CHAPTER 7 - CAR 66 AIRCRAFT MAINTENANCE ......An applicant for an aircraft maintenance licence shall...
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CAR 66 Rev 00 C-1 01 July 2011 CAR PART II CHAPTER 7 - CAR 66 AIRCRAFT MAINTENANCE ENGINEER LICENSING FOREWORD CONTENTS – General CONTENTS – Details UNCONTROLLED COPY WHEN DOWNLOADED Check with GCAA Website to verify current version before using
Transcript of CHAPTER 7 - CAR 66 AIRCRAFT MAINTENANCE ......An applicant for an aircraft maintenance licence shall...
CAR 66
Rev 00 C-1 01 July 2011
CAR PART II
CHAPTER 7 - CAR 66
AIRCRAFT MAINTENANCE ENGINEER
LICENSING
FOREWORD
CONTENTS – General
CONTENTS – Details
UNCONTROLLED COPY WHEN DOWNLOADED
Check with GCAA Website to verify current version before using
CAR 66
Rev 00 C-2 01 July 2011
FOREWORD
1. The General Civil Aviation Authority is known in these regulations as the “GCAA”. 2. Development of the requirements of CAR 66 will be in accordance with Notice of Proposed
Rule Making (NPA) procedures. These procedures allow for the amendment of CAR 66 to be harmonized with amendments to EASA and ICAO Annexes in a timely manner
3. Definitions and abbreviations of terms used in CAR 66 that are specific to a Section are
normally given in that section concerned or, exceptionally, in the associated compliance or guidance material.
4. [New amended and corrected text will be enclosed within heavy brackets until a subsequent “amendment” is issued.]
5. Both Regulations and Guidance Material are presented in Calibri font.
6. This is the initial issue dated 1st of July 2011. All pages of this edition of CAR 66 are now current.
7. Conformity with the Acceptable Means of Compliance (AMC) and Guidance Material (GM) presented in Section 2 is mandatory unless other means of compliance meet the equivalent level of safety, acceptable to the GCAA.
CAR 66
Rev 00 i 01 July 2011
LIST OF EFFECTIVE PAGES
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CAR 66
Rev 00 ii 01 July 2011
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CAR 66
Rev 00 iii 01 July 2011
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CAR 66
Rev 00 iv 01 July 2011
RECORD OF AMENDMENTS
Rev. No. Date of Issue Entered By
00 01 July 2011 GCAA Policy, Regulation & Planning Section
CAR 66
Rev 00 v 01 July 2011
AMENDMENTS HISTORY
Amendment Source(s) Subject(s) Effective Date
Rev. 00
1st July 2011
Based on announcement made to the public on 1st July 2010
(IB. No. 15/2010)
New Regulations 1st July 2011
CAR 66
Rev 00 vi 01 July 2011
CONTENTS (General)
CAR 66
AIRCRAFT MAINTENANCE ENGINEER LICENSING
SECTION 1 - REGULATIONS
SECTION 2 - ACCEPTABLE MEANS OF COMPLIANCE
SECTION 3 - GUIDANCE MATERIAL
CAR 66
Rev 00 vii 01 July 2011
TABLE OF CONTENTS
SECTION 1 REGULATIONS
SUBPART A - AIRCRAFT MAINTENANCE LICENCE AEROPLANES AND
HELICOPTERS
CAR 66. 1 Scope .............................................................................................. 1-A-1
CAR 66.10 Application ..................................................................................... 1-A-1
CAR 66.15 Eligibility ........................................................................................ 1-A-1
CAR 66.20 Privileges ....................................................................................... 1-A-1
CAR 66.25 Basic knowledge requirements ..................................................... 1-A-2
CAR 66.30 Experience requirements .............................................................. 1-A-2
CAR 66.40 Continued validity of the aircraft maintenance licence ............... 1-A-4
CAR 66.45 Type/task training and ratings ...................................................... 1-A-4
CAR 66.55 Evidence of qualifications ............................................................. 1-A-6
CAR 66.70 Conversion provisions ................................................................... 1-A-6
SUBPART B - AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS
CAR 66.100 General ........................................................................................... 1-B-1
SUBPART C - COMPONENTS
CAR 66.200 General .......................................................................................... 1-C-1
APPENDICES
Appendix I Basic Knowledge Requirements........................................................ 2-1
Appendix II Basic Examination Standard ........................................................... 2-57
Appendix III Type Training and Examination Standard ....................................... 2-61
Appendix IV Experience Requirements for Extending a CAR 66 Aircraft Maintenance Licence ...................................................................... 2-68
Appendix V Example of licence format .............................................................. 2-70
SECTION 2 ACCEPTABLE MEANS OF COMPLIANCE
AMC 66.10 Application ................................................................................................ 2-73
AMC 66.20(a) Privileges .................................................................................................. 2-73
AMC 66.20(b) 2 Privileges ................................................................................................... 2-74
AMC 66.25 Basic knowledge requirements................................................................. 2-76
AMC 66.30(a) Experience requirements ......................................................................... 2-76
CAR 66
Rev 00 viii 01 July 2011
AMC 66.30(d) Experience requirements ......................................................................... 2-76
AMC 66.30(e) Experience requirements ......................................................................... 2-76
AMC 66.45(a) Type/task training and ratings ................................................................. 2-76
AMC 66.45(d) Type/task training and ratings ................................................................. 2-77
AMC 66.45(e) Type/task training and ratings ................................................................. 2-77
AMC 66.45(g) Type/task training and ratings ................................................................. 2-77
AMC 66.45(h) Type/task training and ratings ................................................................. 2-77
AMC 66.70 Conversion provisions .............................................................................. 2-79
APPENDICES TO AMC
Appendix I Type Rating Designators ........................................................................... 2-80
Appendix II Aircraft Type Practical Experience List of Tasks...................................... 2-110
SECTION 3 GUIDANCE MATERIALS
GM to CAR 66.20(a) Privileges ......................................................................................................3-1
GM to CAR 66.20(a) Privileges .....................................................................................................3-1
GM to CAR 66.20(b)3 Privileges .....................................................................................................3-2
GM to CAR 66.25(a) Basic knowledge requirements ...................................................................3-2
GM to CAR 66.30(a) Basic knowledge requirements ...................................................................3-2
GM to CAR 66.40 Continued validity of the aircraft maintenance licence .............................3-2
GM to CAR 66.45(d) Type/task training and ratings ....................................................................3-2
GM to CAR 66.45(f) Type/task training and ratings ....................................................................3-3
GM to CAR 66.45(d) and (e) Type/task training and ratings ....................................................................3-3
GM to CAR 66.70 Conversion provisions .................................................................................3-3
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-1 01 July 2011
SUBPART A - AIRCRAFT MAINTENANCE LICENCE AEROPLANES AND HELICOPTERS
CAR 66.1 Scope (a) This section establishes the requirements for the issue of an aircraft maintenance licence and conditions of its validity and use, for aeroplanes and helicopters of the following categories: — Category A — Category B1 — Category B2 — Category C Certifying staff shall be qualified in accordance with this CAR, except as provided for in CAR M.607 (b); CAR M.803 and CAR 145.30(j). (b) Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes, helicopters, turbine and piston engines. The subcategories are: — A1 and B1.1 Aeroplanes Turbine — A2 and B1.2 Aeroplanes Piston — A3 and B1.3 Helicopters Turbine — A4 and B1.4 Helicopters Piston CAR 66.10 Applications An application for an aircraft maintenance licence or amendment to such licence shall be made on appropriate LAME form and/or any other assigned form and in a manner established by the General Civil Aviation Authority (GCAA) and submitted thereto. An application for the amendment to an aircraft maintenance licence shall be made to the General Civil Aviation Authority (GCAA). CAR 66.15 Eligibility An applicant for an aircraft maintenance licence shall be at least 18 years of age. CAR 66.20 Privileges (a) Subject to compliance with paragraph (b), the following privileges shall apply:
1. A category A aircraft maintenance licence permits the holder to issue certificates of release to service following minor scheduled line maintenance and simple defect rectification within the limits of tasks specifically endorsed on the authorisation. The certification privileges shall be restricted to work that the licence holder has personally performed in a CAR 145 organisation.
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-2 01 July 2011
2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of release to service following maintenance, including aircraft structure, power plant and mechanical and electrical systems. Replacement of avionic line replaceable units, requiring simple tests to prove their serviceability, shall also be included in the privileges. Category B1 shall automatically include the appropriate A subcategory.
3. A category B2 aircraft maintenance licence shall permit the holder to issue
certificates of release to service following maintenance on avionic and electrical systems.
4. A category C aircraft maintenance licence shall permit the holder to issue certificates of release to service following base maintenance on aircraft. The privileges apply to the aircraft in its entirety in a CAR 145 organisation.
(b) The holder of an aircraft maintenance licence may not exercise certification privileges unless: 1. in compliance with the applicable requirements of CAR M and/or CAR 145. 2. in the preceding two-year period he/she has, either had six months of
maintenance experience in accordance with the privileges granted by the aircraft maintenance licence or, met the provision for the issue of the appropriate privileges.
3. he/she is able to read, write and communicate to an understandable level in the
language(s) in which the technical documentation and procedures necessary to support the issue of the certificate of release to service are written.
CAR 66.25 Basic knowledge requirements (a) An applicant for an aircraft maintenance licence or the addition of a category or
subcategory to such an aircraft maintenance licence shall demonstrate, by examination, a level of knowledge in the appropriate subject modules in accordance with Appendix I to this CAR. The basic knowledge examinations shall be conducted by a training organisation appropriately approved under CAR 147 or by the GCAA.
(b) Full or partial credit against the basic knowledge requirements and associated
examination shall be given for any other technical qualification considered by the GCAA to be equivalent to the knowledge standard of this CAR. Such credits shall be established and determined by GCAA based on the supporting document presented and individual merits.
CAR 66.30 Experience requirements (a) An applicant for an aircraft maintenance licence shall have acquired:
1. for category A and subcategories B1.2 and B1.4:
(i) three years of practical maintenance experience on operating aircraft, if the applicant has no previous relevant technical training; or
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-3 01 July 2011
(ii) two years of practical maintenance experience on operating aircraft and completion of training considered relevant by the GCAA as a skilled worker, in a technical trade; or (iii) one year of practical maintenance experience on operating aircraft and completion of a CAR 147 approved basic training course.
2. for category B2 and subcategories B1.1 and B1.3:
(i) five years of practical maintenance experience on operating aircraft if the applicant has no previous relevant technical training; or (ii) three years of practical maintenance experience on operating aircraft and completion of training considered relevant by the GCAA as a skilled worker, in a technical trade; or (iii) two years of practical maintenance experience on operating aircraft and completion of a CAR 147 approved basic training course.
3. for category C with respect to large aircraft:
(i) three years of experience exercising category B1.1, B1.3 or B2 privileges on large aircraft or as CAR 145 B1.1, B1.3 or B2 support staff, or, a combination of both; or (ii) five years of experience exercising category B1.2 or B1.4 privileges on large aircraft or as CAR 145 B1.2 or B1.4 support staff, or a combination of both; or
4. for category C with respect to non large aircraft:
three years of experience exercising category B1 or B.2 privileges on non large aircraft or as CAR 145 B1 or B.2 support staff, or a combination of both; or
5. for category C obtained through the academic route:
an applicant holding an academic degree in a technical discipline, from a university or other higher educational institution recognised by the GCAA, three years of experience working in a civil aircraft maintenance environment on a representative selection of tasks directly associated with aircraft maintenance including six months of observation of base maintenance tasks.
(b) An applicant for an extension to an aircraft maintenance licence shall have a minimum
civil aircraft maintenance experience requirement appropriate to the additional category or subcategory of licence applied for as defined in Appendix IV to this CAR.
(c) For category A, B1 and B2 the experience must be practical which means being involved
with a representative cross section of maintenance tasks on aircraft. (d) For all applicants, at least one year of the required experience must be recent
maintenance experience on aircraft of the category/subcategory for which the initial aircraft maintenance licence is sought. For subsequent category/subcategory additions
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-4 01 July 2011
to an existing aircraft maintenance licence, the additional recent maintenance experience required may be less than one year, but must be at least three months. The required experience must be dependent upon the difference between the licence category/subcategory held and applied for. Such additional experience must be typical of the new licence category/subcategory sought.
(e) Notwithstanding paragraph (a), aircraft maintenance experience gained outside a civil
aircraft maintenance environment shall be accepted when such maintenance is equivalent to that required by this CAR as established by the GCAA. Additional experience of civil aircraft maintenance shall, however, be required to ensure understanding of the civil aircraft maintenance environment.
Note: Where it mention ‘aircraft maintenance experience’ above, it means a documented Schedule of Inspection Works compiled in appropriate format as agreed by GCAA.
CAR 66.40 Continued validity of the aircraft maintenance licence (a) The aircraft maintenance licence becomes invalid eight years after its last issue or
amendment, unless the holder submits his/her aircraft maintenance licence to the GCAA that issued it, in order to verify that the information contained in the licence is the same as that contained in the GCAA records.
(b) Any certification privileges based upon an aircraft maintenance licence becomes invalid
as soon as the aircraft maintenance licence is invalid. (c) The aircraft maintenance licence is only valid when issued and/or amended by the
GCAA and when the holder has signed the document. CAR 66.45 Type/task training and ratings (a) The holder of a category A aircraft maintenance licence may only exercise certification
privileges on a specific aircraft type following the satisfactory completion of the relevant category A aircraft task training carried out by an appropriately approved CAR 145 or CAR 147 organisation. The training shall include practical hands on training and theoretical training as appropriate for each task authorised. Satisfactory completion of training shall be demonstrated by an examination and/or by workplace assessment carried out by an appropriately approved CAR 145 or CAR 147 organisation.
(b) Except as otherwise specified in paragraph (g), the holder of a category B1, B2 or C
aircraft maintenance licence shall only exercise certification privileges on a specific aircraft type when the aircraft maintenance licence is endorsed with the appropriate aircraft type rating.
(c) Except as otherwise specified in paragraph (h), ratings shall be granted following
satisfactory completion of the relevant category B1, B2 or C aircraft type training approved by the GCAA or conducted by an appropriately approved CAR 147 maintenance training organisation.
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-5 01 July 2011
(d) Category B1 and B2 approved type training shall include theoretical and practical elements and consist of the appropriate course in relation to the CAR 66.20(a) privileges. Theoretical and practical training shall comply with Appendix III to this CAR.
(e) Category C approved type training shall comply with Appendix III to this CAR. In the case
of a category C person qualified by holding an academic degree as specified in CAR 66.30(a), (5), the first relevant aircraft type theoretical training shall be at the category B1 or B2 level. Practical training is not required.
(f) Completion of approved aircraft type training, as required by paragraphs (b) to (e), shall
be demonstrated by an examination. The examination shall comply with Appendix III to this CAR. The examinations in respect of category B1 or B2 or C aircraft type ratings shall be conducted by training organisations appropriately approved under CAR 147, the GCAA, or the training organisation conducting the approved type training course. Where satisfactory completion of the course is required as part of the assessment procedure for the extension of a licence to include a Type Rating, the course should have been completed within 3 years immediately preceding the date of application for the endorsement or extension.
(g) Notwithstanding paragraph (b), for aircraft other than large aircraft, the holder of a
category B1 or B2 aircraft maintenance licence may also exercise certification privileges, when the aircraft maintenance licence is endorsed with the appropriate group ratings, or manufacturer group ratings, unless the GCAA has determined that the complexity of the aircraft in question requires a type rating.
1. Manufacturer group ratings may be granted after complying with the type rating
requirements of two aircraft types’ representative of the group from the same manufacturer.
2. Full group ratings may be granted after complying with the type rating
requirements of three aircraft types’ representative of the group from different manufacturers. However, no full group rating may be granted to B1 multiple turbine engine aeroplanes, where only manufacturer group rating applies.
3. The groups shall consist of the following:
(i) for category B1 or C:
— helicopter piston engine — helicopter turbine engine — aeroplane single piston engine — metal structure — aeroplane multiple piston engines — metal structure — aeroplane single piston engine — wooden structure — aeroplane multiple piston engines — wooden structure — aeroplane single piston engine — composite structure
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-6 01 July 2011
— aeroplane multiple piston engines — composite structure — aeroplane turbine — single engine — aeroplane turbine — multiple engine
(ii) for category B2 or C:
— aeroplane — helicopter
(h) Notwithstanding paragraph (c), ratings on aircraft other than large aircraft may also be
granted, subject to satisfactory completion of the relevant category B1, B2 or C aircraft type examination and demonstration of practical experience on the aircraft type, unless the GCAA has determined that the aircraft is complex, where paragraph 3 approved type training is required.
In the case of category C ratings on aircraft other than large aircraft, for a person qualified by holding an academic degree as specified in CAR 66.30 (a), (5), the first relevant aircraft type examination shall be at the category B1 or B2 level. 1. Category B1, B2 and C approved type examinations must consist of a mechanical
examination for category B1 and an avionics examination for category B2 and both mechanical and avionics examination for category C.
2. The examination shall comply with Appendix III to this CAR. The examination shall
be conducted by training organisations appropriately approved under CAR 147, or by the GCAA.
3. Aircraft type practical experience shall include a representative cross section of
maintenance activities relevant to the category. CAR 66.55 Evidence of qualification Personnel exercising certification privileges must produce their licence, as evidence of qualification, if requested by an authorized person, within 24 hours. CAR 66.70 Conversion provisions (a) The holder of a certifying staff qualification valid in a foreign State, prior to the date of
entry into force of this CAR may be issued an aircraft maintenance licence without further examination subject to the conditions specified in CAAP 28.
(b) A person undergoing a qualification process valid in a foreign State, prior to the date of
entry into force of this CAR may continue to be qualified. The holder of a qualification gained following such qualification process may be issued an aircraft maintenance licence without further examination subject to the conditions specified in CAAP 28.
SECTION 1 CAR 66 Subpart A
Rev 00 1-A-7 01 July 2011
(c) Where necessary, the aircraft maintenance licence shall contain technical limitations in relation to the scope of the pre-existing qualification.
SECTION 1 CAR 66 Subpart B
Rev 00 1-B-1 01 July 2011
SUBPART B – AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS CAR 66.100 General Until such time as this Subpart specifies a requirement for certifying staff of aircraft other than aeroplanes and helicopters, the relevant GCAA regulations shall apply.
Rev 00 1-C-1 01 July 2011
SUBPART C – COMPONENTS CAR 66.200 General Until such time as this Subpart specifies a requirement for certifying components, the relevant GCAA regulations shall apply.
SECTION 1 CAR 66 Subpart C
Rev 00 2-1 01 July 2011
APPENDIX I
BASIC KNOWLEDGE REQUIREMENTS
1. Knowledge Levels — Category A, B1, B2 and C Aircraft Maintenance Licence Basic knowledge for categories A, B1 and B2 are indicated by the allocation of knowledge levels indicators (1, 2 or 3) against each applicable subject. Category C applicants must meet either the category B1 or the category B2 basic knowledge levels. The knowledge level indicators are defined as follows: Level 1 A familiarisation with the principal elements of the subject. Objectives: The applicant should be familiar with the basic elements of the subject. The applicant should be able to give a simple description of the whole subject, using common words and examples. The applicant should be able to use typical terms. Level 2 A general knowledge of the theoretical and practical aspects of the subject. An ability to apply that knowledge. Objectives: The applicant should be able to understand the theoretical fundamentals of the subject. The applicant should be able to give a general description of the subject using, as appropriate, typical examples. The applicant should be able to use mathematical formulae in conjunction with physical laws describing the subject. The applicant should be able to read and understand sketches, drawings and schematics describing the subject. 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. A capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner.
