and corrosion protection (electrochemical oxidation, galvanic corrosion, stress-corrosion cracking, corrosion in passivated materials, high-temperature corrosion);

                Types of rivets and fasteners (solid shank rivet, blind rivets, self-plugging rivets (mechanical and friction lock), pull-thru rivets, pin rivets, head styles, taper-lok, rivet nut, lockbolt, high shear fastener, identification, measuring);

                Types of welding and welding joints;

                Transmission of loads in and between structures.

2

6L.2 Materials

 

                Types of iron and steel, and their alloys in aviation (cast, forged, tempering, corrosion, strength properties);

                Types of aluminium and aluminium alloys in aviation in airframes, rivets, and fasteners (strength properties, corrosion);

                Common alloying elements for steel and aluminium (influence on the mechanical and physical properties of the alloy);

                Common paint and surface protection materials;

                Common adhesives for use with metals.

2

6L.3 Identifying damages and defects

 

                Inspection procedures (sheet metal, structure, bonded joints, soldered joints, welded and brazed joints, riveted joints, corrosion);

                Identification and classification of cracks, fatigue, and corrosion in metallic structures.

3

6L.4 Standard repair and maintenance procedures

 

                Metal and sheet metal (marking out and calculation of bend allowance, cutting, drilling, bending and forming, inspection of metal work);

                Welding, brazing, soldering and bonding (soldering methods, welding and brazing methods, bonding methods);

                Riveting (riveted joints, rivet spacing and pitch; tools used for riveting and dimpling; inspection of riveted joints);

                Repairing by patching, insertion, and replacement of parts;

                Corrosion treatment;

                Problems in multiple-material systems.

3

MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

Level

7L.1 Theory of flight — gliders and aeroplanes

 

Aerodynamics and flight controls:

                Airflow around a body;

                Boundary layer, laminar and turbulent flow;

                Thrust, weight, aerodynamic resultant;

                Generation of lift and drag angle of attack, polar curve, stall.

Operation and effect of roll control, pitch control, yaw control and rudder limiters:

                Control using dual-purpose controls;

                High-lift devices, slots, slats, flaps, flaperons;

                Drag-inducing devices, lift dumpers, speed brakes, dive brakes;

                Effects of wing fences, saw tooth leading edges;

                Boundary layer control using vortex generators, stall wedges or leading-edge devices;

 Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels.

1

7L.2 Airframe structure — gliders and aeroplanes

 

                Fuselage: construction (truss type, monocoque, semimonocoque), attach points (wing, tail plane, undercarriage);

                Wings: construction (monospar, multispar, box beam), configurations (cantilever, semicantilever, strut/wire braced), fairing;

                Stabilisers: construction, control surface attachments;

                Flight control surfaces: construction and attachment, balancing (mass and aerodynamics);

                Tow hooks (Schweizer and Tost hook);

                Aircraft assembly, storage, jacking, chocking, securing and associated safety precautions;

                Effects of environmental conditions on aircraft handling and operation.

1

7L.3 Air conditioning (ATA 21)

Heating and ventilation for small aircraft.

1

7L.4 Electrical power, cables, and connectors (ATA 24)

 

                Installation and operation of batteries;

                Power generation / power sources (AC/DC) on small aircraft, voltage regulation, power distribution and circuit protection;

                Cable types, construction and characteristics, high-tension and coaxial cables, testing and installation precautions;

                Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes, pin insertion and removal;

                Crimping (crimping, tools, testing of crimp joints);

                Continuity, insulation and bonding techniques and testing;

                Wiring protection techniques (cable looming and loom support, cable clamps, protective sleeving techniques (including heat shrink wrapping), shielding).

2

7L.5 Equipment and furnishing (ATA 25)

 

                Emergency equipment requirements;

 Seats, harnesses, and belts.

2

7L.6 Fire protection and other safety systems (ATA 26)

 

                Portable fire extinguisher;

 Rescue systems (safety parachute, recovery parachute, launching systems, including safety measures for pyrotechnics).

2

7L.7 Flight controls (ATA 27)

 

 Primary controls: aileron, elevator/stabilator, rudder, dual-purpose controls (stabilator,  ruddervator, flaperons);

 Secondary controls: elevator trim systems, wing flaps, slats and spoilers / dive breaks;

 System operation: manual;

 Gust locks, balancing and rigging of flight controls;

 Simple stall-warning systems.

3

7L.8 Fuel system (ATA 28)

 

                System layout;

                Fuel tanks;

                Supply systems;

                Indications and warnings;

                Refuelling and defuelling.

2

7L.9 Hydraulic power (ATA 29)

 

                System layout;

                Hydraulic fluids;

                Hydraulic reservoirs and accumulators, pressure generation (electric, mechanical), filters, pressure control, power distribution, indication and warning systems.

2

7L.10 Ice and rain protection (ATA 30)

 

                Hydrophobic coatings;

 Pitot probe heating.

1

7L.11 Landing gear (ATA 32)

 

                Construction (tricycle, tailwheel, outrigger wheels, skids), shock absorbing;

                Extension and retraction systems: normal and emergency operation;

                Indications and warnings;

                Wheels, brakes, tyres, and steering;

 Standard repair and maintenance procedures for the landing gear.