SECTION 2 CAR 66
Rev 00 2-2 01 July 2011
Objectives: The applicant should know the theory of the subject and interrelationships with other subjects. The applicant should be able to give a detailed description of the subject using theoretical fundamentals and specific examples. The applicant should understand and be able to use mathematical formulae related to the subject. The applicant should be able to read, understand and prepare sketches, simple drawings and schematics describing the subject. The applicant should be able to apply his knowledge in a practical manner using manufacturer’s instructions. The applicant should be able to interpret results from various sources and measurements and apply corrective action where appropriate. 2. Modularisation Qualification on basic subjects for each CAR 66 aircraft maintenance licence category or subcategory should be in accordance with the following matrix. Applicable subjects are indicated by an ‘X’:
Subject modules
A or B1 aeroplane with: A or B1 helicopter with: B2
Turbine engine(s) Piston engine(s) Turbine engine(s) Piston engine(s) Avionics
1 X X X X X
2 X X X X X
3 X X X X X
4 X X X X X
5 X X X X X
6 X X X X X
7 X X X X X
8 X X X X X
9 X X X X X
10 X X X X X
11 X X
12 X X
13 X
14 X
15 X X
16 X X
17 X X
SECTION 2 CAR 66
Rev 00 2-3 01 July 2011
MODULE 1. MATHEMATICS
Level
A B1 B2
1.1 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, square and cube roots. 1.2 Algebra (a) Evaluating simple algebraic expressions, addition, subtraction, multiplication and division, use of brackets, simple algebraic fractions; (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; 1.3 Geometry (a) Simple geometrical constructions; (b) Graphical representation; nature and uses of graphs, graphs of equations/functions; (c) Simple trigonometry; trigonometrical relationships, use of tables and rectangular and polar coordinates.
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SECTION 2 CAR 66
Rev 00 2-4 01 July 2011
MODULE 2. PHYSICS
Level
A B1 B2
2.1 Matter 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 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; Pressure and buoyancy in liquids (barometers). 2.2.2 Kinetics 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; (b) Momentum, conservation of momentum; Impulse; Gyroscopic principles; Friction: nature and effects, coefficient of friction (rolling resistance). 2.2.4 Fluid dynamics (a)
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SECTION 2 CAR 66
Rev 00 2-5 01 July 2011
Level
A B1 B2
Specific gravity and density; (b) Viscosity, fluid resistance, effects of streamlining; effects of compressibility on fluids; Static, dynamic and total pressure: Bernoulli's Theorem, venturi. 2.3 Thermodynamics (a) Temperature: thermometers and temperature scales: Celsius, Fahrenheit and Kelvin; Heat definition. (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. 2.4 Optics (Light) 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 Wave motion: mechanical waves, sinusoidal wave motion, interference phenomena, standing waves; Sound: speed of sound, production of sound, intensity, pitch and quality, Doppler effect.
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SECTION 2 CAR 66
Rev 00 2-6 01 July 2011
MODULE 3. ELECTRICAL FUNDAMENTALS
Level
A B1 B2
3.1 Electron Theory Structure and distribution of electrical charges within: atoms, molecules, ions, compounds; Molecular structure of conductors, semiconductors and insulators. 3.2 Static Electricity and Conduction 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 a vacuum. 3.3 Electrical Terminology 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 Production of electricity by the following methods: light, heat, friction, pressure, chemical action, magnetism and motion. 3.5 DC Sources of Electricity Construction and basic chemical action of: primary cells, secondary cells, lead acid cells, nickel cadmium cells, other alkaline cells; Cells connected in series and parallel; Internal resistance and its effect on a battery; Construction, materials and operation of thermocouples; Operation of photo-cells. 3.6 DC Circuits Ohms Law, Kirchoff'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 and affecting factors; Specific resistance;
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SECTION 2 CAR 66
Rev 00 2-7 01 July 2011
Resistor colour code, values and tolerances, preferred values, wattage ratings; Resistors in series and parallel; Calculation of total resistance using series, parallel and series parallel combinations; Operation and use of potentiometers and rheostats; Operation of Wheatstone Bridge. (b) Positive and negative temperature coefficient conductance; Fixed resistors, stability, tolerance and limitations, methods of construction; Variable resistors, thermistors, voltage dependent resistors; Construction of potentiometers and rheostats; Construction of Wheatstone Bridge; 3.8 Power 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 Operation and function of a capacitor; Factors affecting 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 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;
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SECTION 2 CAR 66
Rev 00 2-8 01 July 2011
Magnetic shielding; Various types of magnetic material; Electromagnets construction and principles of operation; Hand clasp rules to determine: magnetic field around current carrying conductor. (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. 3.11 Inductance/Inductor Faraday's Law; Action of inducing a voltage in a conductor moving 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 the rate of change of primary mutual inductance has on induced voltage; Factors affecting mutual inductance: number of turns in coil, physical size of coil, permeability of coil, position of coils with respect to each other; Lenz's Law and polarity determining rules; Back emf, self induction; Saturation point; Principle uses of inductors; 3.12 DC Motor/Generator Theory Basic motor and generator theory; Construction and purpose of components in DC generator; Operation of, and factors affecting output and direction of current flow in DC generators; Operation of, and factors affecting 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
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SECTION 2 CAR 66
Rev 00 2-9 01 July 2011
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/3 phase principles. 3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits Phase 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 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; Calculation of line and phase voltages and currents; Calculation of power in a three phase system; Primary and Secondary current, voltage, turns ratio, power, efficiency; Auto transformers. 3.16 Filters Operation, application and uses of the following filters: low pass, high pass, band pass, band stop. 3.17 AC Generators 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 connections advantages and uses; Permanent Magnet Generators. 3.18 AC Motors Construction, principles of operation and characteristics of: AC synchronous and induction motors both single and polyphase; Methods of speed control and direction of rotation;
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SECTION 2 CAR 66
Rev 00 2-10 01 July 2011
Methods of producing a rotating field: capacitor, inductor, shaded or split pole.
SECTION 2 CAR 66
Rev 00 2-11 01 July 2011
MODULE 4. ELECTRONIC FUNDAMENTALS
Level
A B1 B2
4.1 Semiconductors 4.1.1 Diodes (a) Diode symbols; Diode characteristics and properties; Diodes in series and parallel; Main characteristics and use of silicon controlled rectifiers (thyristors), light emitting diode, photo conductive diode, varistor, rectifier diodes; Functional testing of diodes. (b) Materials, electron configuration, electrical properties; P and N type materials: effects of impurities on conduction, majority and minority characters; PN junction in a semiconductor, development of a potential across a PN junction in unbiased, forward biased and reverse biased conditions; Diode parameters: peak inverse voltage, maximum forward current, temperature, frequency, leakage current, power dissipation; 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, Shottky diode, photo conductive diode, varactor diode, varistor, rectifier diodes, and Zener diode. 4.1.2 Transistors (a) Transistor symbols; Component description and orientation; Transistor characteristics and properties. (b) Construction and operation of PNP and NPN transistors; Base, collector and emitter configurations; Testing of transistors. Basic appreciation of other transistor types and their uses.
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SECTION 2 CAR 66
Rev 00 2-12 01 July 2011
Application of transistors: classes of amplifier (A, B, C); Simple circuits including: bias, decoupling, feedback and stabilisation; Multistage circuit principles: cascades, push-pull, oscillators, multivibrators, flip-flop circuits. 4.1.3 Integrated Circuits (a) Description and operation of logic circuits and linear circuits/operational amplifiers. (b) Description and operation of logic circuits and linear circuits; Introduction to operation and function of an operational amplifier used as: integrator, differentiator, voltage follower, comparator; Operation and amplifier stages connecting methods: resistive capacitive, inductive (transformer), inductive resistive (IR), direct; Advantages and disadvantages of positive and negative feedback. 4.2 Printed Circuit Boards Description and use of printed circuit boards. 4.3 Servomechanisms (a) Understanding of the following terms: Open and closed loop systems, feedback, follow up, analogue transducers; Principles of operation and use of the following synchro system components/features: resolvers, differential, control and torque, transformers, inductance and capacitance transmitters. (b) Understanding of the following terms: Open and closed loop, follow up, servomechanism, analogue, transducer, null, damping, feedback, deadband; 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; Servomechanism defects, reversal of synchro leads, hunting.
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SECTION 2 CAR 66
Rev 00 2-13 01 July 2011
MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS
Level
A B1.1 B1.3
B1.2 B1.4
B2
5.1 Electronic Instrument Systems Typical systems arrangements and cockpit layout of electronic instrument systems. 5.2 Numbering Systems Numbering systems: binary, octal and hexadecimal; Demonstration of conversions between the decimal and binary, octal and hexadecimal systems and vice versa. 5.3 Data Conversion 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 Operation of data buses in aircraft systems, including knowledge of ARINC and other specifications. 5.5 Logic Circuits (a) Identification of common logic gate symbols, tables and equivalent circuits; Applications used for aircraft systems, schematic diagrams. (b) Interpretation of logic diagrams. 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). (b) Computer related terminology; Operation, layout and interface of the major components in a micro computer including their associated bus systems; Information contained in single and multiaddress instruction words;
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SECTION 2 CAR 66
Rev 00 2-14 01 July 2011
Memory associated terms; Operation of typical memory devices; Operation, advantages and disadvantages of the various data storage systems. 5.7 Microprocessors 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 Operation and use of encoders and decoders; Function of encoder types; Uses of medium, large and very large scale integration. 5.9 Multiplexing Operation, application and identification in logic diagrams of multiplexers and demultiplexers. 5.10 Fibre Optics 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 Principles of operation of common types of displays used in modern aircraft, including Cathode Ray Tubes, Light Emitting Diodes and Liquid Crystal Display. 5.12 Electrostatic Sensitive Devices Special handling of components sensitive to electrostatic discharges; Awareness of risks and possible damage, component and personnel anti-static protection devices. 5.13 Software Management Control Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programmes.
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SECTION 2 CAR 66
Rev 00 2-15 01 July 2011
5.14 Electromagnetic Environment Influence of the following phenomena on maintenance practices for electronic system: EMC-Electromagnetic Compatibility EMI-Electromagnetic Interference HIRF-High Intensity Radiated Field Lightning/lightning protection 5.15 Typical Electronic/Digital Aircraft Systems General arrangement of typical electronic/digital aircraft systems and associated BITE (Built In Test Equipment) testing such as: ACARS-ARINC Communication and Addressing and Reporting System ECAM-Electronic Centralised Aircraft Monitoring EFIS-Electronic Flight Instrument System EICAS-Engine Indication and Crew Alerting System FBW-Fly by Wire FMS-Flight Management System GPS-Global Positioning System IRS-Inertial Reference System TCAS-Traffic Alert Collision Avoidance System
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SECTION 2 CAR 66
Rev 00 2-16 01 July 2011
MODULE 6. MATERIALS AND HARDWARE
Level
A B1 B2
6.1 Aircraft Materials — Ferrous (a) Characteristics, properties and identification of alloy steels used in aircraft; common Heat treatment and application of alloy steels; (b) Testing of ferrous materials for hardness, tensile strength, fatigue strength and impact resistance. 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; (b) Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance. 6.3 Aircraft Materials — Composite and Non-Metallic 6.3.1 Composite and non-metallic 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. (b) The detection of defects/deterioration in composite and non-metallic material. Repair of composite and non-metallic material. 6.3.2 Wooden structures Construction methods of wooden airframe structures; Characteristics, properties and types of wood and glue used in aeroplanes; Preservation and maintenance of wooden structure; Types of defects in wood material and wooden structures;
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SECTION 2 CAR 66
Rev 00 2-17 01 July 2011
The detection of defects in wooden structure; Repair of wooden structure. 6.3.3 Fabric covering Characteristics, properties and types of fabrics used in aeroplanes; Inspections methods for fabric; Types of defects in fabric; Repair of fabric covering. 6.4 Corrosion (a) Chemical fundamentals; Formation by, galvanic action process, microbiological, stress; (b) Types of corrosion and their identification; Causes of corrosion; Material types, susceptibility to corrosion. 6.5 Fasteners 6.5.1 Screw threads Screw nomenclature; Thread forms, dimensions and tolerances for standard threads used in aircraft; Measuring screw threads; 6.5.2 Bolts, studs and screws 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 Tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quick release fasteners, keys, circlips, cotter pins. 6.5.4 Aircraft rivets Types of solid and blind rivets: specifications and identification, heat treatment.
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SECTION 2 CAR 66
Rev 00 2-18 01 July 2011
6.6 Pipes and Unions (a) Identification of, and types of rigid and flexible pipes and their connectors used in aircraft; (b) Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system pipes. 6.7 Springs Types of springs, materials, characteristics and applications. 6.8 Bearings Purpose of bearings, loads, material, construction; Types of bearings and their application. 6.9 Transmissions 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 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 Cable types, construction and characteristics; High tension and co-axial cables; Crimping; Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes.
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SECTION 2 CAR 66
Rev 00 2-19 01 July 2011
MODULE 7. MAINTENANCE PRACTICES
Level
A B1 B2
7.1 Safety Precautions-Aircraft and Workshop Aspects of safe working practices including precautions to take when working with electricity, gases especially oxygen, oils and chemicals. Also, instruction in the remedial action to be taken in the event of a fire or another accident with one or more of these hazards including knowledge on extinguishing agents. 7.2 Workshop Practices Care of tools, control of tools, use of workshop materials; Dimensions, allowances and tolerances, standards of workmanship; Calibration of tools and equipment, calibration standards. 7.3 Tools 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 Avionic General Test Equipment Operation, function and use of avionic general test equipment. 7.5 Engineering Drawings, Diagrams and Standards Drawing types and diagrams, their symbols, dimensions, tolerances and projections; Identifying 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 Drill sizes for bolt holes, classes of fits; Common system of fits and clearances; Schedule of fits and clearances for aircraft and engines;
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SECTION 2 CAR 66
Rev 00 2-20 01 July 2011
Limits for bow, twist and wear; Standard methods for checking shafts, bearings and other parts. 7.7 Electrical Cables and Connectors Continuity, insulation and bonding techniques and testing; Use of crimp tools: hand and hydraulic operated; Testing of crimp joints; Connector pin removal and insertion; Co-axial cables: testing and installation precautions; Wiring protection techniques: Cable looming and loom support, cable clamps, protective sleeving techniques including heat shrink wrapping, shielding. 7.8 Riveting Riveted joints, rivet spacing and pitch; Tools used for riveting and dimpling; Inspection of riveted joints. 7.9 Pipes and Hoses Bending and belling/flaring aircraft pipes; Inspection and testing of aircraft pipes and hoses; Installation and clamping of pipes. 7.10 Springs Inspection and testing of springs. 7.11 Bearings Testing, cleaning and inspection of bearings; Lubrication requirements of bearings; Defects in bearings and their causes. 7.12 Transmissions 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 Swaging of end fittings; Inspection and testing of control cables;
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SECTION 2 CAR 66
Rev 00 2-21 01 July 2011
Bowden cables; aircraft flexible control systems. 7.14 Material handling 7.14.1 Sheet Metal 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 Bonding practices; Environmental conditions Inspection methods 7.15 Welding, Brazing, Soldering and Bonding (a) Soldering methods; inspection of soldered joints. (b) Welding and brazing methods; Inspection of welded and brazed joints; Bonding methods and inspection of bonded joints. 7.16 Aircraft Weight and Balance (a) Centre of Gravity/Balance limits calculation: use of relevant documents; (b) Preparation of aircraft for weighing; Aircraft weighing; 7.17 Aircraft Handling and Storage 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.
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SECTION 2 CAR 66
Rev 00 2-22 01 July 2011
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. (b) General repair methods, Structural Repair Manual; Ageing, fatigue and corrosion control programmes; (c) Non destructive inspection techniques including, penetrant, radiographic, eddy current, ultrasonic and boroscope methods. (d) Disassembly and re-assembly techniques. (e) Trouble shooting techniques 7.19 Abnormal Events (a) Inspections following lightning strikes and HIRF penetration. (b) Inspections following abnormal events such as heavy landings and flight through turbulence. 7.20 Maintenance Procedures 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
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SECTION 2 CAR 66
Rev 00 2-23 01 July 2011
MODULE 8. BASIC AERODYNAMICS
Level
A B1 B2
8.1 Physics of the Atmosphere International Standard Atmosphere (ISA), application to aerodynamics. 8.2 Aerodynamics 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, frost. 8.3 Theory of Flight 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 Flight Stability and Dynamics Longitudinal, lateral and directional stability (active and passive).
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SECTION 2 CAR 66
Rev 00 2-24 01 July 2011
MODULE 9. HUMAN FACTORS
Level
A B1 B2
9.1 General The need to take human factors into account; Incidents attributable to human factors/human error; ‘Murphy's’ law. 9.2 Human Performance and Limitations Vision; Hearing; Information processing; Attention and perception; Memory; Claustrophobia and physical access. 9.3 Social Psychology Responsibility: individual and group; Motivation and de-motivation; Peer pressure; ‘Culture’ issues; Team working; Management, supervision and leadership. 9.4 Factors Affecting Performance Fitness/health; Stress: domestic and work related; Time pressure and deadlines; Workload: overload and underload; Sleep and fatigue, shiftwork; Alcohol, medication, drug abuse. 9.5 Physical Environment Noise and fumes; Illumination; Climate and temperature;
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SECTION 2 CAR 66
Rev 00 2-25 01 July 2011
Motion and vibration; Working environment. 9.6 Tasks Physical work; Repetitive tasks; Visual inspection; Complex systems. 9.7 Communication Within and between teams; Work logging and recording; Keeping up to date, currency; Dissemination of information. 9.8 Human Error Error models and theories; Types of error in maintenance tasks; Implications of errors (i.e accidents) Avoiding and managing errors. 9.9 Hazards in the Workplace Recognising and avoiding hazards; Dealing with emergencies.
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SECTION 2 CAR 66
Rev 00 2-26 01 July 2011
MODULE 10. AVIATION LEGISLATION
Level
A B1 B2
10.1 Regulatory Framework Role of International Civil Aviation Organisation; Role of the General Civil Aviation Authority; Relationship between CAR 145, CAR 66, CAR 147 and CAR M; Relationship with other Aviation Authorities. 10.2 CAR 66 — Certifying Staff — Maintenance Detailed understanding of CAR 66. 10.3 CAR 145 — Approved Maintenance Organisations Detailed understanding of CAR 145. 10.4 CAR-OPS — Commercial & Private Air Transportation Air Operators Certificates; Operators Responsibilities; Documents to be Carried; Aircraft Placarding (Markings); 10.5 Aircraft Certification (a) General Certification rules Type Certification; Supplemental Type Certification; CAR 21 Design/Production Organisation Approvals. (b) Documents Certificate of Airworthiness; Certificate of Registration; Noise Certificate; Weight Schedule; Radio Station Licence and Approval. 10.6 CAR M Detailed understanding of CAR M. 10.7 Applicable National and International Requirements
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SECTION 2 CAR 66
Rev 00 2-27 01 July 2011
(a) Maintenance Programmes, Maintenance checks and inspections; Master Minimum Equipment Lists, Minimum Equipment List, Dispatch Deviation Lists; Airworthiness Directives; Service Bulletins, manufacturers service information; Modifications and repairs; Maintenance documentation: maintenance manuals, structural repair manual, illustrated parts catalogue, etc.; (b) Continuing airworthiness; Test flights; ETOPS, maintenance and dispatch requirements; All Weather Operations, Category 2/3 operations and minimum equipment requirements.