2

7L.12 Lights (ATA 33)

 

                External lights: navigation, anticollision, landing, taxiing;

 Internal lights: cockpit.

2

7L.13 Oxygen (ATA 35)

 

                System layout: storage system (containers), delivery system (continuous flow, diluter demand and pressure demand) and masks/nasal cannula;

                System operation, including charging and discharging;

 The ‘PRICE’ check.

2

7L.14 Pneumatic/vacuum (ATA 36)

 

                System layout;

                Sources, pumps, control and distribution;

 Indication and warnings.

2

7L.15 Water ballast (ATA 41)

Water tanks (main tank, fin tank), drain valves, vents.

2

7L.16 Fasteners

 

                Screw threads: nomenclature, forms, dimensions and tolerances, and measuring;

                Bolts, studs and screws: types (specifications, identification, markings, international standards), nuts (self-locking, anchor, standard types), machine screws (aircraft specifications), studs (types and uses, insertion and removal), self-tapping screws, dowels;

                Locking devices: tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quick-release fasteners, keys, circlips, cotter pins;

                Aircraft rivets: types of solid and blind rivets: specifications and identification, heat treatment.

2

7L.17 Pipes, hoses, and connectors

 

                Types and connectors of pipes and hoses for hydraulic, fuel, oil, pneumatic and air;

                Bending, belling/flaring, inspection, testing and installation of pipes and hoses.

2

7L.18 Springs

Types of springs, materials, characteristics, applications, inspection, and testing.

2

7L.19 Bearings

 

                Purpose of bearings, loads, material, construction;

                Types of bearings, their application, testing, cleaning, inspection, lubrication requirements, and common defects in bearings and their causes.

2

7L.20 Transmission

 

                Gear types, their application, gear ratios, reduction and multiplication gear systems, driven and driving gears, idler gears, mesh patterns, inspection of gears, backlash/play;

                Types, application and inspection of belts and pulleys, chains and sprockets;

                Inspection of screw jacks, lever devices, push–pull rod systems.

2

7L.21 Control cables

 

                Types of cables, end fittings, turnbuckles, compensation devices, pulleys, cable system components, Bowden cables and aircraft flexible control systems;

                Swaging of end fittings;

                Inspection and testing of control cables, Bowden cables, and aircraft flexible control systems.

2

7L.22 Fits and clearances

 

Common system of fits, clearances and tolerances, drill sizes for bolt holes, classes of fits, schedule of fits and clearances for aircraft and engines, limits for bow, twist and wear, standard methods for checking shafts, bearings and other parts.

2

7L.23 Aircraft weight and balance

 

Calculation of centre-of-gravity / balance limits: use of relevant documents, preparation of aircraft for weighing, aircraft weighing.

2

7L.24 Workshop practices and tools

 

                Common hand-tool types, power-tool types, precision tool types and equipment, their operation, care, control, calibration, and standards;

                Operation, function and use of electrical general test equipment;

                Proper handling of engineering drawings, diagrams and standards, and comprehension of the information presented thereupon (symbols, schematics and diagrams);

                Use of workshop materials;

                Dimensions, allowances and tolerances, standards of workmanship;

                Lubrication equipment and methods.

2

7L.25 Disassembly, inspection, repair, and assembly techniques

 

                Types of defects and visual inspection techniques; corrosion removal, assessment and reprotection;

                General repair methods, structural repair manual; ageing, fatigue and corrosion control programmes;

                Non-destructive inspection techniques, including penetrant, radiographic, eddy current, ultrasonic and borescope methods;

                Disassembly and reassembly techniques;

                Troubleshooting techniques.

2

7L.26 Abnormal events

Inspection following lightning strike, HIRF penetration, heavy landing, and flight through turbulence.

2

7L.27 Maintenance procedures

Maintenance planning, modification procedures, stores procedures, maintenance inspection / quality control / quality assurance, additional maintenance procedures, control of life-limited components.

2

MODULE 8L — POWER PLANT

MODULE 8L — POWER PLANT

Level

8L.1 Engine fundamentals — general

 

 Potential energy, kinetic energy, Newton’s laws of motion, Brayton cycle;

 The relationship between force, work, power, energy, velocity, and acceleration;

 Mechanical, thermal, and volumetric efficiencies.

2

8L.2 Piston-engine fundamentals and performance

 

 Operating principles: 2-stroke, 4-stroke, Otto, Diesel, and Rotary (Wankel);

 Piston displacement and compression ratio;

 Engine configuration and firing order;

 Power calculation and measurement;

 Factors that affect engine power;

 Mixtures/leaning, pre-ignition.

2

8L.3 Piston-engine construction

 

 Crank case, crank shaft, cam shafts, sumps;

 Accessory gearbox;

 Cylinder and piston assemblies;

 Connecting rods, inlet and exhaust manifolds;

 Valve mechanisms;

 Propeller reduction gearboxes.

2

8L.4 Piston-engine fuel system (non-electronic)

 

 Carburettors (types, construction and principles of operation, icing and heating);

 Fuel injection systems (types, construction, and principles of operation).

2

8L.5 Starting and ignition systems

 

 Starting systems, preheat systems;

 Magneto types, construction, and principles of operation;

 Ignition harnesses, spark plugs;

 Low- and high-tension systems.

2

8L.6 Air-intake, exhaust, and cooling systems

 

 Construction and operation of induction systems, including alternate air systems;

 Exhaust systems, engine cooling systems — air and liquid.

2

8L.7 Supercharging/turbocharging

 

 Principles and purpose of supercharging and its effects on engine parameters;

 Construction and operation of supercharging/turbocharging systems;

 System-associated terminology;

 Control systems;

 System protection.

2

8L.8 Lubrication systems of piston engines

 

System operation/layout and components.

2

8L.9 Engine indication systems

 

                Indication systems specific to general combustion engines (coolant temperature, oil pressure and temperature, exhaust gas temperature, fuel pressure and flow);

                Indication systems specific to piston engines (cylinder head temperature, manifold pressure, engine speed);

                Indication systems specific to turbine engines (exhaust gas temperature, engine thrust indication, engine speed);

                Indication systems specific to electric engines (voltage).

2

8L.10 Electric aircraft engines

 

 Types and construction of electric motors (AC and DC motors, rotor, stator, bearings, windings, commutator, self-commutated, externally commutated, outrunner and inrunner, motor cooling, etc.);

 Power electronics;

 Transformer, transducer, and inverter;

 Engine control systems;

 Power storage systems (common high-density batteries, chemistry batteries, load cycles, degradation, effects of charging and overcharging, thermal runaway);

 Battery management systems (general functions, battery balancing, monitoring);

 Wiring of electric power storage, power electronics, and electric motor;

 High-energy safety procedures.

2

8L.11 Turbine-engine fundamentals and performance

 

 Constructional arrangement and operation of turbojet and turboprop engines;

 Thrust: thrust horsepower, shaft horsepower, specific fuel consumption;

 Engine pressure ratio;

 Pressure, temperature, and velocity of gas flow;

 Engine ratings, static thrust, limitations.

2

8L.12 Inlet and compressor

 

 Compressor inlet;

 Axial and centrifugal compressor types, constructional features, operating principles  and applications;

 Compressor (stator, rotor, blisk, disk, blades, compressor stall and surge);

 Compressor ratio.

2

8L.13 Combustion chamber, starting and ignition system

 

 Constructional features and principles of operation;

 Operation of engine start systems and components;

 Ignition systems and components (exciter, ignition plugs and glow plugs).

2

8L.14 Turbine section and exhaust

 

 Operation and characteristics of different turbine blade types, nozzle guide vanes;

 Gas producer turbine and power turbine, blade-to-disk attachment;

 Causes and effects of turbine blade stress and creep;

 Engine exhaust nozzle and noise reduction.

2

8L.15 Other turbine-engine components and systems

 

 General knowledge of the type features and principles of bearings and seals in turbine  engines;

 System operation, layout and components of lubrication systems in small turbine  engines (separate lubrication, as part of the fuel system);

 System operation, layout and components of air and fuel systems in small turbine  engines;

 Turboprop reduction gears.

2

8L.16 Turbine-engine inspection and ground operation

 

 Standard procedures for starting and ground run-up and interpretation of engine  power output and parameters;

 Inspection of engine and components to criteria, tolerances and data specified by the  engine manufacturer;

 Foreign object damage (FOD).

2

8L.17 Propeller

 

 Propeller fundamentals (blade element theory, blade angles, angle of attack, rotational  speed, propeller slip, aerodynamic/centrifugal/thrust forces, torque, relative airflow,               vibration and resonance);

 Propeller construction (methods of construction and materials used in  wooden/composite/metal propellers, blade station, blade face, blade shank, blade               back/thrust face and hub assembly, fixed pitch, controllable pitch, constant speed               propeller, propeller/spinner installation);

 Propeller pitch control (speed control and mechanical/electrical pitch change methods,  feathering, propeller accumulators, overspeed protection);

 Environmental protection (de-icing and metal tipping);

 Propeller balancing (static and dynamic) and blade tracking;

 Damage assessment, erosion, corrosion, impact damage, delamination and decay;

 Standard treatment and repair methods for propellers.

2

8L.18 Full authority digital engine control (FADEC)

 

 Operation of engine control and fuel-metering systems in piston and turbine engines,  including electronic engine control (FADEC);

 System layout and components.

2

8L.19 Lubricants and fuels

 

 Properties and specifications of standard, alternate and drop-in fuels, fuel additives,  and lubricants.

2

8L.20 Engine and propeller installation

 

 Construction of nacelles;

 Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration  mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting              points and drains;

 Extension and retraction systems, including propeller position control;

 Propeller installation.

2

8L.21 Engine monitoring and ground operation

 

 Procedures for starting and ground run-up;

 Interpretation of engine power output and parameters;

 Inspection of engine and components to criteria, tolerances and data specified by the  engine manufacturer;

 Foreign object damage (FOD).

2

8L.22 Engine/propeller storage and preservation

 

 Preservation and depreservation of the engine, the propeller, and accessories/systems.

2

MODULE 9L — BALLOONS: HOT-AIR BALLOONS

MODULE 9L — BALLOONS: HOT-AIR BALLOONS

Level

9L.1 Theory of flight — hot-air balloons

 

 Aerostatics and controls;

 Principles;

 Effect on envelopes, wind effect, altitude, and temperature effects.