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SECTION 2 CAR 66
Rev 00 2-28 01 July 2011
MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Level
A1 B1.1 B2
11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices, slots, slats, flaps, flaperons; Drag inducing devices, spoilers, lift dumpers, speed 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; 11.1.2 High Speed Flight Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number, compressibility buffet, shock wave, aerodynamic heating, area rule; Factors affecting airflow in engine intakes of high speed aircraft; Effects of sweepback on critical Mach number. 11.2 Airframe Structures — General Concepts (a) Airworthiness requirements for structural strength; Structural classification, primary, secondary and 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 provision.
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SECTION 2 CAR 66
Rev 00 2-29 01 July 2011
Aircraft bonding (b) Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive 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. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 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. 11.3.2 Wings (ATA 57) Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 11.3.3 Stabilisers (ATA 55) Construction; Control surface attachment. 11.3.4 Flight Control Surfaces (ATA 55/57) Construction and attachment; Balancing — mass and aerodynamic. 11.3.5 Nacelles/Pylons (ATA 54) Construction; Firewalls; Engine mounts. 11.4 Air Conditioning and Cabin Pressurisation (ATA 21)
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SECTION 2 CAR 66
Rev 00 2-30 01 July 2011
11.4.1 Air supply Sources of air supply including engine bleed, APU and ground cart; 11.4.2 Air Conditioning Air conditioning systems; Air cycle and vapour cycle machines; Distribution systems; Flow, temperature and humidity control system. 11.4.3 Pressurisation Pressurisation systems; Control and indication including control and safety valves; Cabin pressure controllers. 11.4.4 Safety and warning devices Protection and warning devices. 11.5 Instruments/Avionic Systems 11.5.1 Instrument Systems (ATA 31) Pitot static: altimeter, air speed 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; Angle of attack indication, stall warning systems; Other aircraft system indication. 11.5.2 Avionic Systems Fundamentals of system lay-outs and operation of; Auto Flight (ATA 22); Communications (ATA 23); Navigation Systems (ATA 34). 11.6 Electrical Power (ATA 24) Batteries Installation and Operation; DC power generation; AC power generation; Emergency power generation;
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SECTION 2 CAR 66
Rev 00 2-31 01 July 2011
Voltage regulation; Power distribution; Inverters, transformers, rectifiers; Circuit protection. External/Ground power; 11.7 Equipment and Furnishings (ATA 25) (a) Emergency equipment requirements; Seats, harnesses and belts. (b) Cabin lay-out; Equipment lay-out; Cabin Furnishing Installation; Cabin entertainment equipment; Galley installation; Cargo handling and retention equipment; Airstairs. 11.8 Fire Protection (ATA 26) (a) Fire and smoke detection and warning systems; Fire extinguishing systems; System tests. (b) Portable fire extinguisher 11.9 Flight Controls (ATA 27) Primary controls: aileron, elevator, rudder, spoiler; Trim control; Active load control; High lift devices; Lift dump, speed brakes; System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;
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SECTION 2 CAR 66
Rev 00 2-32 01 July 2011
Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems; Balancing and rigging; Stall protection/warning system. 11.10 Fuel Systems (ATA 28) System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling; Longitudinal balance fuel systems. 11.11 Hydraulic Power (ATA 29) System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Pressure Control; Power distribution; Indication and warning systems; Interface with other systems. 11.12 Ice and Rain Protection (ATA 30) Ice formation, classification and detection; Anti-icing systems: electrical, hot air and chemical; De-icing systems: electrical, hot air, pneumatic and chemical; Rain repellant; Probe and drain heating. Wiper systems 11.13 Landing Gear (ATA 32)
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SECTION 2 CAR 66
Rev 00 2-33 01 July 2011
Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, brakes, antiskid and autobraking; Tyres; Steering. 11.14 Lights (ATA 33) External: navigation, anti-collision, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 11.15 Oxygen (ATA 35) System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings; 11.16 Pneumatic/Vacuum (ATA 36) System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 11.17 Water/Waste (ATA 38) Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing; Corrosion aspects. 11.18 On Board Maintenance Systems (ATA 45) Central maintenance computers; Data loading system; Electronic library system; Printing;
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SECTION 2 CAR 66
Rev 00 2-34 01 July 2011
Structure monitoring (damage tolerance monitoring).
SECTION 2 CAR 66
Rev 00 2-35 01 July 2011
MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Note: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1.2 subcategory.
Level
A2 B1.2 B2
11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices, slots, slats, flaps, flaperons; Drag inducing devices, spoilers, lift dumpers, speed 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; 11.1.2 High Speed Flight — N/A 11.2 Airframe Structures — General Concepts (a) Airworthiness requirements for structural strength; Structural classification, primary, secondary and 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 provision. Aircraft bonding (b) Construction methods of: stressed skin fuselage, formers, stringers, longerons,
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SECTION 2 CAR 66
Rev 00 2-36 01 July 2011
bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive 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. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) Construction and pressurisation sealing; Wing, tail-plane pylon and undercarriage attachments; Seat installation; Doors and emergency exits: construction and operation; Window and windscreen attachment. 11.3.2 Wings (ATA 57) Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 11.3.3 Stabilisers (ATA 55) Construction; Control surface attachment. 11.3.4 Flight Control Surfaces (ATA 55/57) Construction and attachment; Balancing — mass and aerodynamic. 11.3.5 Nacelles/Pylons (ATA 54) (a) Nacelles/Pylons: — Construction; — Firewalls; — Engine mounts. 11.4 Air Conditioning and Cabin Pressurisation (ATA 21) Pressurisation and air conditioning systems; Cabin pressure controllers, protection and warning devices. 11.5 Instruments/Avionic Systems
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SECTION 2 CAR 66
Rev 00 2-37 01 July 2011
11.5.1 Instrument Systems (ATA 31) Pitot static: altimeter, air speed 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; Angle of attack indication, stall warning systems. Other aircraft system indication. 11.5.2 Avionic Systems Fundamentals of system lay-outs and operation of: — Auto Flight (ATA 22); — Communications (ATA 23); — Navigation Systems (ATA 34). 11.6 Electrical Power (ATA 24) Batteries Installation and Operation; DC power generation; Voltage regulation; Power distribution; Circuit protection; Inverters, transformers. 11.7 Equipment and Furnishings (ATA 25) (a) Emergency equipment requirements; Seats, harnesses and belts. (b) Cabin lay-out; Equipment lay-out; Cabin Furnishing Installation (level 2); Cabin entertainment equipment; Galley installation; Cargo handling and retention equipment; Airstairs. 11.8 Fire Protection (ATA 26)
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SECTION 2 CAR 66
Rev 00 2-38 01 July 2011
(a) Fire extinguishing systems; Fire and smoke detection and warning systems; System tests. (b) Portable fire extinguisher. 11.9 Flight Controls (ATA 27) Primary controls: aileron, elevator, rudder; Trim tabs; High lift devices; System operation: manual; Gust locks; Balancing and rigging; Stall warning system. 11.10 Fuel Systems (ATA 28) System lay-out; Fuel tanks; Supply systems; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling. 11.11 Hydraulic Power (ATA 29) System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical; Pressure Control; Power distribution; Indication and warning systems. 11.12 Ice and Rain Protection (ATA 30) Ice formation, classification and detection;
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SECTION 2 CAR 66
Rev 00 2-39 01 July 2011
De-icing systems: electrical, hot air, pneumatic and chemical; Probe and drain heating; Wiper systems. 11.13 Landing Gear (ATA 32) Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, brakes, antiskid and autobraking; Tyres; Steering. 11.14 Lights (ATA 33) External: navigation, anti collision, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 11.15 Oxygen (ATA 35) System lay-out: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings; 11.16 Pneumatic/Vacuum (ATA 36) System lay-out; Sources: engine/APU, compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interfaces with other systems. 11.17 Water/Waste (ATA 38) Water system lay-out, supply, distribution, servicing and draining; Toilet system lay-out, flushing and servicing; Corrosion aspects.
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SECTION 2 CAR 66
Rev 00 2-40 01 July 2011
MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS
Level
A3 A4
B1.3 B1.4
B2
12.1 Theory of Flight — Rotary Wing Aerodynamics 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 settling, overpitching; Auto-rotation; Ground effect. 12.2 Flight Control Systems Cyclic control; Collective control; Swashplate; Yaw control: Anti-Torque 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 and fly-bywire; Artificial feel; Balancing and Rigging. 12.3 Blade Tracking and Vibration Analysis Rotor alignment; Main and tail rotor tracking; Static and dynamic balancing; Vibration types, vibration reduction methods; Ground resonance.
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SECTION 2 CAR 66
Rev 00 2-41 01 July 2011
12.4 Transmissions Gear boxes, main and tail rotors; Clutches, free wheel units and rotor brake. 12.5 Airframe Structures (a) Airworthiness requirements for structural strength; Structural classification, primary, secondary and 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 provision. (b) Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning and anti-corrosive 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 of surface protection, such as chromating, anodising, painting; Surface cleaning. Airframe symmetry: methods of alignment and symmetry checks. 12.6 Air Conditioning (ATA 21) 12.6.1 Air supply Sources of air supply including engine bleed and ground cart; 12.6.2 Air Conditioning
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SECTION 2 CAR 66
Rev 00 2-42 01 July 2011
Air conditioning systems; Distribution systems; Flow and temperature control systems; Protection and warning devices. 12.7 Instruments/Avionic Systems 12.7.1 Instrument Systems (ATA 31) Pitot static:altimeter, air speed 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 — HUMS; Other aircraft system indication. 12.7.2 Avionic Systems Fundamentals of system layouts and operation of: Auto Flight (ATA 22); Communications (ATA 23); Navigation Systems (ATA 34). 12.8 Electrical Power (ATA 24) Batteries Installation and Operation; 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. (b)
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SECTION 2 CAR 66
Rev 00 2-43 01 July 2011
Emergency flotation systems; Cabin lay-out, cargo retention; Equipment lay-out; Cabin Furnishing Installation. 12.10 Fire Protection (ATA 26) Fire and smoke detection and warning systems; Fire extinguishing systems; System tests. 12.11 Fuel Systems (ATA 28) System lay-out; Fuel tanks; Supply systems; Dumping, venting and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling. 12.12 Hydraulic Power (ATA 29) System lay-out; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Pressure Control; Power distribution; Indication and warning systems; Interface with other systems. 12.13 Ice and Rain Protection (ATA 30) Ice formation, classification and detection; Anti-icing and de-icing systems: electrical, hot air and chemical; Rain repellant and removal; Probe and drain heating.
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SECTION 2 CAR 66
Rev 00 2-44 01 July 2011
12.14 Landing Gear (ATA 32) Construction, shock absorbing; Extension and retraction systems: normal and emergency; Indications and warning; Wheels, tyres, brakes; Steering; Skids, floats. 12.15 Lights (ATA 33) External: navigation, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 12.16 Pneumatic/Vacuum (ATA 36) System lay-out; Sources: engine, compressors, reservoirs, ground supply.; Pressure control; Distribution; Indications and warnings; Interfaces with other systems.
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SECTION 2 CAR 66
Rev 00 2-45 01 July 2011
MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS
Level
A B1 B2
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; — yaw control, rudder limiters; Control using elevons, ruddervators; High lift devices: slots, slats, flaps; Drag inducing devices: spoilers, lift dumpers, speed brakes; Operation and effect of trim tabs, servo tabs, control surface bias. (b) High Speed Flight Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number. (c) Rotary Wing Aerodynamics Terminology; Operation and effect of cyclic, collective and anti-torque controls. 13.2 Structures — General Concepts (a) Fundamentals of structural systems. (b) Zonal and station identification systems; Electrical bonding; Lightning strike protection provision. 13.3 Autoflight (ATA 22) Fundamentals of automatic flight control including working principles and current terminology; Command signal processing; Modes of operation: roll, pitch and yaw channels; Yaw dampers; Stability Augmentation System in helicopters;
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SECTION 2 CAR 66
Rev 00 2-46 01 July 2011
Automatic trim control; Autopilot navigation aids interface; Autothrottle systems. Automatic Landing Systems: principles and categories, modes of operation, approach, glideslope, land, go-around, system monitors and failure conditions. 13.4 Communication/Navigation (ATA 23/34) Fundamentals of radio wave propagation, antennas, transmission lines, communication, receiver and transmitter; Working principles of following systems: — Very High Frequency (VHF) communication; — High Frequency (HF) communication; — Audio; — Emergency Locator Transmitters; — Cockpit Voice Recorder; — Very High Frequency omnidirectional range (VOR); — Automatic Direction Finding (ADF); — Instrument Landing System (ILS); — Microwave Landing System (MLS); — Flight Director systems; Distance Measuring Equipment (DME); — Very Low Frequency and hyperbolic navigation (VLF/Omega); — Doppler navigation; — Area navigation, RNAV systems; — Flight Management Systems; — Global Positioning System (GPS), Global Navigation Satellite Systems (GNSS); — Inertial Navigation System; — Air Traffic Control transponder, secondary surveillance radar; — Traffic Alert and Collision Avoidance System (TCAS); — Weather avoidance radar; — Radio altimeter; — ARINC communication and reporting; 13.5 Electrical Power (ATA 24) Batteries Installation and Operation; DC power generation; AC power generation; Emergency power generation; Voltage regulation; Power distribution; Inverters, transformers, rectifiers; Circuit protection; External/Ground power. 13.6 Equipment and Furnishings (ATA 25) Electronic emergency equipment requirements;
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SECTION 2 CAR 66
Rev 00 2-47 01 July 2011
Cabin entertainment equipment. 13.7 Flight Controls (ATA 27) (a) Primary controls: aileron, elevator, rudder, spoiler; Trim control; Active load control; High lift devices; Lift dump, speed brakes; System operation: manual, hydraulic, pneumatic; Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks. Stall protection systems. (b) System operation: electrical, fly by wire. 13.8 Instrument Systems (ATA 31) 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; Fuel quantity indicating systems; Gyroscopic principles;
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SECTION 2 CAR 66
Rev 00 2-48 01 July 2011
Artificial horizons; Slip indicators; Directional gyros; Ground Proximity Warning Systems; Compass systems; Flight Data Recording systems; Electronic Flight Instrument Systems; Instrument warning systems including master warning systems and centralised warning panels; Stall warning systems and angle of attack indicating systems; Vibration measurement and indication. 13.9 Lights (ATA 33) External: navigation, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 13.10 On board Maintenance Systems (ATA 45) Central maintenance computers; Data loading system; Electronic library system; Printing; Structure monitoring (damage tolerance monitoring).
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SECTION 2 CAR 66
Rev 00 2-49 01 July 2011
MODULE 14. PROPULSION
Level
A B1 B2
14.1 Turbine Engines (a) Constructional arrangement and operation of turbojet, turbofan, turboshaft and turbopropeller engines; (b) Electronic Engine control and fuel metering systems (FADEC). 14.2 Engine Indicating Systems Exhaust gas temperature/Interstage turbine temperature systems; Engine speed; Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems; Oil pressure and temperature; Fuel pressure, temperature and flow; Manifold pressure; Engine torque; Propeller speed.
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SECTION 2 CAR 66
Rev 00 2-50 01 July 2011
MODULE 15. GAS TURBINE ENGINE
Level
A B1 B2
15.1 Fundamentals Potential energy, kinetic energy, Newton's laws of motion, Brayton cycle; The relationship between force, work, power, energy, velocity, acceleration; Constructional arrangement and operation of turbojet, turbofan, turboshaft, turboprop. 15.2 Engine Performance 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 Compressor inlet ducts Effects of various inlet configurations; Ice protection. 15.4 Compressors Axial and centrifugal types; Constructional features and operating principles and applications; Fan balancing; Operation: Causes and effects of compressor stall and surge; Methods of air flow control: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades; Compressor ratio. 15.5 Combustion Section Constructional features and principles of operation. 15.6 Turbine Section Operation and characteristics of different turbine blade types; Blade to disk attachment;
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SECTION 2 CAR 66
Rev 00 2-51 01 July 2011
Nozzle guide vanes; Causes and effects of turbine blade stress and creep. 15.7 Exhaust Constructional features and principles of operation; Convergent, divergent and variable area nozzles; Engine noise reduction; Thrust reversers. 15.8 Bearings and Seals Constructional features and principles of operation. 15.9 Lubricants and Fuels Properties and specifications; Fuel additives; Safety precautions. 15.10 Lubrication Systems System operation/lay-out and components. 15.11 Fuel Systems Operation of engine control and fuel metering systems including electronic engine control (FADEC); Systems lay-out and components. 15.12 Air Systems Operation of engine air distribution and anti-ice control systems, including internal cooling, sealing and external air services. 15.13 Starting and Ignition Systems Operation of engine start systems and components; Ignition systems and components; Maintenance safety requirements. 15.14 Engine Indication Systems 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;
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SECTION 2 CAR 66
Rev 00 2-52 01 July 2011
Engine speed; Vibration measurement and indication; Torque; Power.
15.15 Power Augmentation Systems Operation and applications; Water injection, water methanol; Afterburner systems. 15.16 Turbo-prop Engines
Gas coupled/free turbine and gear coupled turbines; Reduction gears; Integrated engine and propeller controls; Overspeed safety devices.
15.17 Turbo-shaft engines
Arrangements, drive systems, reduction gearing, couplings, control systems.
15.18 Auxiliary Power Units (APUs)
Purpose, operation, protective systems.
15.19 Powerplant Installation
Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains.
15.20 Fire Protection Systems
Operation of detection and extinguishing systems.
15.21 Engine Monitoring and Ground Operation
Procedures for starting and ground run-up; Interpretation of engine power output and parameters; Trend (including oil analysis, vibration and boroscope) monitoring; Inspection of engine and components to criteria, tolerances and data specified by engine manufacturer; Compressor washing/cleaning; Foreign Object Damage.
15.22 Engine Storage and Preservation
Preservation and depreservation for the engine and accessories/systems.