1

9L.2 General airframe of hot-air balloons

 

Components and assembly of a hot-air balloon:

 Identification plate;

 Envelope;

 Heater system / burner;

 Suspension cables;

 Basket;

 Lines and ropes (crown line, actuationline).

2

9L.3 Envelope

 

 Shape and assembly of envelope (poles, equator, panels, gores, special shapes);

 Fabrics, seams, and materials;

 Crown ring;

 Deflation port/parachute and ripping panel;

 Load tapes (horizontal and vertical) and rip stoppers;

 Turning vent;

 Mouth;

 Skirt/scoop;

 Diaphragms/catenaries (special shapes).

3

9L.4 Heater system / burner

 

 System layout (burner, fuel tanks, fuel lines);

 Types of burners (whisper-/cow-burner, main/take-off burner);

 Functionality, materials, use, inspection, and care of:

 fuel tanks (propane cylinders, material, valves, fittings, fuel quantity gauge),

 fuel lines / gas hoses,

 burner (piezo igniter, pilot light and valve, blast valve, heat exchanger / burner coils,  nozzle, etc.).

3

9L.5 Basket and basket suspension (including alternative devices)

 

 Common assembly of and materials for hot-air balloon baskets;

 Rigging points, burner frame, burner support rods, metal frame, basket padding and  leather trim;

 Basket weave, grab handles, cylinder attachment, take-off aid and rope;

 Basket wire and basket wire routing;

 Basket floor, basket frame / load-bearing frame, sliders, rawhide protective covering.

3

9L.6 Instruments

 

Basic operation, maintenance, and testing of:

 altimeter (mechanical and electronic);

 variometer (mechanical and electronic);

 pyrometer / temperature sensors;

 Mode S transponder;

 VHF radio;

 Emergency locator transmitter (ELT) and personal locator beacon (PLB).

2

9L.7 Equipment

 

 Required equipment for free-ballooning operation and its care.

2

9L.8 Hot-air balloon handling and storage

 

 Ground procedures for hot-air balloons, rigging and launch preparation;

 Safe handling of propane;

 Effects of environmental conditions on hot-air balloon handling.

2

9L.9 Disassembly, inspection, repair, and assembly techniques

 

 Types of defects and visual inspection techniques;

 Allowable damage to and tolerance of envelope, basket, lines, ropes, etc.;

 Common test procedures (grab test);

 General repair methods for envelopes, load ring, ropes and lines, basket;

 Inspection methods for envelopes, ropes and lines, basket;

 Ageing, fatigue;

 Disassembly and reassembly techniques;

 Troubleshooting techniques.

3

MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS

MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS

Level

10L.1 Theory of flight — gas balloons

 

Aerostatics and controls:

 Principles;

 Effect on envelopes, wind effect, altitude, and temperature effects.

1

10L.2 General airframe of gas balloons

 

Components and assembly of a gas balloon:

 Identification plate;

 Envelope;

 Valve;

 Netting;

 Load ring (hoop);

 Basket;

 Lines and ropes (drag rope, mooring line, valve line, emergency opening rope, ripping line, neckline).

2

10L.3 Envelope

 

 Shape and assembly of envelope (poles, equator, panels);

 Fabrics, seams, and materials;

 Deflation opening and parachute;

 Load belt;

 Ripping panel;

 Appendix;

 Emergency opening;

 Holding-down patches;

 Ballonets;

 Electrostatic properties.

3

10L.4 Netting

 

 Netting assembly (net ring, net, mesh);

 Mesh dimensions (knots, sizes, angles);

 Materials for netting and accessories;

 Electrostatic properties.

3

10L.5 Valves, parachutes, and other related systems

 

 Construction, operation, maintenance and testing of manoeuvring/helium valves, pressure  relief valves, gas-tight parachutes, and ballonet fans;

 Construction, operation, maintenance and testing of parachute-centring belt and pull- down belts.

3

10L.6 Load ring

 

 Function, material, and common problems (steel pipe, strops, toggles).

3

10L.7 Basket (including alternative devices)

 

Common assembly of and materials for hot-air/gas balloon baskets:

 Metal frame, basket padding and leather trim;

 Basket weave, grab handles, basket strops and toggles, ballast system (bags, support and  sand dumpers);

 Basket wire and basket wire routing;

 Basket floor, basket frame / load-bearing frame, sliders, rawhide protective covering.

3

10L.8 Ropes and lines

 

Functionality, materials, use, inspection, and care of:

 Shroud lines / envelope ropes / bridles;

 Trail rope /drag rope and trail-rope bag;

 Holding ropes;

 Valve line/ valve cord and parachute rope;

 Emergency opening rope;

 Appendix pull-close rope;

 Appendix anchor line;

 Inflation aid.

3

10L.9 Instruments

 

Basic operation, maintenance, and testing of:

 Altimeter (mechanical and electronic);

 Variometer (mechanical and electronic);

 Mode-S transponder;

 VHF radio;

 Emergency locator transmitter (ELT) and personal locator beacon (PLB).

2

10L.10 Tethered gas balloon (TGB) systems

 

Functionality, operation, materials, use, inspection, and care of:

 Launch platform;

 Winch system: winch (electric, hydraulic, emergency operation), tether cable (cable,  sheaves, swivel, clamps), and control panel;

 Gondola (metal-tubing construction);

 Night lighting.

3

10L.11 Equipment

 

 Required equipment for free-ballooning and for tethered operations, and its care.

2

10L.12 Gas-balloon handling and storage

 

 Ground procedures and mooring for gas balloons and tethered gas balloons, ballasting,  rigging and launch preparation;

 Safe handling of hydrogen, helium, illuminating gas, and other lifting gases;

 Lifting gas (charging, purifying and leak testing, pressure monitoring);

 Effects of environmental conditions on gas-balloon handling.

2

10L.13 Disassembly, inspection, repair, and assembly techniques

 

 Types of defects and visual inspection techniques;

 Allowable damage to and tolerance of envelope, basket, lines, ropes, etc.;

 Common test procedures (grab test, tensile strength, tear growth, porosity, electric  resistivity, etc.);

 General repair methods for envelopes, load ring, ropes and lines, basket/gondola;

 Inspection methods for envelopes, load ring, ropes and lines, basket/gondola (especially  for steel frames and welds on TGB gondolas);

 Ageing, fatigue and corrosion control programmes;

 Disassembly and reassembly techniques;

 Troubleshooting techniques.

3

MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS

MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS

Level

11L.1 Theory of flight and control of airships

 

 Control using fins, rudders and elevators;

 Aerodynamic lift and aerodynamic balance;

 Stability and control;

 Free ballooning;

 Operation of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs,  mass balance, control surface bias, aerodynamic balance panels;

 Vectored thrust;

 Fire and lightning protection.

2

11L.2 Airship airframe structure — general concepts

 

 Classification of airships (rigid airship, semi-rigid airship, non-rigid airship);

 Construction of semi-rigid airships (envelope, ballonet, membranes, nose cone, internal  structures, keel, trusses, longerons, suspension lines);

 Construction of non-rigid airships (envelope, ballonet, catenary curtains, suspension lines,  air scoops);

 Attachment of stabilisers and control surfaces to the airframe.

2

11L.3 Airship envelope

 

 Nose cone battens / bow strips;

 Catenary systems (catenary curtain, support/suspension cables);

 Ballonets and their positioning (forward, aft);

 Air systems (air scoops, ballonet fans, empennage air system, dampers and transfer fans).

2

11L.4 Gondola

 

 General knowledge of gondola construction (metal-tubing gondolas, metal-structure  gondolas, composite gondolas);

 Doors, windows, and hatches;

 Attachment of the gondola to the airframe/envelope;

 Gondola layout, equipment and furnishing (emergency equipment requirements, seats,  harnesses and belts);

 Simple water/waste systems in airships;

 Gondola heating and ventilation (ventilations and heating systems, heat exchanger,  blower);

 Landing gear (construction, shock absorbing, tyres, weight-on-wheels).

3

11L.5 Airship flight controls (ATA 27/55)

 

 Primary controls (rudder, elevator, asymmetric thrust, thrust vectoring);

 Trim control;

 System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;

 Balancing and rigging.

3

11L.6 Electrical power (ATA 24)

 

 Installation and operation of batteries;

 DC power generation;

 AC power generation;

 Voltage regulation;

 Power distribution;

 Wiring, electrical connections;

 Inverters, transformers, rectifiers;

 Circuit protection;

 External/ground power.

3

11L.7 Lights (ATA 33)

 

 External: navigation, anticollision, landing, taxiing, ground approach light, aft landing light;

 Internal: flight compartment (cockpit) and passenger compartment (cabin);

 Emergency.

2

11L.8 Ice and rain protection

 

 Windscreen wipers and windscreen de-misting systems;

 Surface de-icing systems.

3

11L.9 Fuel systems (ATA 28)

 

 System layout;

 Fuel tanks: venting, draining;

 Supply systems;

 Cross-feed and transfer;

 Indications and warnings;

 Refuelling and defuelling.

2

11L.10 Engine and propellers in airships

 

 General understanding of engine layout, thrust vectoring, swivel systems, ducted  propellers and control system.

2

11L.11 Airship handling and storage

 

 Ground procedures and mooring with and without mooring mast, ballasting, hangaring,  rigging and launch preparation;

 Lifting gas (charging, purifying and leak testing, pressure monitoring);

 Effects of environmental conditions on airship handling.

2

11L.12 Disassembly, inspection, repair, and assembly techniques

 

 Types of defects and visual inspection techniques;

 Corrosion removal, assessment and reprotection;

 General repair methods, structural repair manual;

 Ageing, fatigue and corrosion control programmes;

 Non-destructive inspection techniques;

 Disassembly and reassembly techniques;

 Troubleshooting techniques.

2

MODULE 12L — RADIO COM / ELTs / TRANSPONDERS / INSTRUMENTS

MODULE 12L — RADIO COM / ELTs / TRANSPONDERS / INSTRUMENTS

Level

12L.1 Radio COM / ELTs

 

Fundamentals of radio-wave propagation, antennas, transmission lines, communication, receiver, and transmitter.

Working principle of:

 Emergency locator transmitters (ELTs);

 Very-high-frequency (VHF) communications;

 installation and testing of ELTs and VHF radio and antennas.

2

12L.2 Transponder and FLARM

 

 Air traffic control transponder, secondary surveillance radar (basic operation,  configuration, modes);

 FLARM;

 Installation and testing.