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SECTION 2 CAR 66
Rev 00 2-53 01 July 2011
MODULE 16. PISTON ENGINE
Level
A B1 B2
16.1 Fundamentals Mechanical, thermal and volumetric efficiencies; Operating principles — 2 stroke, 4 stroke, Otto and Diesel; Piston displacement and compression ratio; Engine configuration and firing order. 16.2 Engine Performance Power calculation and measurement; Factors affecting engine power; Mixtures/leaning, pre-ignition. 16.3 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. 16.4 Engine Fuel Systems 16.4.1 Carburettors Types, construction and principles of operation; Icing and heating. 16.4.2 Fuel injection systems Types, construction and principles of operation. 16.4.3 Electronic engine control Operation of engine control and fuel metering systems including electronic engine control (FADEC); Systems lay-out and components. 16.5 Starting and Ignition Systems Starting systems, pre-heat systems; Magneto types, construction and principles of operation;
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SECTION 2 CAR 66
Rev 00 2-54 01 July 2011
Ignition harnesses, spark plugs; Low and high tension systems. 16.6 Induction, Exhaust and Cooling Systems Construction and operation of: induction systems including alternate air systems; Exhaust systems, engine cooling systems — air and liquid. 16.7 Supercharging/Turbocharging 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 Properties and specifications; Fuel additives; Safety precautions. 16.9 Lubrication Systems System operation/lay-out and components. 16.10 Engine Indication Systems Engine speed; Cylinder head temperature; Coolant temperature; Oil pressure and temperature; Exhaust Gas Temperature; Fuel pressure and flow; Manifold pressure. 16.11 Powerplant Installation Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains. 16.12 Engine Monitoring and Ground Operation Procedures for starting and ground run-up;
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SECTION 2 CAR 66
Rev 00 2-55 01 July 2011
Interpretation of engine power output and parameters; Inspection of engine and components: criteria, tolerances, and data specified by engine manufacturer. 16.13 Engine Storage and Preservation Preservation and depreservation for the engine and accessories/systems.
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SECTION 2 CAR 66
Rev 00 2-56 01 July 2011
MODULE 17. PROPELLER
Level
A B1 B2
17.1 Fundamentals 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 Construction methods and materials used in wooden, composite and metal propellers; Blade station, blade face, blade shank, blade back and hub assembly; Fixed pitch, controllable pitch, constant speeding propeller; Propeller/spinner installation. 17.3 Propeller Pitch Control Speed control and pitch change methods, mechanical and electrical/electronic; Feathering and reverse pitch; Overspeed protection. 17.4 Propeller Synchronising Synchronising and synchrophasing equipment. 17.5 Propeller Ice Protection Fluid and electrical de-icing equipment. 17.6 Propeller Maintenance 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 Propeller preservation and depreservation
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SECTION 2 CAR 66
Rev 00 2-57 01 July 2011
APPENDIX II
BASIC EXAMINATION STANDARD 1. Standardisation Basis For Examinations 1.1. All basic examinations must be carried out using the multi-choice question format and essay questions as specified below. 1.2. Each multi-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. 1.3. Each essay question requires the preparation of a written answer and the candidate must be allowed 20 minutes to answer each such question. 1.4. Suitable essay questions must be drafted and evaluated using the knowledge syllabus in CAR 66 Appendix I Modules 7, 9 and 10. 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 Part-66 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 must 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 must not be used to determine whether a candidate has passed. 1.11. All modules that make up a complete CAR 66 aircraft maintenance licence category or subcategory must be passed within a 4 year time period of passing the first module except in the case specified in paragraph 1.12. A failed module may not be retaken for at least 90 days following the date of the failed module examination, except in the case of a CAR 147 approved maintenance training organisation which conducts a course of retraining tailored to the failed subjects in the particular module when the failed module may be retaken after 30 days. 1.12. The 4 year time period specified in paragraph 1.11 does not apply to those modules which are common to more than one CAR 66 aircraft maintenance licence category or
SECTION 2 CAR 66
Rev 00 2-58 01 July 2011
subcategory and which were previously passed as part of another such category or subcategory examination. 2. Question Numbers for the CAR 66 Appendix I Modules 2.1. Subject Module 1 Mathematics: Category A-16 multi-choice and 0 essay questions. Time allowed 20 minutes. Category B1-32 multi-choice and 0 essay questions. Time allowed 43 minutes. Category B2-32 multi-choice and 0 essay questions. Time allowed 43 minutes. 2.2. Subject Module 2 Physics: Category A-32 multi-choice and 0 essay questions. Time allowed 43 minutes. Category B1-52 multi-choice and 0 essay questions. Time allowed 68 minutes. Category B2-52 multi-choice and 0 essay questions. Time allowed 68 minutes. 2.3. Subject Module 3 Electrical Fundamentals: Category A-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B1-52 multi-choice and 0 essay questions. Time allowed 68 minutes. Category B2-52 multi-choice and 0 essay questions. Time allowed 68 minutes. 2.4. Subject Module 4 Electronic Fundamentals: Category A-None. Category B1-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B2-40 multi-choice and 0 essay questions. Time allowed 50 minutes. 2.5. Subject Module 5 Digital Techniques/Electronic Instrument Systems: Category A-16 multi-choice and 0 essay questions. Time allowed 20 minutes. Category B1.1 & B1.3-40 multi-choice and 0 essay questions. Time allowed 50 minutes. Category B1.2 & B1.4-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B2-72 multi-choice and 0 essay questions. Time allowed 90 minutes. 2.6. Subject Module 6 Materials and Hardware: Category A-52 multi-choice and 0 essay questions. Time allowed 68 minutes.
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Rev 00 2-59 01 July 2011
Category B1-72 multi-choice and 0 essay questions. Time allowed 90 minutes. Category B2-60 multi-choice and 0 essay questions. Time allowed 75 minutes. 2.7. Subject Module 7 Maintenance Practices: Category A-72 multi-choice and 2 essay questions. Time allowed 90 minutes plus 40 minutes. Category B1-80 multi-choice and 2 essay questions. Time allowed 100 minutes plus 40 minutes. Category B2-60 multi-choice and 2 essay questions. Time allowed 75 minutes plus 40 minutes. 2.8. Subject Module 8 Basic Aerodynamics: Category A-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B1-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B2-20 multi-choice and 0 essay questions. Time allowed 25 minutes. 2.9. Subject Module 9 Human factors: Category A-20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes. Category B1-20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes. Category B2-20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes. 2.10. Subject Module 10 Aviation Legislation: Category A-32 multi-choice and 2 essay question. Time allowed 40 minutes plus 40 minutes. Category B1-40 multi-choice and 2 essay question. Time allowed 50 minutes plus 40 minutes. Category B2-40 multi-choice and 2 essay question. Time allowed 50 minutes plus 40 minutes. 2.11. Subject Module 11a Turbine Aeroplane Aerodynamics, Structures and Systems: Category A-100 multi-choice and 0 essay questions. Time allowed 125 minutes. Category B1-132 multi-choice and 0 essay questions. Time allowed 165 minutes. Category B2-None. 2.12. Subject Module 11b Piston Aeroplane Aerodynamics, Structures and Systems: Category A-72 multi-choice and 0 essay questions. Time allowed 90 minutes. Category B1-100 multi-choice and 0 essay questions. Time allowed 125 minutes.
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Rev 00 2-60 01 July 2011
Category B2-None. 2.13. Subject Module 12 Helicopter Aerodynamics, Structures and Systems: Category A-92 multi-choice and 0 essay questions. Time allowed 115 minutes. Category B1-116 multi-choice and 0 essay questions. Time allowed 145 minutes. Category B2-None. 2.14. Subject Module 13 Aircraft Aerodynamics, Structures and Systems: Category A-None. Category B1-None. Category B2-132 multi-choice and 0 essay questions. Time allowed 165 minutes. 2.15. Subject Module 14 Propulsion: Category A-None. Category B1-None. Category B2-28 multi-choice and 0 essay questions. Time allowed 35 minutes. 2.16. Subject Module 15 Gas Turbine Engine: Category A-60 multi-choice and 0 essay questions. Time allowed 75 minutes. Category B1-92 multi-choice and 0 essay questions. Time allowed 115 minutes. Category B2-None. 2.17. Subject Module 16 Piston Engine: Category A-52 multi-choice and 0 essay questions. Time allowed 65 minutes. Category B1-72 multi-choice and 0 essay questions. Time allowed 90 minutes. Category B2-None. 2.18. Subject Module 17 Propeller: Category A-20 multi-choice and 0 essay questions. Time allowed 25 minutes. Category B1-32 multi-choice and 0 essay questions. Time allowed 40 minutes. Category B2-None.
SECTION 2 CAR 66
Rev 00 2-61 01 July 2011
APPENDIX III
TYPE TRAINING AND EXAMINATION STANDARD 1. Type training levels The three levels listed below define the objectives that a particular level of training is intended to achieve. Level 1 General Familiarisation A brief overview of the airframe, systems and powerplants as outlined in the Systems Description Section of the Aircraft Maintenance Manual. 1. Course objectives: Upon completion of the course, the student will be able to identify
safety precautions related to the airframe, its systems and powerplant 2. Identify maintenance practices important to the airframe, its systems and powerplant 3. Define the general layout of the aircraft's major systems 4. Define the general layout and characteristics of the powerplant 5. Identify special tooling and test equipment used with the aircraft Level 2 Ramp and transit Basic system overview of controls, indicators, principal components including their location and purpose, servicing and minor troubleshooting. Course objectives: In addition to the information contained in the Level 1 General Familiarisation course, at the completion of this Level 2 Ramp and Transit training, the student will be able to: 1. Recall the safety precautions to be observed when working on or near the aircraft,
power plant and systems. 2. Demonstrate knowledge of the main ramp and transit (through-flight) activities of the
following: (a) Doors, windows and hatches. (b) Electrical power supplies. (c) Fuel. (d) Auxiliary power unit. (e) Power plant. (f) Fire protection.
SECTION 2 CAR 66
Rev 00 2-62 01 July 2011
(g) Environmental Control Systems. (h) Hydraulic power. (i) Landing gear. (j) Flight controls. (k) Water/waste. (l) Oxygen. (m) Flight and service interphone. (n) Avionics. (o) Cabin equipment/furnishings. 3. Describe systems and aircraft handling particularly access, power availability and sources. 4. Identify the locations of the principal components. 5. Explain the normal functioning of each major system, including terminology and
nomenclature. 6. Perform the procedures for ramp and transit servicing associated with the aircraft for
the following systems: Fuel, Power Plants, Hydraulics, Landing Gear, Water/Waste, and Oxygen.
7. Demonstrate proficiency in use of crew reports and on-board reporting systems (minor
troubleshooting) and determine aircraft airworthiness per the MEL/CDL. 8. Identify and use appropriate documentation. 9. Locate those procedures for replacement of components for ramp and transit activities
identified in objective 2. Level 3 Line and base maintenance training 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 III Line and Base Maintenance training, the student will be able to: (a) Perform system, engine, component and functional checks as specified in the
maintenance manual.
SECTION 2 CAR 66
Rev 00 2-63 01 July 2011
(b) Correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level. (c) Describe procedures for replacement of components unique to aircraft type. 2. Type training standard Type training must include a theoretical and practical element. 2.1. Theoretical element As a minimum the elements in the Syllabus below that are specific to the aircraft type must be covered. Additional elements introduced due to technological changes shall also be included. Training levels are those levels defined in paragraph 1 above. After the first type course for category C certifying staff all subsequent courses need only be to level 1.
Introduction Module Title
General Aircraft(dimensions/weights MTOW etc)
Time limits/maintenance checks
Levelling and weighing
Towing and taxiing
Parking/mooring
Servicing
Standard practices-only type particular
B2 module-safety items/mechanical interface
B1 module-safety items/avionics interface
Aeroplanes/Helicopters: Aeroplanes turbine
Aeroplanes piston
Helicopters turbine
Helicopters piston
Avionics
B1 C B1 C B1 C B1 C B2
Blade tracking and vibration analysis
Transmissions
Airframe structure
Main rotor
Tail rotor/rotor drive
Rotor flight control
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
3
3
3
3
3
3
1
1
1
1
1
1
3
3
3
3
3
3
1
1
1
1
1
1
-
-
1
-
-
-
Airframe Structure
Fuselage Doors
Fuselage
3
3
3
1
1
3
3
3
1
1
1
-
-
-
-
-
-
-
-
-
-
-
-
1
-
-
SECTION 2 CAR 66
Rev 00 2-64 01 July 2011
Fuselage Windows
Wings
Stabilisers
Flight Control Surfaces
Nacelles/Pylons
3
3
3
3
3
1
1
1
1
1
3
3
3
3
3
1
1
1
1
1
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
Zonal & Station Identification Systems
1 1 1 1 1 1 1 1 1
Air Supply
Air Conditioning
Pressurisation
Safety & Warning Devices
3
3
3
3
1
1
1
1
3
3
-
-
1
1
-
-
3
3
-
-
1
1
-
-
3
3
-
-
1
1
-
-
1
1
1
1
Instrument Systems
Avionics Systems
3
2
1
1
3
2
1
1
3
2
1
1
3
2
1
1
3
3
Electrical Power
3 1 3 1 3 1 3 1 3
Equipment & Furnishings
Electronic Emergency Equip. Requir. & Cabin
Entertainment Equipment
3
-
1
1
3
-
1
-
3
-
1
-
3
-
1
-
-
3
Fire Protection
3 1 3 1 3 1 3 1 1
Flight Controls
Sys. Operation: Electrical/Fly-by-Wire
3
3
1
1
3
-
1
-
3 1
-
3
-
1
-
2
3
Fuel Systems
3 1 3 1 - 1 3 1 1
Hydraulic Power
3 1 3 1 3 1 3 1 1
Ice & Rain Protection
3 1 3 1 3 1 3 1 1
Landing Gear
3 1 3 1 3 1 3 1 1
Lights
3 1 3 1 3 1 3 1 3
Oxygen
3 1 3 1 - - - - 1
Pneumatic/Vacuum
3 1 3 1 3 1 3 1 1
Water/Waste
3 1 3 1 - - - - 1
On-board Maintenance Systems
3 1 3 1 - - - - 1
Turbine Engines:
Constructional arrangement and operation
- - - - - - - - 1
Engine Performance
3 1 - - 3 1 - - 1
Inlet
3 1 - - 3 1 - - -
Compressors
3 1 - - 3 1 - - -
Combustion Section
3 1 - - 3 1 - - -
SECTION 2 CAR 66
Rev 00 2-65 01 July 2011
Turbine Section
3 1 - - 3 1 - - -
Exhaust
3 1 - - 3 1 - - -
Bearings and Seals
3 1 - - 3 1 - - -
Lubricants and Fuels
3 1 - - 3 1 - - -
Lubrication Systems
3 1 - - 3 1 - - -
Fu1el Systems
3 1 - - 3 1 - - 1
Engine controls
3 1 - - 3 1 - - 1
FADEC 3 1 - -- 2 1 - - 3
Air Systems 3 1 - - 3 1 - - -
Starting & Ignition Systems
3 1 - - 3 1 - - -
Engine Indicating Systems
3 1 - - 3 1 - - 3
Power Augmentation Systems
3 1 - - - - - - -
Turbo-prop Engines
3 1 - - - - - - -
Turbo-shaft Engines
- - - - 3 1 - - -
Auxiliary Power Units (APUs)
3 1 - - - - - - 1
Power plant Installation
3 1 - - 3 1 - - -
Fire Protection Systems
3 1 - - 3 1 - - 1
Engine Monitoring and Ground Operation
3 1 - - 3 1 - - -
Engine Storage and Preservation
3 1 - - 3 1 - - -
Piston Engines:
Engine Performance
3 - 3 1 - - 3 1 1
Engine Construction
3 - 3 1 - - 3 1 1
Engine Fuel Systems
3 - 3 1 - - 3 1 1
Carburettors
3 - 3 1 - - 3 1 -
Carburettors
3 - 3 1 - - 3 1 -
Fuel injection systems
3 - 3 1 - - 3 - 1
Engine controls
3 1 - - 3 1 - 1 3
FADEC 3 - 2 1 - - 2 1 -
Starting and Ignition Systems
3 - 3 1 - - 3 1 -
Induction, Exhaust and Cooling Systems
3 - 3 1 - - 3 1 -
Supercharging/Turbo charging
3 - 3 1 - - 3 1 -
SECTION 2 CAR 66
Rev 00 2-66 01 July 2011
Lubricants and Fuels
3 - 3 1 - - 3 1 -
Engine Indication Systems
3 - 3 1 - - 3 1 3
Power plant Installation
3 - 3 1 - - 3 1 -
Engine Monitoring and Ground Operation 3
3 - 3 1 - - 1 -
Engine Storage and Preservation 3
3 - 3 1 - - 1 -
Propellers:
Propeller -General
3 1 3 1 - - - - 1
Propeller Construction
3 1 3 1 - - - - -
Propeller Pitch Control
3 1 3 1 - - - - -
Propeller Synchronising
3 1 3 1 - - - - -
Propeller Electronic control
2 1 2 1 - - - - 3
Propeller Ice Protection 3 1 3 1 - - - - -
Propeller Maintenance
3 1 3 1 - - - - -
2.2. Practical element The practical training element must consist of the performance of representative maintenance tasks and their assessment, in order to meet the following objectives: (a) 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.
(b) Correctly use all technical literature and documentation for the aircraft. (c) 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.
3. Type training examination standard Where aircraft type training is required, the examination must be written and complies with the following: 1. Format of the examination is of the multiple-choice type. Each multiple-choice question
must have three alternative answers of which only one must be the correct answer. The time for answering is based upon a nominal average of 120 seconds per level 3 question and 75 seconds per level 1 or 2 questions.
2. The examination must 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.
SECTION 2 CAR 66
Rev 00 2-67 01 July 2011
3. The number of questions must be at least one question per hour of instruction subject
to a minimum of two questions per Syllabus subject. The Authority will assess number and level of questions on a sampling basis when approving the course.
4. The examination pass mark is 75 %. 5. Penalty marking is not to be used to determine whether a candidate has passed. 6. 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. 4. Type examination standard Where type training is not required, the examination must be oral, written or practical assessment based, or a combination thereof. Oral examination questions must be open. Written examination questions must be essay type or multiple-choice questions. Practical assessment must determine a person's competence to perform a task. Examination subjects must be on a sample of subjects drawn from paragraph 2 type training/examination syllabus, at the indicated level. The examination must ensure that the following objectives are met: (a) Properly discuss with confidence the aircraft and its systems. (b) 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.
(c) Correctly use all technical literature and documentation for the aircraft. (d) 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.
A written report must be made by the examiner to explain why the candidate has passed or failed.
SECTION 2 CAR 66
Rev 00 2-68 01 July 2011
APPENDIX IV
EXPERIENCE REQUIREMENTS FOR EXTENDING A CAR 66 AIRCRAFT MAINTENANCE LICENCE The table below shows the experience requirements for adding a new category or subcategory to an existing CAR 66 licence. The experience must be practical maintenance experience on operating aircraft in the subcategory relevant to the application. The experience requirement will be reduced by 50 % if the applicant has completed an approved CAR 147 course relevant to the subcategory.
To: From:
A1 A2 A3 A4 B1.1 B1.2 B1.3 B1.4 B2
A1 6 months
6 months 6 months 2 years 6 months 2 years 1 year 2 years
A2 6 months 6 months 6 months 2 years 6 months 2 years 1 year 2 years
A3 6 months 6 months
6 months 2 years 2 years 6 months 2 years
A4 6 months 6 months
2 years 2 years 6 months 2 years
B1.1 None 6 months
6 months 6 months 6 months 6 months 6 months 1 year
B1.2 6 months None 6 months 6 months 2 years 2 years 6 months 2 years
B1.3 6 months 6 months
None 6 months 6 months 6 months 6 months 1 year
B1.4 6 months 6 months
6 months None 2 years 6 months 2 years 2 years
B2 6 months 6 months
6 months 6 months 1 year 1 year 1 year 1 year
SECTION 2 CAR 66
Rev 00 2-69 01 July 2011
CAR 66 AIRCRAFT MAINTENANCE LICENCE
1. An example of the CAR 66 aircraft maintenance licence can be found on the following pages (Appendix V). 2. The document must be printed in the standardised form shown but may be reduced in size to accommodate its computer generation if desired. When the size is reduced care should be exercised to ensure sufficient space is available in those places where official seals/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 the CAR 66 aircraft maintenance licence. 3. The document shall be printed in the English. 4. Each licence holder must have a unique licence number based upon a UAE identifier and an alpha-numeric designator. 5. The document may have the pages in any order and need not have some or any divider lines as long as the information contained is positioned such that each page layout can clearly be identified with the format of the example CAR 66 aircraft maintenance licence contained herein. The aircraft type rating page need not be issued until the first type endorsement is included. 6. The document may be prepared by the GCAA or by any CAR 145 approved maintenance organisation in accordance with a procedure approved by the GCAA and contained in the CAR 145 maintenance organisation exposition except that in all cases the GCAA will issue the document. 7. The preparation of any variation to an existing CAR-66 aircraft maintenance licence may be carried out by the GCAA or by any CAR 145 approved maintenance organisation in accordance with a procedure approved by the GCAA and contained in the CAR-145 maintenance organisation exposition except that in all cases the GCAA will issue the document with the variation. 8. The CAR 66 aircraft maintenance licence once issued is required to be kept by the person to whom it applies in good condition and who shall remain accountable for ensuring that no unauthorised entries are made. 9. Failure to comply with paragraph 8 may invalidate the document and could lead to the holder not being permitted to hold any CAR 145 certification authorisation and may result in prosecution under UAE law. 10. With regard to the aircraft type rating page the GCAA may choose not to issue this page until the first aircraft type rating needs to be endorsed and will need to issue more than one aircraft type rating page when there are a number to be listed. 11. Notwithstanding 10 each page issued will be in this format and contain the specified information for that page. 12. If there are no limitations applicable, the LIMITATIONS page will be issued stating ‘No limitations’. 13. Where a pre-printed format is used, 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.
SECTION 2 CAR 66
Rev 00 2-70 01 July 2011
APPENDIX V
UNITED ARAB EMIRATES
CAR-66
AIRCRAFT MAINTENANCE ENGINEER LICENCE
AMEL-XXXXX Issuing Date Page 1 of 8
I. UNITED ARAB EMIRATES
GENERAL CIVIL AVIATION AUTHORITY
II. CAR 66 AIRCRAFT MAINTENANCE ENGINEER LICENCE
III. License No: AMEL – XXXXX «Photo» IV. Full Name: Full Name IVa. Date of Birth: DD MM YY IVb. Place of Birth: Place of Birth
V. Address of Holder:
VI. Nationality:
VII.
Signature of Holder
VIIIa This licence is issued in accordance with the provisions of U.A.E
Civil Aviation Regulations and with Annex I to the Convention on
International Civil Aviation signed on 7 December 1944.
IX. License valid until:
X. Signature of issuing
officer & issuing date.
for Director General
of GCAA
«IssuingDate»
XI. Stamp of General
Civil Aviation
Authority:
AMEL-XXXXX Issuing Date Page 2 of 8
VIII b. Conditions:
1) . This licence must be signed by the holder. 2) Endorsement of any (sub) categories on the
page(s) entitled CAR 66 (SUB) CATEGORIES only, does not permit the holder to issue a certificate of release to service for an aircraft.
3) . This license when endorsed with an aircraft type rating meets the intent of ICAO Annex 1.
4) The privileges of the holder of this license are prescribed by CAR 66 and the applicable requirements of CAR M and CAR 145.
5) This license remains valid until the date specified unless previously suspended or revoked.
6) The privileges of this license may not be exercised unless in the preceding two years period the holder has had either six months of maintenance experience in accordance with the privileges granted by the license, or met the provision for the issue of the appropriate privileges.
AMEL-XXXXX Issuing Date Page 3 of 8
XII a. CAR 66 (SUB) CATEGORIES
(Sub)Category Date
B1 - Aeroplanes Turbines
B1 – Helicopter Turbines
DD MM YY
DD MM YY
B2 - Avionics DD MM YY
(NO FURTHER ENTRIES ON THIS PAGE)
AMEL-XXXXX Issuing Date Page 4 of 8
SECTION 2 CAR 66
Rev 00 2-71 01 July 2011
XII b. CAR 66 AIRCRAFT TYPE OR GROUP RATINGS
A/C Type or Group Cat Date
Airbus A310 (GE CF6). B1.1 DD MM YY
Airbus A340 (RR RB 211
Trent 500).
B1.1 DD MM YY
Agusta A109 (Turbomeca
Arriel 1)
Airbus A 340 (RR RB 211
Trent 500).
B1.3
C
DD MM YY
DD MM YY
(NO FURTHER ENTRIES ON THIS PAGE)
AMEL-XXXXX Issuing Date Page 5 of 8
XIII CAR 66 LIMITATION
A/C Type or Group Cat Limitations
Avionics B2 6,7
Airbus A310 (GE CF6). B1.1 25,26
(NO FURTHER ENTRIES ON THIS PAGE)
Refer to limitation code on CAAP 28 (Latest issue)
AMEL-XXXXX Issuing Date Page 6 of 8
INTENTIONALLY LEFT BLANK
AMEL-XXXXX Issuing Date Page 7 of 8
XIVa. AMEL is issued
based on:
XIVb. Initial Issuing Date: DD MM YY
AMEL-XXXXX Issuing Date Page 8 of 8
SECTION 2 CAR 66
Rev 00 2-72 01 July 2011
ACCEPTABLE MEANS OF COMPLIANCE AMC 66.10 Application 1. Maintenance experience should be written up in a manner that the reader has a reasonable understanding of where, when and what maintenance constitutes the experience. A task by task account is not necessary but at the same time a bland statement “X years maintenance experience completed” is not acceptable. A log book of maintenance experience is desirable and the Authority may require such log book to be kept. It is acceptable to cross refer in the Form LAME 04 and/or any other assigned form to other documents containing information on maintenance. 2. Applicants claiming the maximum reduction in AMC 66.30(a) total experience based upon having successfully completed CAR 147.200 approved basic training should include the CAR 147 certificate of recognition for approved basic training. 3. Applicants claiming reduction in AMC 66.30(a) total experience based upon having successfully completed technical training in an organisation or institute recognised by the Authority as a competent organisation or institute, should include the relevant certificate of successful completion of training. AMC 66.20(a) Privileges The following definition of line and base maintenance should apply: Line maintenance is any maintenance that is carried out before flight to ensure that the aircraft is fit for the intended flight. It may include: - trouble shooting; - defect rectification; - component replacement with use of external test equipment if required. Component replacement may include components such as engines and propellers; - scheduled maintenance and/or checks including visual inspections that will detect obvious unsatisfactory conditions/discrepancies but do not require extensive in depth inspection. It may also include internal structure, systems and power plant items which are visible through quick opening access panels/doors; - minor repairs and modifications which do not require extensive disassembly and can be accomplished by simple means; - for temporary or occasional cases (airworthiness directives, hereinafter AD; service bulletins, hereinafter SB) the quality manager may accept base maintenance tasks to be performed by a line maintenance organisation provided all requirements are fulfilled. The GCAA will prescribe the conditions under which these tasks maybe performed. Maintenance tasks falling outside these criteria are considered to be base maintenance. Note: Aircraft maintained in accordance with "progressive" type programmes need to be individually assessed in relation to this paragraph. In principle, the decision to allow some "progressive" checks to be carried out is determined by the assessment that all tasks within the particular check can be carried out safely to the required standards at the designated line maintenance station.
SECTION 2 CAR 66
Rev 00 2-73 01 July 2011
AMC 66.20(b) 2 Privileges The 6 months maintenance experience in 2 years should be understood as consisting of two elements, duration and nature of the experience. The minimum to meet the requirements for these elements may vary depending on the size and complexity of the aircraft and type of operation and maintenance. 1. Duration: Within an approved maintenance organization: - 6 months continuous employment within the same organisation; or -6 months split up into different blocks, employed within the same or in different organisations. The 6 months period can be replaced by 100 days of maintenance experience in accordance with the privileges, whether they have been performed within an approved organisation or as independent certifying staff according to CAR M.801(b)2 or as a combination hereof. When certifying staff maintains and releases aircraft in accordance with CAR M.801 (b) 2, in certain circumstances this number of days may even be reduced by 50% when agreed in advance by the GCAA. These circumstances consider the cases where the holder of a CAR 66 licence happens to be the owner of an aircraft and carries out maintenance on his own aircraft, or where a licence holder maintains an aircraft operated for low utilization, that does not allow the licence holder to accumulate the required experience. This reduction should not be combined with the 20% reduction permitted when carrying out technical support, or maintenance planning, continuing airworthiness management or engineering activities. To avoid a too long period without experience, the working days should be spread over the intended 6 months period. 2. Nature of the experience: Depending on the category of the aircraft maintenance licence, the following activities are considered relevant for maintenance experience: - Servicing; - Inspection; - Operational and functional testing; - Trouble-shooting; - Repairing; - Modifying; - Changing component; - Supervising these activities; - Releasing aircraft to service. For category A certifying staff, the experience should include exercising the privileges, by means of performing tasks related to the authorization on at least one aircraft type for each licence subcategory. This means tasks as mentioned in AMC 145.30(g), including servicing, component changes and simple defect rectifications. For category B1 and B2, for every aircraft included in the authorization the experience should be on that particular aircraft or on a similar aircraft within the same licence subcategory. Two aircraft can be
SECTION 2 CAR 66
Rev 00 2-74 01 July 2011
considered as similar when they have similar technology, construction and comparable systems, which means equally equipped with the following (as applicable to the licence category): a) Propulsion systems (piston or turboprop or turbofan or turbo shaft or jet-engine or push propellers); and b) Flight control systems (only mechanical controls or hydro-mechanically powered controls or electro-mechanically powered controls); and c) Avionic systems (analog systems or digital systems); and d) Structure (manufactured of metal or composite or wood). As an alternative to the above: - In the case of B1 licence endorsed with group ratings (either manufacturer group or full group) as defined in CAR 66.45(g) the holder may show experience on at least one aircraft type per group and per aircraft structure (metal, composite, wood). - In the case of a B2 licence endorsed with group ratings (either manufacturer group or full group) as defined in CAR 66.45(g) the holder may show experience on at least one aircraft type per group. For category C, the experience should cover at least one of the aircraft types endorsed on the authorization. For a combination of categories, the experience should include some activities of the nature shown in paragraph 2 in each category. A maximum of 20% of the experience duration required may be replaced by the following relevant activities on an aircraft type of similar technology, construction and with comparable systems: - Aircraft maintenance related training as an instructor/assessor or as a student; - Maintenance technical support/engineering; - Maintenance management/planning. The experience should be documented in an individual log book or in any other recording system (which may be an automated one) containing the following data: a) Date; b) Aircraft type; c) Aircraft identification i.e. registration; d) ATA chapter; e) Operation performed i.e. 100 FH check, MLG wheel change, engine oil check and complement, SB embodiment, trouble shooting, structural repair, STC embodiment…; f) Type of maintenance i.e. base, line; g) Type of activity i.e. perform, supervise, release; h) Category used A, B1, B2 or C. Remark: this experience requirement does not apply to:
SECTION 2 CAR 66
Rev 00 2-75 01 July 2011
- Certifying staff issuing a certificate of release of aircraft as per CAR M.607 (b); - Pilot-owner certifying tasks according to CAR M.803; and - Certifying staff according to CAR 145.30(j) and Appendix IV of CAR 145. AMC 66.25 Basic knowledge requirements 1 For an applicant being a person qualified by holding an academic degree in a aeronautical, mechanical or electronic discipline from a recognised university or other higher educational institute the need for any examination will depend upon the course taken in relation to Appendix I to CAR 66 2 Knowledge gained and examinations passed during previous experiences, for example, in military aviation and civilian apprenticeships will be credited where the GCAA is satisfied that such knowledge and examinations are equivalent to that required by Appendix I to CAR 66. AMC 66.30(a) Experience requirements 1. For a category C applicant holding an academic degree the representative selection of tasks should include the observation of hangar maintenance, maintenance planning, quality assurance, record-keeping, approved spare parts control and engineering development. 2. While an applicant to a CAR 66 category C licence may be qualified by having 3 years experience as category B1 or B2 certifying staff only in line maintenance, it is however recommended that any applicant to a category C holding a B1 or B2 licence demonstrate at least 12 months experience as a B1 or B2 base maintenance support staff. 3. A skilled worker is a person who has successfully completed a course of training, acceptable to the GCAA, involving the manufacture, repair, overhaul or inspection of mechanical, electrical or electronic equipment. The training would include the use of tools and measuring devices. AMC 66.30(d) Experience requirements To be considered as recent experience; at least 50% of the required 12 month experience should be gained within the 12 month period prior to the date of application for the CAR 66 aircraft maintenance licence. The remainder of the experience should have been gained within the 7 year period prior to application. Experience should be supported by documentary evidence in the format as agreed by GCAA. AMC 66.30(e) Experience requirements 1. For category A the additional experience of civil aircraft maintenance should be a minimum of 6 months. For category B1 or B2 the additional experience of civil aircraft maintenance should be a minimum of 12 months. 2. Aircraft maintenance experience gained outside a civil aircraft maintenance environment can include aircraft maintenance experience gained in armed forces, coast guards, police etc. or in aircraft manufacturing. AMC 66.45(a) Type/task training and ratings 1 For category A certifying staff specific training on each aircraft type will be required reflecting the authorised task(s) as indicated under CAR 66.20 (a) 1.
SECTION 2 CAR 66
Rev 00 2-76 01 July 2011
2 Appropriately approved CAR 145 or CAR 147 organisation means compliance with the applicable paragraphs of AMC 66.45. AMC 66.45(d) Type/task training and ratings 1. The training should give adequate detailed theoretical knowledge of the aircraft, its main parts, systems, equipment, interior and applicable components, including training in the systems in use for technical manuals and maintenance procedures. The course should also take into account the following: (a) in service experience on the aircraft type; (b) feedback from in-service difficulties/occurrence reporting etc; (c) significant airworthiness directives and/or service bulletins; (d) known human factors issues associated with the particular aircraft type. 2. Theoretical training should be supported by training aids such as aircraft system components. Ground simulator time, engine ground running and computer based training (CBT) etc may also be utilised. 3. Theoretical and practical training should also take into account critical aspects of Fuel Tank Safety (FTS) airworthiness limitation items (ALI) including Critical Design Configuration Control Limitations (CDCCL). 4. Knowledge is also recommended of relevant inspections and limitations as applicable to the effects of environmental factors such as cold and hot climates, wind, moisture, etc. 5. The practical training should comprise a period of 4 months for applicants with no recent recorded previous practical experience of aircraft of comparable construction and systems, including the engines, but this can be reduced to a minimum of 4 weeks for applicant with such previous experience. 6. A programme of structured on-job-training (OJT) may be prepared to satisfy the practical training requirement. Where the practical training element is conducted by or under the responsibility of the training organisation under a CAR 147 approval, it should be considered as part of the approved course and as such, its acceptance by the GCAA should be supported by a detailed syllabus showing its content and duration. The individual practical training records should be designed in a manner that they demonstrate compliance with the detailed practical training syllabus. Such records may take the form of an individual training logbook. The logbook should be designed such that tasks may be countersigned by the CAR 147 school or other course provider. Where the practical training element is conducted by a maintenance organisation approved under CAR 145, under its own responsibility, its acceptance by the GCAA should be supported by a detailed syllabus showing its content and duration. The individual practical training records should be designed in a manner that they demonstrate compliance with the detailed practical training syllabus. Alternatively, the practical training element may consist of a structured OJT programme. In this case the maintenance organisation approved under CAR 145 should provide applicants for a type rating a logbook indicating a list of tasks to be performed under supervision. The logbook should be designed such that tasks may be countersigned by the supervisor. The list of tasks should be accepted directly for each individual – depending on the individual’s previous experience, or indirectly through the acceptance of a procedure giving delegation to the maintenance organisation. In all cases the practical element should include an acceptable cross
SECTION 2 CAR 66
Rev 00 2-77 01 July 2011
section of maintenance tasks, which, in the case of a structured OJT, can be tailored to accommodate the operating profile of the CAR 145 organisation whilst also supplementing the theoretical course elements. The means by which the practical element is supervised and the control of the standard should be acceptable to the GCAA. The duration of the practical type training element should take into account significant differences between types and be acceptable to the GCAA. These differences will require considerably more practical training for certifying staff who are not familiar with the new techniques and technologies. Some examples of differences may include, but are not limited to, the following elements: Fly by wire, glass cockpit avionics, significant structural differences, etc. 7. Before grant of the aircraft type, the applicant should be able to:
(a) demonstrate by knowledge examination a detailed understanding of applicable systems, their operation and maintenance; (b) 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 trouble shooting, repairs, adjustments, replacements, rigging and functional checks such as engine run, etc, if required; (c) correctly use all technical literature and documentation for the aircraft; (d) 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.
8. The practical assessment should also 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 trouble shooting, repairs, adjustments (rigging), replacements and functional/operational checks etc including engine operation (ground running) if required. AMC 66.45(e) Type/task training and ratings Category C certifying staff may not carry out the duties of category B1 or B2, or equivalent within base maintenance, unless they hold the relevant B1 or B2 category and have passed type training corresponding to the relevant B1 or B2 category. AMC 66.45(g) Type/task training and ratings 1. “Aircraft types representative of a group” means that:
- for the B1 category the aircraft type should include typical systems and engines relevant to the group (e.g. retractable undercarriage, pressurisation, variable pitch propeller, etc. for the single piston engine metal subgroup) and, - for the B2 category the aircraft type should include complex avionics systems such as radio coupled autopilot, EFIS (Electronic flight instrument system), flight guidance systems, etc .
2. A “multiple engines” group automatically includes the corresponding “single engine” group. AMC 66.45(h) Type/task training and ratings 1. Type experience should cover an acceptable cross section of tasks from Appendix II. For the first aircraft type of each manufacturer group, at least 50% of the Appendix II tasks, as applicable to the concerned aircraft type and licence category should be performed. For the second aircraft type of
SECTION 2 CAR 66
Rev 00 2-78 01 July 2011
each manufacturer group, this should be reduced to 30%. For subsequent aircraft types of each manufacturer group, this should be reduced to 20%. 2. Type experience should be demonstrated by the submission of acceptable schedule of works or logbook showing the Appendix II tasks performed by the applicant as specified by the GCAA. AMC 66.70 Conversion provisions Technical limitations will be deleted, as appropriate, when the person satisfactorily sits the relevant conversion examination and gains relevant experience.