2

12L.3 Instruments

 

 Pitot-static: altimeter, airspeed indicator, vertical speed indicator, total energy probes;

 Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation  indicator, turn and slip indicator, turn coordinator;

 Compasses: direct reading, remote reading;

 Angle-of-attack indication, stall-warning systems;

 Glass and analogue cockpit;

 Indications of other aircraft systems;

 Installation and testing of instruments.

2

12L.4 Avionics general test equipment

 

 Operation, function, and use of general test equipment for avionics.

1

Appendix VIII — Basic examination standard for category L aircraft maintenance licence

Regulation (EU) 2023/989

(a) The standardisation basis for examinations related to the Appendix VII basic knowledge requirements shall be as follows:

(i) all examinations must be carried out using the multiple-choice question format as specified in point (ii). The incorrect alternatives must seem equally plausible to anyone ignorant of the subject. All of the alternatives should be clearly related to the question and of similar vocabulary, grammatical construction and length. In numerical questions, the incorrect answers should correspond to procedural errors such as corrections applied in the wrong sense or incorrect unit conversions: they must not be mere random numbers;

(ii) each multiple-choice question must have three alternative answers of which only one must be the correct answer and the candidate must be allowed a time per module which is based upon a nominal average of 75 seconds per question;

(iii) the pass mark for each module is 75 %;

(iv) penalty marking (negative points for failed questions) is not to be used;

(v) the level of knowledge required in the questions must be proportionate to the level of technology of the aircraft category.

(vi) a failed module may not be retaken for at least 90 days from the date of the failed module examination;

(vii) the maximum number of attempts for each examination is three in a 12-month period.

(b) The number of questions per module shall be as follows:

(i) module 1L ‘BASIC KNOWLEDGE’: 20 questions.

Time allowed: 25 minutes;

(ii) module 2L ‘HUMAN FACTORS’: 20 questions.

Time allowed: 25 minutes;

(iii) module 3L ‘AVIATION LEGISLATION’: 28 questions.

Time allowed: 35 minutes;

(iv) module 4L ‘WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC’: 40 questions.

Time allowed: 50 minutes;

(v) module 5L ‘COMPOSITE STRUCTURE’: 32 questions.

Time allowed: 40 minutes;

(vi) module 6L ‘METALLIC STRUCTURE’: 32 questions.

Time allowed: 40 minutes;

(vii) module 7L ‘AIRFRAME – GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS’: 60 questions.

Time allowed: 75 minutes;

(viii) module 8L ‘POWER PLANT’: 64 questions.

Time allowed: 80 minutes;

(ix) module 9L ‘BALLOONS – HOT-AIR BALLOONS’: 36 questions.

Time allowed: 45 minutes;

(x) module 10L ‘BALLOONS – GAS (FREE/TETHERED) BALLOONS’: 44 questions.

Time allowed: 55 minutes;

(xi) module 11L ‘AIRSHIPS – HOT-AIR/GAS AIRSHIPS’: 40 questions.

Time allowed: 50 minutes;

(xii) Module 12L ‘RADIO COM/ELT/TRANSPONDER/INSTRUMENTS’: 20 questions.

Time allowed: 25 minutes.

NUMBER OF QUESTIONS PER SUBMODULE

The tables below show the number of questions recommended for each submodule. Justified deviations from these values are also acceptable, provided that the sum of the questions for the submodules equals the total number for a given module.

MODULE 1L — BASIC KNOWLEDGE

MODULE 1L — BASIC KNOWLEDGE

Nr of questions

20

1L.1 Mathematics

4

1L.2 Physics

5

1L.3 Electrics

4

1L.4 Aerodynamics/aerostatics

2

1L.5 Workplace safety and environmental protection

5

MODULE 2L — HUMAN FACTORS

MODULE 2L — HUMAN FACTORS

Nr of questions

20

2L.1 General

3

2L.2 Human performance and limitations

2

2L.3 Social psychology

2

2L.4 Factors that affect performance

4

2L.5 Physical environment

4

2L.6 The ‘Dirty Dozen’ and risk-mitigation

5

MODULE 3L — AVIATION LEGISLATION

MODULE 3L — AVIATION LEGISLATION

Nr of questions

28

3L.1 Regulatory framework

4

3L.2 Continuing airworthiness regulations

6

3L.3 Repairs and modifications (Part-ML)

5

3L.4 Maintenance data (Part-ML)

5

3L.5 Licence privileges and how to exercise them properly (Part-66, Part-ML)

8

MODULE 4L — WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

MODULE 4L — WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

Nr of questions

40

4L.1 Combined structures made of wood, metal tube and fabric

8

4L.2 Materials

8

4L.3 Identifying damages and defects

12

4L.4 Standard repair and maintenance procedures

12

MODULE 5L — COMPOSITE STRUCTURE

MODULE 5L — COMPOSITE STRUCTURE

Nr of questions

32

5L.1 Fibre-reinforced plastic (FRP) airframe

6

5L.2 Materials

6

5L.3 Identifying damages and defects

10

5L.4 Standard repair and maintenance procedures

10

MODULE 6L — METALLIC STRUCTURE

MODULE 6L — METALLIC STRUCTURE

Nr of questions

32

6L.1 Metallic airframe

6

6L.2 Materials

6

6L.3 Identifying damages and defects

10

6L.4 Standard repair and maintenance procedures

10

MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

Nr of questions

60

7L.1 Theory of Flight — gliders and aeroplanes

4

7L.2 Airframe Structure — gliders and aeroplanes

4

7L.3 Air conditioning (ATA 21)