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Rev 00 2-79 01 July 2011
APPENDIX I
AIRCRAFT TYPE RATINGS
FOR PART-66 AIRCRAFT MAINTENANCE LICENCE
The following aircraft type ratings will be used to ensure a common standard. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Basic Regulation at its Implementing Rules, this list being only intended for the purpose of maintenance. In the following table, the groups of aircraft are defined as follows:
List No. Aircraft:
1 Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating
2 Aeroplanes of 5700 kg and below, requiring type training and individual type rating (A-tr)
3 Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below, eligible for type examinations and manufacturer group ratings
4 Aeroplanes single turbine engine (ASTE) of 5700 kg and below, eligible for type examinations and group ratings
5 Aeroplanes multiple piston engines – metal structure (AMPE-MS), eligible for type examinations and group ratings
6 Aeroplanes single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings
7 Aeroplanes multiple piston engines – wooden structure (AMPE-WS),eligible for type examinations and group ratings
8 Aeroplanes single piston engine – wooden structure/metal tube-fabric (ASPE-WS), eligible for type examinations and group ratings
9 Aeroplanes multiple piston engines – composite structure (AMPE-CS),eligible for type examinations and group ratings
10 Aeroplanes single piston engine – composite structure (ASPE-CS), eligible for type examinations and group ratings
11 Multi-engine helicopters (MEH), requiring type training and individual type rating
12 Helicopters – single turbine engine (HSTE), eligible for type examinations and group ratings
13 Helicopters – single piston engine (HSPE), eligible for type examinations and group ratings
Column 1 includes the TC holder as defined in the TCDS (EASA, FAA or other). For aeroplanes of group 1 and 2 and helicopters, the Column 2 includes the aircraft models as defined in the relevant TCDS (EASA, FAA or other). The following column includes the ‘commercial designation’ when available. Column 3 includes the relevant individual type rating. Only the designations of the ratings in column 3 should be used for endorsing individual type ratings on CAR 66 licences. However, it is subjected that the aircraft type being listed in the UAE GCAA civil aircraft registry list. Note: Aircraft STC data are not included in this table.
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Rev 00 2-80 01 July 2011
1. Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating.
1. TC holder 2. Aeroplanes Model Commercial Designation
3. Type rating endorsement
AIRBUS SN 601 Corvette Aerospatiale SN-601 (PW JT15D)
A300 B1 A300 B2-1A A300 B2-1C A300 B2K-3C A300 B2-202 A300 B2-203 A300B4-2C A300B4-102 A300B4-103 A300B4-203 A300C4-203 A300F4-203
Airbus A300 basic model (GE CF6)
A300B2-320 A300B4-120 A300B4-220
Airbus A300 basic model (PW JT9D)
A300B4-601 A300B4-603 A300B4-605R A300F4-605R A300C4-605R variant F
Airbus A300-600 (GE CF6)
A300B4-622 A300B4-622R A300F4-622R
Airbus A300-600 (PW 4000)
A300B4-620 A300C4-620
Airbus A300-600 (PW JT9D)
A310-304 A310-308 A310-203 A310-221 A310-203C
Airbus A310 (GE CF6)
A310-324 A310-325 A310-322 A310-222 A310-204
Airbus A310 (PW 4000)
A318-120 series Airbus A318 (PW 6000)
A318-110 series A319-110 series A320-111 A320-210 series A321-110 series A321-210 series
Airbus A318/A319/A320/A321 (CFM56)
A319-130 series A320-230 series A321-130 series A321-230 series
Airbus A319/A320/A321 (V2500)
A330-200 series A330-300 series
Airbus A330 (GE CF6)
A330-220 series A330-320 series
Airbus A330 (PW 4000)
A330-240 series A330-340 series
Airbus A330 ( RR RB211 Trent 700)
A340-210 series A340-310 series
Airbus A340 (GE CFM56)
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Rev 00 2-81 01 July 2011
A340-540 series A340-640 series
Airbus A330 ( RR RB211 Trent 500)
A380-840 series Airbus A380 ( RR RB211 Trent 900)
A380-860 series Airbus A380 ( EA GP7200)
A300F4-608ST Beluga Airbus A330-600ST (GE CF6)
AIRCRAFT INDUSRIES
L-410 M/UVP L-410 UVP-E L-410 UVP-E9 L-410 UVP-E20 L-410 UVP-E20 CARGO L-410 UVP-E-LW L-410 UVP-LW
Turbolet Let L-410 (Walter M601)
L-420 Let L-420 (Walter M601)
ALENIA AERONAUTICA
C-27J Alenia C-27J (Allison/RR AE 2100)
ANTONOV AN-26 AN-26B
Antonov AN26 (Ivchenko AI-24)
ATR-GIE Avions de Transport Regional
ATR 42-200 ATR 42-300 ATR 42-320
ATR 42-200/300 series (PWC PW120)
ATR 72-101 ATR 72-102 ATR 72-201 ATR 72-202 ATR 72-221 ATR 72-212
ATR 72-100/200 series (PWC PW120)
ATR 42-400 ATR 42-500 ATR 42-500 ATR 72-212A ATR 72-212A
42-500 42-600 72-500 72-600
ATR 72-400/500/72-212A (PWC PW120)
BAE SYSTEMS BAe 146 series 100 BAe 146 series 200 BAe 146 series 300 AVRO 146-RJ70 AVRO 146-RJ85 AVRO 146-RJ100 AVRO 146-RJ115
BAe 146/AVRO 146-RJ (Honeywell ALF500 series)
HS.748 series 1 HS.748 series 2 HS.748 series 2A HS.748 series 2B
HS 748 (RRD Dart)
HP.137 Jetstream Mk.1 HP.137 Jetstream Mk.1
Jetstream 1 Jetstream 2
HP.137 (Turbomeca Astazou)
Jetstream 200 Jetstream 200 (Turbomeca Astazou)
Jetstream 3101 Jetstream 3201
Jetstream 31 Jetstream 32/32EP
Jetstream 31/32 (Honeywell TPE331)
Jetstream 4100 Jetstream 4101
Jetstream 41 (Honeywell TPE331)
BAe ATP ATP (PWC PW 120)
THE BOEING COMPANY
B707-100 B707-100B B707-100B B707-300B series B707-300C series B720 B720B
Long Body Long Body Short Body
Boeing 707/720 (PW JT3D)
B707-200 B707-200B
Boeing 707 (PW JT4)
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Rev 00 2-82 01 July 2011
B707-300 series
B707-400 series Boeing 707 (RR Conway)
B727 series B727-100 series B727C series
Boeing 727 (PW JT8D)
B727-100C series B727-200 series
Boeing 727 (PW JT8D)
B737-100 B737-200 B737-200C
Boeing 737-100/200 (PW JT8D)
B737-300 B737-400 B737-500
Boeing 737-300/400/500 (CFM56)
B737-600 B737-700 B737-800 B737-900 B737-900ER
Boeing 737-600/700/800/900 (CFM56)
B747-100B Boeing 747-100 (RR RB211)
B747-400 B747-400F/SF(BCF) B747-100B SUD
Boeing 747-100 (PW JT9D)
B747-200B B747-200C B747-200F B747-300
Boeing 747-200/300 (GE CF6)
B747-200B B747-200F B747-200C
Boeing 747-200/300 (PW JT9D)
B747SP Boeing 747SP (PW JT9D)
B747-300 Boeing 747-200/300 (PW JT9D)
B747-200B B747-200F B747-200C
Boeing 747-200/300 (RR RB211)
B747SP Boeing 747SP (RR RB211)
B747-300 Boeing 747-200/300 (RR RB211)
B747-400 B747-400D B747-400F/SF(BCF)
Boeing 747-400 (GE CF6)
B747-400 B747-400F/SF(BCF)
Boeing 747-400 (PW 4000)
B747-400 B747-400F/SF(BCF)
Boeing 747-400 (RR RB211)
B747-81 B747-8F
Intercontinental Freighter
Boeing 747-8 (GE GEnx)
B757-200C B757-200PF B757-300
Boeing 757-200/300 (PW 2000)
B757-200C B757-200PF B757-30 B777-20
Boeing 757-200/300 (RR RB211)
B767-200 B767-300
Boeing 767-200/300 (PW 4000)
B767-200 B767-300
Boeing 767-200/300 (PW JT9D)
B767-300 Boeing 767-300 (RR RB211)
B767-200 B767-300 B767-300F B767-400ER
Boeing 767-200/300/400 (GE CF6)
B777-200
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Rev 00 2-83 01 July 2011
B777-200LR B777-200ER B777F
Freighter
Boeing 777-200/300 (GE 90)
B777-200 B777-300
Boeing 777-200/300 (PW 4000)
B777-200 B777-300
Boeing 777-200/300 (RR RB211 Trent 800)
B787-8 Dreamliner Boeing 787-8 (RR RB211 Trent 1000)
B777-8 Dreamliner Boeing 787-8 (GEnx)
BOMBARDIER CL-215-1A10 Canadair CL-215 (PW R2800)
CL-216-6B11 (CL-215T Variant)
Canadair CL-215 (PWC PW120)
CL-216-6B11 (CL-415 Variant)
Canadair CL-415 (PWC PW123)
BD-100-1A10 Challenger 300 Bombardier BD-100-1A10 (Honeywell AS907)
BD-700-1A10 BD-700-1A11
Global Express Global 5000
Bombardier BD-700 series (RRD BR710)
CL600-1A11 Challenger 600 Bombardier CL-600-1A11 (Honeywell ALF502)
CL-600-2A12 (601 Variant) CL-600-2B16 (601-3A Variant) CL-600-2B16 (601-3R Variant)
Challenger 601 Challenger 601-3A Challenger 601-3R
Bombardier CL-600-2A12/-2B16 (Variant CL 601/601-3A/3R)(GE CF34)
CL-600-2B16 (CL 604 Variant) CL-600-2B16 (CL 604 Variant)
Challenger- 604 (MSN <5701) Challenger 604 (MSN >5701)
Bombardier CL-600-2B16 (Variant CL 604)(GE CF34)
CL-600-2B19 Regional Jet Series 100 Bombardier CL-600-2B19 (GE CF34)
CL-600-2C10 CL-600-2D15 CL-600-2D24 CL-600-2E25
Regional Jet Series 700/701/702 Regional Jet Series 705 Regional Jet Series 900 Regional Jet Series 1000
Bombardier CL-600-2C10/-2D15/-2D24/-2E25 (GE CF34)
DHC-8-101 DHC-8-102 DHC-8-103 DHC-8-106 DHC-8-201 DHC-8-202 DHC-8-301 DHC-8-311 DHC-8-314 DHC-8-315
DHC-8 series 100 DHC-8 series 100 DHC-8 series 100 DHC-8 series 100 DHC-8 series 200 DHC-8 series 200 DHC-8 series 300 DHC-8 series 300 DHC-8 series 300 DHC-8 series 300
Bombardier DHC-8-100/200/300 (PWC PW 120)
DHC-8-400 DHC-8-401 DHC-8-402
DHC-8 series 400 DHC-8 series 400 DHC-8 series 400
Bombardier DHC-8-400 (PWC PW 150)
SHORT BROTHERS PLC
SD3-30 SD3-60 SD3-SHERPA SD3-60 SHERPA
Variant 200 Variant 200 Variant 200 Variant 200
Shorts SD3 series -30/SD3-60 (PWC PT6)
EADS CASA C-212-CB C-212-CC C-212-CD C-212-CE C-212-CF C-212-DD C-212-DF C-212-EE
Aviocar Aviocar Aviocar Aviocar Aviocar Aviocar Aviocar Aviocar
CASA C212 (Honeywell TPE331)
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Rev 00 2-84 01 July 2011
C-212-VA Aviocar
C-212-DE Aviocar CASA C-212 (PWC PT6)
CN-235 CASA CN-235 (GE CT7)
CN-235-100 CN-235-200 CN-235-300
CASA CN-235 (GE CT7)
C-295 CASA C-295 (PWC PW127)
CESSNA AIRCRAFT Company
525B 525C
Citation Jet CJ3 Citation Jet CJ4
Cessna 525B/C (William FJ 44)
550 560 560
Citation Bravo Citation Encore Citation Encore +
Cessna 550/560 (PWC PW530/535)
550 S550 560 560
Citation II Citation S/II Citation V Citation Ultra
Cessna 550/560 (PWC JT15D)
560XL 560XLS 560XLS+
Citation Excel Citation XLS Citation XLS+
Cessna 560XL/XLS (PWC PW545)
650 650
Citation III-IV Citation VII
Cessna 650 (Honeywell TFE731)
680 Sovereign Cessna 680 (PWC PW306)
750 Citation X Cessna 750 (RR Corp AE3007C)
DASSAULT AVIATION
Falcon 10 Falcon 10 (Honeywell TFE731)
Fan Jet Falcon (Basic) Fan Jet Falcon Falcon 20 (GE CF700)
Fan Falcon Jet Series C Fan Falcon Jet Series D Fan Falcon Jet Series E Fan Falcon Jet Series F
Mystere Falcon 20-C5 Mystere Falcon 20-D5 Mystere Falcon 20-E5 Mystere Falcon 20-F5
Falcon 20-5 (Honeywell TFE731)
Fan Jet Falcon Series G Mystere Falcon 200 Mystere Falcon 20GF
Falcon 200 (Honeywell ATF 3-6)
Mystere Falcon 50 Falcon 50 (Honeywell TFE731)
Mystere Falcon 50 F50EX Falcon 50 (Honeywell TFE731)
Mystere Falcon 900 Mystere Falcon 900
F900B
Falcon 900 (Honeywell TFE731)
Mystere Falcon 900 F900C Falcon 900C (Honeywell TFE731)
Falcon 900EX Falcon 900EX (Honeywell TFE731)
Falcon 900EX Falcon 900EX Falcon 900EX
F900EX EASy F900D F900LX
Falcon 900EX EASy (Honeywell TFE731)
Falcon 2000 Falcon 2000 (CFE 738)
Falcon 2000EX Falcon 2000EX (PWC PW308)
Falcon 2000EX Falcon 2000EX Falcon 2000EX
Falcon 2000EX EASy (PWC PW308)
Falcon 7X Falcon 7X (PWC PW307A)
RUAG Aerospace GmbH (DORNIER)
228-100 series 228-200 series
Dornier 228 (Honeywell TPE331)
328-100 series 328-200 series
Dornier 328-100 (PWC PW119) Dornier 328-200 (PWC PW306)
EMBRAER EMB-120 EMB-120RT EMB-120ER EMB-120FC EMB-120QC
Brasilia Brasilia Brasilia Brasilia Brasilia
Embraer EMB-120 (PWC PW110 series)
EMB-135ER
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Rev 00 2-85 01 July 2011
EMB-135LR EMB-135BJ EMB-145 EMB-145ER EMB-145EU EMB-145EP EMB-145LR EMB-145LU EMB-145MP EMB-145MK
Legacy 600 Legacy 650
Embraer EMB-135/145 (RR Corp AE3007A)
ERJ-170-100 STD ERJ-170-100 LR ERJ-170-200 STD ERJ-170-200 LR ERJ-190-100 STD ERJ-190-100 LR ERJ-190-100 SR ERJ-190-100 IGW ERJ-190-100 ECJ ERJ-190-200 STD ERJ-190-200 LR ERJ-190-200 IGW
ERJ-170 ERJ-170 ERJ-175 ERJ-175 ERJ-190 ERJ-190 ERJ-190 ERJ-190AR Lineage 1000 ERJ-195 ERJ-195 ERJ-195AR
Embraer ERJ-170/190 (GE CF34)
EMB-505 Phenom 300 Embraer EMB-505 (PWC PW535)
(FOKKER –FAIRCHILD) MARYLAND AIR INDUSTRIES
F-27A to –M FH-227 FH-227B FH-227C FH-227D FH-227E
Fokker F27/ Fairchild F-27/FH-227 (RRD Dart) FOKKER
SERVICES F27 Mark 100 F27 Mark 200 F27 Mark 300 F27 Mark 400 F27 Mark 500 F27 Mark 600 F27 Mark 700
Friendship Friendship Friendship Friendship Friendship Friendship Friendship
F27 Mark 050 F27 Mark 0502 F27 Mark 0604
Fokker 50 Fokker 50 Fokker 60
Fokker 50/60 Series (PWC PW 125/1270
F28 Mark 1000 F28 Mark 1000C F28 Mark 2000 F28 Mark 3000 F28 Mark 3000C F28 Mark 3000R F28 Mark 3000RC
Fellowship Fellowship Fellowship Fellowship Fellowship Fellowship Fellowship
Fokker F28 Series (RRD Spey)
F28 Mark 4000 Fellowship Fokker F28 Series (RRD Spey)
F28 Mark 0I00 F28 Mark 0070
Fokker 100 Fokker 70
Fokker 70/100 (RRD Tay)
GULFSTREAM AEROSPACE LP (GALP) c/o Israel Aircraft Industries
1125 West wind Astra Astra SPX G100
Gulfstream 100
Gulfstream (IAI) 100/1125/Astra SPX (Honeywell TFE731)
Gulfstream G150 Gulfstream 150 Gulfstream (IAI) G150 (Honeywell TFE731)
Gulfstream 200/Galaxy
Galaxy 200 Gulfstream (IAI) 200/Galaxy (PWC PW 306)
GULFSTREAM AEROSPACE Corporation
G-159 Gulfstream I Gulfstream G-159 (RRD Dart)
G-1159 G-1159A G-1159B
Gulfstream II Gulfstream IIB Gulfstream III
Gulfstream G-1159 Series (RRD Spey)
G-IV/GIV-SP Gulfstream GIV/GIV-SP Gulfstream GIV Series (RRD RRD Tay)
SECTION 2 CAR 66
Rev 00 2-86 01 July 2011
GIV (300) GIV (G400)
Gulfstream G300 Gulfstream G400
GIV-X (G450) GIV-X (G350)
Gulfstream G450 Gulfstream G350
Gulfstream GIV-X Series (RRD Tay)
GV Gulfstream GV Gulfstream GV basic model (RRD BR710)
GV-SP (G550) GV-SP(500)
Gulfstream G550 Gulfstream G500
Gulfstream GV-SP Series (RRD BR710)
HAWKER BEECHCRAFT Corporation
HS.125 Series 700 HS.125 Series 800 Hawker 800 DH.125 Series 1 DH.125 Series 3 HS.125 Series 3 HS.125 Series F3 BH.125 Series 400 DH.125 Series 400 HS.125 Series F400 BH.125 Series 600 HS.125 Series 600 HS.125 Series F600
Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Beechcraft Hawker Hawker Siddeley Hawker Siddeley Beechcraft Hawker Hawker Siddeley Hawker Siddeley
BAe 125 Series /700/800 (Honeywell TFE731)
Hawker 750 Hawker 800XP Hawker 850XP Hawker 900XP
Hawker 750 Hawker 800XP Hawker 850XP Hawker 900XP
BAe 125 Series 750/800XP/850XP/900XP (Honeywell TFE731)
DH.125 Series 1 HS.125 Series 1 DH.125 Series 3 HS.125 Series 3 HS.125 Series F3 DH.125 Series 400 HS.125 Series 400 BH.125 Series 400 HS.125 Series F400 BH.125 Series 600 HS.125 Series 600 HS.125 Series F600
Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Hawker Siddeley Beechcraft Hawker Hawker Siddeley Beechcraft Hawker Hawker Siddeley Hawker Siddeley
BAe 125 Series (RRD Viper)
BAe.125 series 1000A/B Hawker 1000
BAe 125 Series 1000 (PWC PW305)
300 300LW B300 B300C
Super King Air Super King Air Super King Air 350 Super King Air 350C
Beech 300 Series (PWC PT6)
400 400A MU-300 MU-300-10
Beechjet Beechjet (Hawker 400XP) Diamond I/IA Diamond II
Beech 400/ Mitsubishi MU-300 (PWC JT15)
1900 1900C 1900D
Airliner Airliner Airliner
Beech 1900 (PWC PT6)
4000 Hawker 4000 Hawker 4000 (PWC PW308)
ISRAEL AIRCRAFT INDUSTRIES
IAI 1121 IAI 1121A IAI 1121B IAI 1123
Jetcommander Jetcommander Jetcommander Commodore Jet
IAI 1121/1123 (GE CJ610)F
IAI 1124 IAI 1124A
Westwind Westwind
IAI 1124 (Honey TFE731)
SECTION 2 CAR 66
Rev 00 2-87 01 July 2011
KELOWNA (Convair)
440 Convair 580 (RR Corp 501)
LEARJET 24/24A 24B/24B-A 24C 24D/24D-A 24E 24F/24F-A 25 25A 25B 25C 25D 25F
Learjet 24/25 (GE CJ610)
28 29
Learjet 28/29 (GE CJ 610)
31/31A Learjet 31 (Honeywell TFE731)
35/25A 36/36A
Learjet 35/36 (Honeywell TFE731)
Learjet 45 Learjet 40
LJ45 LJ45
Learjet Model 45 (Honeywell TFE731)
55/55B/55C Learjet 55 (Honeywell TFE731)
Learjet 60 Upgraded Learjet 60
LJ60 LJ60XR
Learjet 60 (PWC PW305)
LOCKHEED MARTIN Corporation
1329-25 JetStar II Lockheed 1329 (Honeywell TFE731)
1329-23A 1329-23D 1329-23E
JetStar JetStar (-8 version)
Lockheed 1329 (PWC JT12)
Model 188C Model L-188
Electra Electra
Lockheed 188 (RR Corp 501)
382 382B 382E 382F 382G
Hercules Hercules Hercules Hercules Hercules
Lockheed 382 (RR Corp 501)
382J Hercules II Lockheed 382 (RR AE2100)
L-1011-385-1 L-1011-385-1-14 L-1011-385-1-1-15 L-1011-385-3
TriStar TriStar TriStar TriStar
Lockheed L-1011 (RR RB211)
McDONNELL DOUGLAS Corporation
DC-8 Series 70 DC-8 Series 70F
DC-8 (CFM56)
DC-8 Series 50 DC-8F DC-8 Series 60 DC-8 Series 60F
DC-8 (PW JT3D)
DC-8 Series 40 DC-8 (RR Conway)
DC-9-10 Series DC-9-20 Series DC-9-30 Series DC-9-40 Series DC-9-50 Series
DC-9 (PW JT8D)
DC-9-81 (MD-81) Series DC-9-82 (MD-82) Series DC-9-83 (MD-83) Series DC-9-87 (MD-87) Series MD-88
MD-80 Series (PW JT8D)
SECTION 2 CAR 66
Rev 00 2-88 01 July 2011
MD-90 Series MD-90 (IAE V2500)
717-200 MD 717-200 (RRD BR700-715)
DC-10-10 DC-10-30 DC-10-30F
DC-10/MD-10 (GE CF6)
MD-11 MD-11F
MD-11 (GE CF6)
MD-11 MD-11 (PW 4000)
M7 AEROSPACE
SA227-AT SA227-TT SA227-CC SA227-DC SA227-AC SA227-BC
Swearingen Metro Swearingen Metro
Fairchild SA227 Series (Honeywell TPE331)
SA227-PC Swearingen Metro Fairchild SA227 Series (PWC PT6)
POLSKIE ZAKLADY LOTNICZE
PZL M28 00 PZL M28 02 PZL M28 05
PZL M 28 (PWC PT6)
SABRELINER Corporation
NA-265-65 Sabreliner NA-265 (Honeywell TFE731)
NA-265-65 Sabreliner NA-265 (PW TJ12)
SAAB AB, SAAB Aerosystems
340A (SF340) 340B
Saab-Fairchild 340A Saab (SF) 340 (GE CT7)
2000 Saab 2000 (RR Corp AE2100)
TUPOLEV PSC TU 204-120CE Tupolev TU 204 (RR RB211)
VIKING AIR DHC-7-100 DHC-7-101 DHC-7-102 DHC-7-103 DHC-7-110 DHC-7-111
De Havilland DHC-7 (PWC PT6)