1

7L.4 Electrical power, cables, and connectors (ATA 24)

3

7L.5 Equipment and furnishing (ATA 25)

2

7L.6 Fire protection and other safety systems (ATA 26)

2

7L.7 Flight controls (ATA 27)

3

7L.8 Fuel system (ATA 28)

2

7L.9 Hydraulic power (ATA 29)

2

7L.10 Ice and rain protection (ATA 30)

1

7L.11 Landing gear (ATA 32)

3

7L.12 Lights (ATA 33)

1

7L.13 Oxygen (ATA 35)

1

7L.14 Pneumatic/vacuum (ATA 36)

1

7L.15 Water ballast (ATA 41)

1

7L.16 Fasteners

2

7L.17 Pipes, hoses, and connectors

2

7L.18 Springs

1

7L.19 Bearings

1

7L.20 Transmissions

2

7L.21 Control cables

3

7L.22 Fits and clearances

1

7L.23 Aircraft weight and balance

2

7L.24 Workshop practices and tools

4

7L.25 Disassembly, inspection, repair, and assembly techniques

4

7L.26 Abnormal events

3

7L.27 Maintenance procedures

4

MODULE 8L — POWER PLANT

MODULE 8L — POWER PLANT

Nr of questions

64

8L.1 Engine fundamentals — general

2

8L.2 Piston-engine fundamentals and performance

2

8L.3 Piston-engine construction

3

8L.4 Piston-engine fuel system (non-electronic)

2

8L.5 Starting and ignition systems

3

8L.6 Air intake, exhaust, and cooling systems

2

8L.7 Supercharging/turbocharging

2

8L.8 Lubrication systems of piston engines

2

8L.9 Engine indication systems

3

8L.10 Electric and hybrid aircraft engines

9

8L.11 Turbine-engine fundamentals and performance

2

8L.12 Inlet and compressor

2

8L.13 Combustion chamber, starting and ignition system

2

8L.14 Turbine section and exhaust

2

8L.15 Other turbine-engine components and systems

2

8L.16 Turbine-engine inspections and ground operation

3

8L.17 Propeller

7

8L.18 Full authority digital engine control (FADEC)

2

8L.19 Lubricants and fuels

3

8L.20 Engine and propeller installation

4

8L.21 Engine monitoring and ground operation

3

8L.22 Engine/propeller storage and preservation

2

Note:  In accordance with Appendix VII ‘1. Modularisation’ to Annex III, Module 8L training subjects for L5 category AML and, therefore, the number of questions, should be limited to the relevant propulsion system. As such, in the above table, certain submodules may not be applicable and should not be taken into account, and the total number of questions should also be adapted accordingly.

MODULE 9L — BALLOONS: HOT-AIR BALLOONS

MODULE 9L — BALLOONS: HOT-AIR BALLOONS

Nr of questions

36

9L.1 Theory of flight — hot-air balloons

2

9L.2 Airframe of hot-air balloons

3

9L.3 Envelope

4

9L.4 Heater system / burner

4

9L.5 Basket and basket suspension (including alternative devices)

4

9L.6 Instruments

5

9L.7 Equipment

2

9L.8 Hot-air balloon handling and storage

4

9L.9 Disassembly, inspection, repair, and assembly techniques

8

MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS

MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS

Nr of questions

44

10L.1 Theory of flight of gas balloons

2

10L.2 Airframe of gas balloons

3

10L.3 Envelope

3

10L.4 Netting

1

10L.5 Valves, parachutes, and other related systems

1

10L.6 Load ring

1

10L.7 Basket (including alternative devices)

4

10L.8 Ropes and lines

2

10L.9 Instruments

5

10L.10 Tethered gas balloon (TGB) systems

8

10L.11 Equipment

2

10L.12 Gas-balloon handling and storage

4

10L.13 Disassembly, inspection, repair, and assembly techniques

8

MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS

MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS

Nr of questions

40

11L.1 Theory of flight and control of airships

3

11L.2 Airship airframe structure — general concepts

3

11L.3 Airship envelope

3

11L.4 Gondola

6

11L.5 Airship flight controls (ATA 27/55)

2

11L.6 Electrical power (ATA 24)

3

11L.7 Lights (ATA 33)

1

11L.8 Ice and rain protection

2

11L.9 Fuel systems (ATA 28)

3

11L.10 Engines and propellers in airships

2

11L.11 Airship handling and storage

4

11L.12 Disassembly, inspection, repair, and assembly techniques

8

MODULE 12L — RADIO COM / ELTs / TRANSPONDERS / INSTRUMENTS

MODULE 12L — RADIO COM / ELTs / TRANSPONDER / INSTRUMENTS

Nr of questions

20

12L.1 Radio COM / ELTs

6

12L.2 Transponder and FLARM

5

12L.3 Instruments

8

12L.4 Avionics general test equipment

1

Appendix IX Assessment method for the multimedia-based training (MBT)

Regulation (EU) 2023/989

1. The purpose of this Appendix is to establish the requirements for the assessment and approval by a competent authority of any course that includes MBT in accordance with point 66.B.135.

This Appendix may be used for the assessment of other training courses if the competent authority decides that the assessment method laid down in this Appendix are appropriate for such other courses.

The assessment shall be conducted by the competent authority against all the criteria laid down in Table (A), grouped in four categories from (a) to (d). The competent authority shall clearly identify in the table the MBT product being assessed and its production and update versions.

2. The competent authority carrying out the assessment shall put itself in the position of the student or the end user and shall rate each criterion listed in Table (A) individually on a rating scale from 1 to 5, as follows:

1: Not acceptable. Does not meet the required criteria.

2: Partially acceptable, but improvement is needed to meet the required criteria.

3: Acceptable. Meets the required criteria.

4: Good. Meets the required criteria with enhancements made.

5: Excellent. Exceeds the required criteria.

3. If one or more of the criteria is rated below 3, an alternative learning process shall be requested by the competent authority in order to enhance the suitability of the product to an acceptable level.

4. Once the competent authority has rated each of the individual criteria listed in Table (A) , the following combined rating scale shall be used by the competent authority to determine the overall suitability level for each MBT learning resource:

 100–80: Excellent learning resource. It offers different functionalities and meets the required suitability criteria.

 79–60: The learning resource meets the required suitability criteria.

 59–40: The learning resource does not allow for a sufficiently worthy educational use. It can be used for ‘informal’ training only.

 39–20: The learning resource is below the average. It does not meet several required suitability criteria.

Before approving the product, the competent authority shall check that the final score of the MBT is equal to or above 60, and that there is no single criterion that is rated below 3.

Table (A): Assessment for the multimedia-based training (MBT)

Assessment table for the multimedia-based training (MBT)

Product identification:

Name:

Version:

 

SCORE (1–5)

Category (a) ‘academic quality’

Information reliability

1. The information is reliable.

 

Information relevance

2. The information is relevant.

 

Category (b) ‘pedagogical quality’

Pedagogical formulation/ construction

3. The quality of the resource simplification is adequate.

 

4. The educational resource presents an appropriate number of overviews and summaries.

 

5. The resource is clearly structured (summaries, plans).

 

6. The structure promotes its use in the pedagogical context.

 

Pedagogical strategies

7. The learning objectives are stated.

 

8. The resource includes stimuli to promote learning.

 

9. The resource creates interaction between student and instructor.

 

10. The active engagement of the student is fostered.

 

11. Student-centred learning is present.

 

12. Problem-solving tasks encourage learning.

 

13. The resource enables communication between students.

 

14. The student is able to see their learning progress.

 

Student assessment methods

15. The resource provides a self-assessment procedure.

 

Category (c) ‘didactic quality’

Learning activities

16. The content refers to real-life situations that the student could possibly face in an actual maintenance environment.

 

Learning content

17. The content is adequate to meet the learning objectives.

 

Category (d) ‘technical quality’

Design

18.  The content and organisation of the learning resource includes the appropriate use of colours, interactivity, graphic quality, animations, and illustrations.

 

Browsing

19. Navigation methods are clear, consistent, and intuitive.

 

Technological aspects

20. Multimedia techniques promote the transfer of information.

 

Final score:

 

Notes:

The following shall be taken into account by the competent authority when assessing the MBT against the individual criteria listed in Table (A):

Categories:

(a) Academic quality

The information presented in the multimedia resource shall have two characteristics:

i. Reliability: the information is reliable, current, and relatively free of errors. The information complies with the current regulatory requirements.

ii. Relevance: the information is relevant to the learning objectives defined for the course. It supports the student in achieving the learning objectives.

(b) Pedagogical quality

The MBT emphasises the activities which promote the development of the required knowledge and skills.

The main criteria for each product are related to three aspects:

i. Pedagogical formulation/construction: it is characterised by the quality of simplification, the presence of summaries as well as the use of diagrams, figures, animations, and illustrations. It evaluates whether the structure of the learning resource promotes its use in a pedagogical context. This refers to the ease of orientation (summary, lesson plan), presence of appropriate interactions, usability (back, forward, scroll boxes, etc.), and communication resources (questions and answers, FAQs, forum, etc.)

ii. Pedagogical strategies: teaching and learning styles should be based on active teaching approaches to build meaningful situations related to learning objectives and to learner motivation.

iii. Student assessment methods: methods are implemented to measure the achievement of learning objectives.

(c) Didactic quality

i. Learning activities: the content refers to real-life situations the student could possibly face in an actual maintenance environment.

ii. Learning content: the content is adequate to meet the learning objectives.

(d) Technical quality

This section assesses the design, browsing and technological aspects of the learning resources:

i. Design: the content and organisation of the learning resource shall promote the appropriate use of colours, interactivity, graphic quality for selected images, animations, and illustrations.

ii. Browsing: while navigating, the student should be able to find a plan, an index, or a detailed table of contents. The suggested choices or guidelines shall be clear and the groupings within the menus shall be consistent.

iii. Technological aspects: multimedia techniques aim to combine and exploit the capacities of any new technology in education to enhance the transfer of knowledge. Therefore, the system shall favour the use of animations, simulations, or any other interactive elements.