SECTION 2 CAR 66
Rev 00 2-89 01 July 2011
2. Aeroplanes of 5700kg and below, requiring type training and individual type rating (A-tr).
1 TC Holder 2 Aeroplanes Model
Commercial Designation
3 Type rating endorsement
AERO VODOCHODY
Ae 270 Aero Ae-270 (PWC PT6)
AIRCRAFT INDUSTRIES
L-410m L-410 UVP L-410 UVP-LW L-410 UVP-FG L-410 UVP-E-LW
Turbolet Turbolet
Let L-410 LW (Walter-M601)
CESSNA AIRCRAFT Company
425 Corsair/Conquest I Cessna 425 (PWC PT6)
441 Cessna 441 (Honeywell TPE331)
500 Citation/Citation I Cessna 500/501/551 (PWC JT15D)
501 551
Citation Citation II
Cessna 500/501/551 (PWC JT15D) Cessna 500/501/551 (PWC JT15D)
510 Cessna 510 (PWC PW615)
525 525A
Citation Jet CJI Citation Jet CJ2
Cessna 525/525A (William FJ 44)
DORNIER Seastar
Seastar CD2 Dornier Seastar CD2 (PWC PT6)
ECLIPSE AEROSPACE Inc.
EA500 Eclipse EA500 (PWC PW610)
EMBRAER Empresa Brasileira de Aeronautica
EMB-110P1 EMB-110P2
Bandeirante Bandeirante
Embraer EMB-110 (PWC PT6)
EMB-121A EMB-121A1 EMB-121V
Xingu I Xingu II Xingu III
Embraer EMB-121 (PWC PT6)
EMB-500 Phenom 100 Embraer EMB-500 (PWC PW617)
HAWKER BEECHCRAFT Corporation
65-90 65-A90 65-A90-1 65-A90-4 65-A90-2 B90 C90 C90A C90GT C90GTi E90 F90 H90
King Air King Air King Air King Air King Air King Air King Air King Air King Air King Air King Air King Air King Air
Beech 90 Series (PWC PT6)
200/A200 200C/A200C 200CT/A200CT 200T B200 B200C B200CT B200T B200GT B200CGT
Beech 200 Series (PWC PT6)
SECTION 2 CAR 66
Rev 00 2-90 01 July 2011
99 99A A99 A99A B99 C99 100 A100 A100A/C
Airliner Airliner Airliner Airliner King Air King Air King Air
Beech 99/100 Series (PWC PT6)
B100 Beech B100 (Honeywell TPE331)
390 Premier 1, 1A Beech 390 (Williams FJ44)
ISRAEL AIRCRAFT Industries
Arava 101B Arava 101B (PWC PT6)
LEARJET LJ23 Learjet 23 (GE CJ610)
M7 AEROSPACE
SA226-T SA226-TC SA226-AT SA226-T(B)
Fairchild SA226 (Honeywell)
MITSUBISHI Heavy Industries
MU-2B MU-2B-10 MU-2B-20 MU-2B-25 MU-2B-30 MU-2B-35 MU-2B-40 MU-2B-36 MU-2B-60
Mitsubishi MU-2B (Honeywell TPE331)
PIAGGIO Aero Industries
P.166 DP1 Piaggio P166 (PWC PT6)
P180 Avanti Piaggio P 188 Avanti/Avanti II (PWC PT6) P180 Avanti II
PILATUS AIRCRAFT
PC-12 PC-12/45 PC-12/47 PC-12/47E
Pilatus PC-12 (PWC PT6)
PIPER AIRCRAFT
PA-42-1000 Cheyenne 400LS Piper PA-42 (Honeywell TPE331)
PA-42 PA-42-720 PA-42-720R
Cheyenne III Cheyenne IIIA Cheyenne IIIA
Piper PA-42 (PWC PT6)
PA-46-500TP Malibu Meridian Piper PA -46-500TP (PWC PT6)
REIMS AVIATION
F 406 Caravan II Reims-Cessna F 406 (PWC PT6)
SOCATA TBM 700A TBM 700B TBM 700C1 TBM 700C2
Socata TBM 700/850 (PWC PT6)
TBM 700N TBM 850
TWIN COMMANDER AIRCRAFT Corporation
680-T 680-V 680-W 681 690 690A 690B
Twin Commander-680/681/690/695 Series (Honeywell TPE331)
SECTION 2 CAR 66
Rev 00 2-91 01 July 2011
690C 690D 695 695A 695B
VIKING AIR (Bombardier) (De Havilland)
DHC-6-1 DHC-6-100/110 DHC-6-200/210 DHC-6-300/310/320 DHC-6-400
Twin Otter Twin Otter Twin Otter Twin Otter Twin Otter
De Havilland DHC-6 (PWC PT6)
VULCANAIR AP68TP300 AP68TP600
Spartacus Viator
Vulcanair AP68TP Series (RR Corp 250)
SF600 SF600A
Vulcanair SF600 (RR Corp 250)
SECTION 2 CAR 66
Rev 00 2-92 01 July 2011
3. Aeroplanes multiple turbine engines (AMTE) of 5700kg and below, eligible for type examinations and group ratings.
TC holder Type rating endorsement
GOVERNMENT AIRCRAFT FACTORIES (ASTA)
Nomad N24A (RR Corp 250)
B-N GROUP Ltd. (Britten-Norman)
Britten-Norman BN2T Series (RR Corp 250)
RUAG Aerospace Services GmbH Dornier Do 28 Series –(PWC PT6)
DORNIER Dornier Do 28 (Walter M601)
M7 AEROSPACE (Fairchild-Swearingen Corp)
Fairchild SA26-T (PW PT6)
Fairchild SA26-AT (Honeywell TPE331)
PIPER AIRCRAFT Corporation Piper PA-31T Series (PWC PT6)
SHORT BROTHERS Shorts SC7 (Honeywell TPE331)
SECTION 2 CAR 66
Rev 00 2-93 01 July 2011
4. Aeroplanes single turbine engine (ASTE) of 5700kg and below, eligible for type examinations and group ratings.
TC holder Type rating endorsement
AIR TRACTOR Air Tractor AT-302 (Lycoming LTP-101)
Air Tractor AT-400/500/600/800 Series (PWC PT6)
ZLIN AIRCRAFT Zlin Z-37 T Series (Walter M601)
ALENIA AERMACCHI Aermacchi SF260 (RR Corp 250)
ALLIED AG CAT Productions
Grumman G-164 (PWC PT6)
CESSNA AIRCRAFT Company Cessna (Soloy) 206/207 (RR Corp 250)
Cessna 208 Series (PWC PT6)
Cessna 210 (RR Corp 250)
EADS PZL "WARSZAWA-OKECIE" EADS PZL PZL-106 BT (Walter M601)
EADS PZL PZL-1061 BTU (PWC PT6)
EXTRA Flugzeugproduktions- und Vertiebs GmbH
Extra EA-400-500 (RR Corp 250)
GROB Luft- und Raumfahrt Grob G 520 Series (Honeywell TPE331)
MAULE AEROSPACE TECHNOLOGY Maule MX-7 (RR Corp 250)
PACIFIC AEROSPACE Corporation PAC 750XL (PWC PT6)
PILATUS AIRCRAFT Pilatus PC-6 Series (PWC PT6)
Pilatus PC-6 Series (Turbomeca Astazou)
Pilatus PC-6 Series (Honeywell TPE 331)
THRUSH AIRCRAFT Ayres S2R-Series (PWC PT6)
VIKING AIR (Bombardier) (De Havilland)
DeHavilland DHC-2 (PWC PT6)
SECTION 2 CAR 66
Rev 00 2-94 01 July 2011
5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible to type examinations and group ratings.
TC holder Type rating endorsement
AEROSTAR AIRCRAFT Corporation Piper PA-60/61 Series (Lycoming)
AIRCRAFT INDUSTRIES Let L 200 (LOM)
B-N Group (Britten- Norman) Britten-Norman BN2 (Lycoming) Britten-Norman BN2A Series (Lycoming) Britten-Norman BN2B Series (Lycoming)
CESSNA AIRCRAFT Company/ REIMS AVIATION
Cessna 310/320nSeries (Continental) Cessna 335 (Continental) Cessna 336 (Continental) Cessna/Reims-Cessna 337 Series (Continental) (not pressurised) Cessna /Reims-Cessna 337 Series (Continental) (pressurised) Cessna 340 (Continental) Cessna 401/402 (Continental) Cessna 404 (Continental) Cessna 411 (Continental) Cessna 414 (Continental) Cessna 421 (Continental) Cessna T303 (Continental)
GENERAL AVIA Costruzioni Aeronautiche
General Avia F20 Series (Lycoming)
HAWKER BEECHCRAFT Corporation
Beech 50 Series (Lycoming) Beech 55 Series (Continental) Beech 56 Series (Lycoming) Beech 58 Series (Continental) Beech 58P Series (Continental) Beech 58TC Series (Continental) Beech 60 Series (Lycoming) Beech 65-80 Series (Lycoming) Beech 76 Series (Lycoming) Beech 95 Series (Lycoming)
OMA SUD SPA Sky Technologies SKYCAR (Lycoming)
PIAGGIO Aero Industries
Piaggio P166 (Lycoming)
PIPER AIRCRAFT Piper PA-23 Aztec (Lycoming) Piper PA-30 Series (Lycoming) Piper PA-31 Series (Lycoming) Piper PA-31P (Lycoming) Piper PA-34 Series (Lycoming) Piper PA-34 Series (Continental) Piper PA-39/40 Series (Lycoming) Piper PA-44 Series (Lycoming)
PZL MIELEC PZL-M20 (PZL)
RUAG Aerospace Services GmbH Do 28 Series (Lycoming)
SOCATA Grumman GA-7 (Lycoming)
STOL AIRCRAFT Corporation Republic UC-1 (Lycoming)
TECNAM Costruzioni Aeronautiche
Tecnam P2006T (Rotax)
TWIN COMMANDER AIRCRAFT Corporation
Commander 685 (Continental) Commander 500 Series/680 Series (Lycoming) Rockwell 700 (Lycoming)
SECTION 2 CAR 66
Rev 00 2-95 01 July 2011
VULCANAIR Vulcanair P.68 Series (Lycoming) Vulcanair F600A (Lycoming)
SECTION 2 CAR 66
Rev 00 2-96 01 July 2011
6. Aeroplane single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings.
TC Holder Type rating endorsement
AERO Sp.z.o.o Aero AT-3 (Rotax)
AIRCRAFT INDUSTRIES Let Z-37 Series (LOM)
AIR TRACTOR Air Tractor AT-250/300 (PW R985) Air Tractor AT-301/401/501 (PW R1340) Air Tractor AT-401 (PZL-3S)
Air Transport Group Holdings, Inc Lake C/LA Series (Lycoming)
ALENIA AERMACCHI Aermacchi AL60 (Continental) Aermacchi Al60 (Lycoming) SIAI-Marchetti S.205/S.208 (Lycoming) SIAI-Marchetti S.205 (Franklin) Aermacchi SF260 Series (Lycoming)
ALLIED AG CAT Productions
Grumman G-164 (Continental) Grumman G-164 (Jacobs) Grumman G-164 (PW R Series)
APEX Aircraft CEAPR
Robin HR 100 series (Lycoming) Robin HR 100 series (Continental) Robin R 1180 series (Lycoming) Robin R 3000 series (Lycoming)
ALPHA AVIATION (APEX Aircraft) Robin HR 200/ R 2000 series (Lycoming)
ARV Aviation ARV 1 Super 2 (Hewland)
BÖLKOW Bölkow BO 208 (Continental) Bölkow BO 209 (Lycoming)
COMMANDER PREMIER AIRCRAFT CO. Commander 112 (Lycoming) Commander 114 (Lycoming)
DE HAVILLAND Support
Beagle B.121 series 1 (Continental) Beagle B.121 series 2/3 (Lycoming)
DYNAC AEROSPACE Corporation Aerocommander 100 (Lycoming)
CESSNA AIRCRAFT Company/ REIMS AVIATION
Cessna 150 Series (Rotax) Cessna/Reims-Cessna 150/F150 Series (continental) Cessna/Reims-Cessna 152/F152 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (continental) Cessna 172 Series (Thielet) Cessna 175 Series (Lycoming) Cessna 175 Series (Continental) Cessna 177 Series (Lycoming) Cessna 180 Series (Continental) Cessna/Reims-Cessna 182/F182 Series (Lycoming) Cessna/Reims-Cessna 182/F182 Series (continental Cessna/Reims-Cessna 182/F182 Series (SMA) Cessna 185 Series (continental) Cessna 188 Series (continental) Cessna 206 Series (continental) Cessna 206 Series (Lycoming) Cessna 207 Series (continental) Cessna 210 Series (continental)
EVEKTOR Evektor EV-97 (Rotax)
FFA ALTENRHEIN AS202 Series (Lycoming)
FLS AEROSPACE OA7 Optica Series (Lycoming) Club Sprint/Sprint 160 (Lycoming)
SECTION 2 CAR 66
Rev 00 2-97 01 July 2011
FUJI eavy Industries Fuji FA-200 Series (Lycoming)
GARDAN Gardan GY 80 (Lycoming)
GENERAL AVIA Contruzioni Aeronautiche General Avia F.22 (Lycoming)
GIPPSLAND Aeronautics Gippsland GA8 (Lycoming)
HAWKER BEECHCRAFT Corporation Beech 23 Series (Lycoming) Beech A23 (Continental) Beech 24 Series (Lycoming) Beech 33 Series (Continental) Beech 35 Series (Continental) Beech 36 Series (Continental) Beech 77 (Lycoming)
S.C. Constructii Aeronautice S.A IAR-46 (Rotax)
INTERCEPTOR AIRCRAFT Corporation Aerocommander 200 (Continental)
LAVIA ARGENTINA S.A (LAVIASA) Piper PA-25 Series (Lycoming)
MAULE AEROSPACE TECHNOLOGY Maule M4 (Continental) Maule M4 (Franklin) Maule M5 (Lycoming) Maule M5 (Franklin) Maule M5 (Continental) Maule M6 (Lycoming) Maule M7 Series (Lycoming) Maule MX-7 (Lycoming)
METEOR Meteor FL53 (Continental) Meteor FL54 (Continental) Meteor FL55 (Lycoming)
MOONEY AIRPLANE Conpany Mooney M20B to M20S/M22 (Lycoming) Mooney M20 (Continental)
PILATUS AIRCRAFT Pilatus PC-6 Series (Lycoming)
PIPER AIRCRAFT Piper PA-24 Series (Lycoming) Piper PA-28 Series (Lycoming) Piper PA-28 Series (Continental) Piper PA-28 Series (Thielert) Piper PA-32 Series (Lycoming) Piper PA-36 Series (Lycoming) Piper PA-36 Series (Continental) Piper PA-38 Series (Lycoming) Piper PA-46 Series (Continental) Piper PA-46 Series (Lycoming)
SKY Int Aviat Husky A (Lycoming)
EADS PZL “WARSZAWA-OKECIE” PZL-101A Gawron (Ivchenko) PZL-104A Wilga (Ivchenko) PZL-104 Wilga Series (PZL) PZL M 18 (PZL) PZL M 26 (Lycoming) PZL- 104 Wilga (Lycoming)
REGAL AIR, Inc. REGAL Air 305 Series (Continental)
REVO, Inc. REVO C/LA-4 Series (Lycoming)
SOCATA SOCATA MS 881 (Potez) SOCATA 894/PZL Koliber (Franklin) SOCATA Rallye Series (Continental) SOCATA Rallye Series ( Lycoming) SOCATA TB Series (Lycoming)
SYMPHONY AIRCRAFT Industries Symphony OMF-100-160 (Lycoming)
TECNAM Constuzioni Aeronautiche Tecnam P92 (Rotax)
SECTION 2 CAR 66
Rev 00 2-98 01 July 2011
Tecnam P96/P2002/P2004 (Rotax)
THRUSH Aircraft Ayres S2R (PW R-985)
TRUE FLIGHT Holdings Grumman/Ameracan AA-1 Series (Lycoming) Grumman/ Ameracan AA-5 Series (Lycoming)
VULCANAIR Partenavia P.64 (Lycoming) Partenavia P.66 (Lycoming)
WASSMER CERVA CE43 (Lycoming) CERVA CE44 (Continental)
YAKOVLEV Yakovlev YAK-18T (Vedeneyev) Yakovlev YAK-54/55/55M (Vedeneyev)
ZLIN AIRCRAFT (MORAVAN AVIATION) Zlin Z-42 Series (LOM) Zlin Z-43 (LOM) Zlin Z-50 (LOM) Zlin Z-50L Series (Lycoming) Zlin Z-26 Series (Walter Minor/Avia) Zlin Z-143L(Lycoming) Zlin Z-242L (Lycoming) Zlin Z-526L (Lycoming)
SECTION 2 CAR 66
Rev 00 2-99 01 July 2011
7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for type examinations and group ratings. No aircraft in this list.
SECTION 2 CAR 66
Rev 00 2-100 01 July 2011
8. Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE-WS), eligible for type examinations and group ratings.
TC holder Type rating endorsement
ALEXANDRIA AIRCRAFT Bellanca 14-19 Series (Continental) Bellanca 17-30/17-31 Series (Continental)
APEX CEAPR Robin ATL/ATL S (JPX 4T60) Robin ATL L (Limbach L2000)
APEX Dyn’Aero CAP 10 (Lycoming)
APEX CEAPR Robin DR 220 Series (Continental) Robin DR 250 Series (Lycoming) Robin DR 300 Series (Lycoming) Robin DR 400 Series (Lycoming) Robin DR 400RP (Porsche) Robin DR 400RP (Thielert)
AERICAN CHAMPION Champion 7 Series (Continental) Champion 7 Series (Lycoming) Champion 8 Series (Lycoming)
BOLKOW Klemm K1.107/F.207 (Continental) Bolkow F.207 (Lycoming)
MOONEY AIRPLANE Company Mooney M20/M20A (Lycoming) Mooney M18L (Continental)
NIPPER Nipper T-66 (Stark)
EIS RF 6B (Continental) RF 6B (Lycoming)
SCHEIBE Flugzeugbau SF 23 Series (Continental)
SKY INTERNATIONAL Pitts S-1 Series (Lycoming) Pitts S-2 Series (Lycoming)
Skyfox Aviation Ltd CA25 Series (Rotax)
SLINGSBY Aviation Slingsby T67 Series (Lycoming)
Eis GmBH RS 180 (Lycoming)
TAYLORCRAFT 2000 Taylorcraft 19 Series (Continental) Taylorcraft F21/F22 Series (Lycoming)
VULCANAIR Partenavia P57 (Lycoming)
WACO Aircraft Company Waco YMF (Jacobs)
WASSMER WA40 Series (Lycoming) WA41 (Lycoming) WA4/21 Series (Lycoming)
SECTION 2 CAR 66
Rev 00 2-101 01 July 2011
9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for type Examinations and group ratings
TC holder Type rating endorsement
DIAMOND AIRCRAFT Industries Diamond DA42 Series (Thielert) Daimond DA42 Series (Austro Engine)
SECTION 2 CAR 66
Rev 00 2-102 01 July 2011
10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible for type examinations And group rating.
TC holder Type rating endorsement
APEX Dyn’Aero CAP 20/21 (Lycoming) CAP230 Series (Lycoming)
AQUILA Aviation by Excellence AG Aquila AT01 (Rotax)
CESSNA AIRCRAFT Company (COLOMBIA) Cessna C300/C350/C400 (Continental)
CIRRUS Design Corporation Cirrus SR20 (Continental) Cirrus SR22 (Continental)
DIAMOND AIRCRAFT Industries Diamond DA20/DV20 (Rotax) Diamond DA20 (Continental) Diamond DA40 (Lycoming Diamond DA40 D (Thielert) Diamond DA 40 (Austro Engine)
AIRCRAFT Design and Certification (WD) D4 Fascination (Rotax)
EXTRA Flugzeugproduktions und Vertriebs-GmbH
Extra EA-300 (Lycoming) Extra EA-400 (Continental)
FFT GYROFLUG SC01 Series (Lycoming)
GROB Luft-und Raumfahrt Grob G115/120 Series (Lycoming)
INSTYTUT LOTNICTWA Instytut lotnictwa I-23 Manager (Lycoming)
INIZIATIVE INDUSTRIALI ITALIANE III Sky Arrow 650/710 (Rotax)
ISSOIRE AVIATION Issoire APM 20/30 (Rotax)
LIBERTY AEROSPACE Incorporated Liberty XL-2 (Continental)
GOMOLZIG Ruschmeyer R90-230RG (Lycoming)
SEASTAR CORP TSC Series (Lycoming)
SUKHOI Sukhoi SU-29 (Vedeneev) Sukhoi SU-31 (Vedeneev) Sukhoi SU-26 (Vedeneev) Sukhoi Su-29/31 (MGA)
SLINGSBY AVIATION Slingsby t67A/T67B/T67C/T67M series (Lycoming)
SECTION 2 CAR 66
Rev 00 2-103 01 July 2011
11. Multi-engine helicopters (MEH) – requiring type training and individual type rating.
1 TC holder 2 Helicopter Model
Commercial Designation
3 Type rating endorsement
AGUSTA A109E A109S AW109SP
Agusta A109 Series (PWC PW206/207)
A109 A109A A109AII A109C
Agusta A109 Series (RR Corp 250)
A109K2 Agusta A109 (Turbomeca Arriel 1)
A109E A109LUH
Agusta A109 Series (Turbomeca Arrius 2)
AB139 AW139
Agusta AB139 (PWC PT6)
EH101-500 Series EH101-510 Series EH101-300
Agusta/Westland EH-101 (GE CT7)
AGUSTA AB 212 Bell 212/Agusta AB212 PWC PT6)(
BELL HELICOPTER TEXTRON
212
214ST Bell 214ST (GE CT7)
412 412EP 412CF
Bell 412/Agusta AB412 (PWC PT6)
AGUSTA AB 412 AB412 EP
BELL HELICOPTER CANADA
427 Bell 427 (PWC PW207D)
222 222B 222U
Bell 222 (Honeywell LTS 101)
230 230 Exercutive 230 Utility 230 EMS
Bell 230 (RR Corp 250)
427 Bell 427 (PWC PW207D)
429 Bell 429 (PWC PW207D)
430 Bell 430 (RR Corp 250)
ERICKSON AIR-CRANE
EAC S-64F Erickson S-64 (PW JFTD 12)
EUROCOPTER SA 330 F SA 330 G SA 330 J
Eurocopter SA 330 (Turbomeca Turmo)
AS 332 C AS332 L AS 332 C1 As 332 L1
Eurocopter AS 332 (Turbomeca Makila 1A/1A2)
AS 332 L2 Eurocopter AS 332 L2 (Turbomeca Makila 1A2)
AS 355 E AS 355 F AS 355 F1 AS 355 F2
Eurocopter AS 355 (RR Corp 250)
SECTION 2 CAR 66
Rev 00 2-104 01 July 2011
AS 355 N AS 355 NP
Eurocopter AS 355 (Turbomeca Arrius 1)
SA 365 N Dauphin Eurocopter SA 365 N (Turbomeca Arriel 1)
SA 365 N1 AS 365 N2
Eurocopter SA 365 N1, AS 365 N2 (turbomeca Arriel 1)
AS 365 N3 Eurocopter AS 365 N3 (turbomeca Arriel 2C)
EC 155 B EC 155 B1
Eurocopter EC 155 (Turbomeca Arriel 2)
EC 225 LP Eurocopter EC 225 (Turbomeca Makila 2A)
SA 365 C SA 365 C1 SA 365 C2 SA 365 C3
Dauphin Eurocopter SA 365 C Series (Turbomeca Arriel 1)
SA 366 G1 Dauphin Eurocopter SA 366 G1 Series ( Lycoming LTS101)
EUROCOPTER DEUTSCHLAND GmbH
BO 105 BO 105 C/CBS-4/-5 BO 105 D/DB BO 105 DB-4 BO 105 DBS Series BO 105 LS A-1/A-3 BO 105 S
BO 105 Series (RR Corp 250)
Ec 135 P1 Series EC 135 P2 Series EC 635 P2+
Eurocopter 135 (PWC PW206)
EC 135 T1 Series EC 135 T2 Series EC 635 T1 EC 635 T2 Series
Eurocopter EC 135 (Turbomeca Arrius 2B)
MBB-BK 117 A Series MBB-BK 117 B Series
Eurocopter MBB-BK 117 A/B (Honeywell LTS 101)
MBB-BK 117 C1 Eurocopter MBB-BK 117 C1 (Turbomeca Arriel 1)
MBB-BK 117 C2 Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1)
KAMOV KA-32A/T Kamov Ka 32 (Klimov)
MD HELICOPTERS, INC.
MD900 MD Helicopter MD900 (PWC PW206/207)
PZL-SWIDNIK W-3A W-3AS
PZL-Swidnik W-3A/W-3AS (Rzeszow PZL-10W)
AGUSTA AS61N AS61NI
Agusta AS61N/Sikorsky S-61N (GE CT58) SIKORSKY
AIRCRAFT S-61N S-61NM
S-58 BT to JT Sikorsky S-58 (PWC PT6T)
S-76A Sikorsky S-76A (RR Corp 250)
S-76A S-76A+ Sikorsky S-76A (Turbomeca Arriel 1)
SECTION 2 CAR 66
Rev 00 2-105 01 July 2011
S-76A S-76A++
S-76B S-76B Sikorsky S-76B (PWC PT6)
S-76C
Sikorsky S-76C (Turbomeca Arriel 1)
S-76C S-76C
S-76C+ S-76C++
Sikorsky S76C (Turbomeca Arriel 2)
S-92A Sikorsky S-92A (GE CT7-8)
SECTION 2 CAR 66
Rev 00 2-106 01 July 2011
12. Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings.
1 TC holder 2 Helicopter Model
Commercial Designation
3 Type rating endorsement
AGUSTA A119 AW119 Mk II
Koala Agusta A119/ Agusta AW119 Mk II (PWC PT6)
BELL HELICOPTER TEXTRON
214B 214B-1
Bell 214 (Honeywell T5508)
BELL HELICOPTER CANADA
407
Bell 407 (RR Corp 250)
AGUSTA AB 204 B Series AB 205 A1
Agusta AB204, AB205 / Bell 204, 205 (Honeywell T53)
BELL HELICOPTER TEXTRON, INC.
204B 205A-1
AGUSTA AB 206A AB 206B
Agusta AB206 / Bell 206 (RR Corp 250) BELL
HELICOPTER TEXTRON CANADA LIMITED
206 Series from A to L
THE ENSTROM HELICOPTER CORPORATION
480 480B
Enstrom 480 (RR Corp 250)
EUROCOPTER
AS 350 AS 350 B1 AS 350 B2 AS 350 BA AS 350 BB
Ecureuil
Eurocopter AS 350 (Turbomeca Arriel 1)
AS 250 B3 Eurocopter AS350 (Turbomeca Arriel 2B)
AS 350 D Eurocopter AS 350 (Honeywell LTS 101)
EC 120 B Colibri Eurocopter EC 120 (Turbomeca Arrius 2F)
EC 130 B4 Eurocopter EC 130 (Turbomeca Arriel 2B)
SA 315 B Lama Eurocopter SA 315B (Turbomeca Artouste)
SA 3180 SA 318 B SA 318 C
Alouette-Astazou
Eurocopter SA 318 (Turbomeca Astazou)
SA 319 B Alouette III Eurocopter SA 319 (Turbomeca Astazou XIV)
SA 341 G Gazelle Eurocopter SA 341 (Turbomeca Astazou)
SA 342 J
Gazelle Eurocopter SA 342 J (Turbomeca Astazou XIV)
SA 360C Dauphin Eurocopter SA 360
SE 3160 SA 316 B SA 316 C
Alouette III
Eucopter SA 316 B/SA 316 C (Turbomeca Artouste)
KAMAN AEROSPACE CORPORATION
K-1200
Kaman K-1200 (Honeywell T5317)
SECTION 2 CAR 66
Rev 00 2-107 01 July 2011
MD HELICOPTERS INC. (MDHI)
369 H series 369 D to FF
MD Helicopters 369 Series / SEI NH-500D (RR Corp 250) S.E.I SERVIZI
ELICOTTERISTICI ITALIANI
NH-500D
MD HELICOPTERS INC. (MDHI)
600N 500N
MD Helicopters 369 Series / SEI NH-500D (RR Corp 250) S.E.I SERVIZI
ELICOTTERISTICI ITALIANI
AMD-500N
PZL-ŚWIDNIK SW-4 PZL SW-4 (RR Corp 250)
SCHWEIZER AIRCRAFT CORPORATION
269D
Schweizer 269D (RR Corp 250)
SECTION 2 CAR 66
Rev 00 2-108 01 July 2011
13. Helicopters – Single piston engine (HSPE), eligible for type examinations and group ratings.
1 TC Holder 2 Helicopter Model
Commercial Designation
3 Type rating endorsement
ANTARES INTERNATIONAL
SH-4 Silvercraft SH-4 (Franklin)
AGUSTA AB 102 Agusta AB 102 (PW S1H4)
BRANTLY INTERNATIONAL, INC.
B-2
Brantly B2 (Lycoming)
HELICOPTÈRES GUIMBAL
G2 Cabri Cabri G2 (Lycoming)
THE ENSTROM HELICOPTER CORPORATION
F-28 Series 280 Series
Enstrom F-28/280 (Lycoming)
SEI (BREDA-NARDI)
NH 300C
Model 300C
Schweizer / Breda Nardi 269/300 (Lycoming)
SCHWEIZER AIRCRAFT CORPORATION
269A 269B 269C 269C-1
ROBINSON HELICOPTER COMPANY
R22 R22 ALPHA R22 BETA R22 MARINER R44 R44 II
Robinson R22/R44 Series (Lycoming)
SIKORSKY AIRCRAFT
S-58 A to J Sikorsky S-58 (Wright Cyclone)
SECTION 2 CAR 66
Rev 00 2-109 01 July 2011
APPENDIX II
Aircraft Basic /Type Practical Experience List of Tasks
Time limits/Maintenance checks 100 hour check (general aviation aircraft) “B” or “C” check (transport category aircraft) Review records for compliance with airworthiness directives. Review records for compliance with component life limits. Procedure for Inspection following heavy landing. Procedure for Inspection following lightning strike. Dimensions/Areas Locate component(s) by station number. Perform symmetry check. Lifting and Shoring Assist in : Jack aircraft nose or tail wheel. Jack complete aircraft. Sling or trestle major component. Levelling/Weighing Level aircraft. Weigh aircraft. Prepare weight and balance amendment. Check aircraft against equipment list. Towing and Taxiing Tow aircraft. Be part of aircraft towing team. Parking and mooring Tie down aircraft. Park, secure and cover aircraft. Position aircraft in dock. Secure rotor blades. Placards and Markings Check aircraft for correct placards. Check aircraft for correct markings.
Servicing Refuel aircraft. Defuel aircraft. Check tire pressures. Check oil level. Check hydraulic fluid level. Check accumulator pressure. Charge pneumatic system. Grease aircraft. Connect ground power. Service toilet/water system Perform pre-flight/daily check Vibration and Noise Analysis Analyse helicopter vibration problem. Analyse noise spectrum. Air Conditioning Replace combustion heater. Replace outflow valve. Replace vapour cycle unit. Replace air cycle unit. Replace cabin blower. Replace heat exchanger. Replace pressurisation controller. Clean outflow valves. Check operation of air conditioning /heating system Check operation of pressurisation system Troubleshoot faulty system Auto flight Install servos. Rig bridle cables Replace controller. Replace amplifier. Check operation of auto-pilot. Check operation of auto-throttle. Check operation of yaw damper. Check and adjust servo clutch. Perform autopilot gain adjustments. Perform mach trim functional check. Troubleshoot faulty system. Check autoland system Check flight management systems Check stability augmentation system
SECTION 2 CAR 66
Rev 00 2-110 01 July 2011
Communications Replace VHF com unit. Replace HF com unit. Replace existing antenna. Replace static discharge wicks. Check operation of radios. Perform antenna VSWR check. Perform Selcal operational check. Perform operational check of passenger address system. Functionally check audio integrating system. Repair co-axial cable. Troubleshoot faulty system. Electrical Power Charge lead/acid battery. Charge ni-cad battery. Check battery capacity. Deep-cycle ni-cad battery. Replace generator/alternator. Replace switches. Replace circuit breakers. Adjust voltage regulator. Amend electrical load analysis report. Repair/replace electrical feeder cable. Troubleshoot faulty system Equipment/Furnishings Replace carpets Replace crew seats. Replace passenger seats. Check inertia reels. Check seats/belts for security. Check emergency equipment. Check ELT for compliance with regulations. Repair toilet waste container. Repair upholstery. Change cabin configuration. Fire protection Check fire bottle contents. Check operation of warning system. Check cabin fire extinguisher contents. Check lavatory smoke detector system. Install new fire bottle. Replace fire bottle squib. Troubleshoot faulty system. Inspect engine fire wire detection systems
Flight Controls Replace horizontal stabiliser. Replace elevator. Replace aileron. Replace rudder. Replace trim tabs. Install control cable and fittings. Replace flaps. Replace powered flying control unit Replace flat actuator Adjust trim tab. Adjust control cable tension. Check control range and sense of movement. Check for correct assembly and locking. Troubleshoot faulty system. Fuel Replace booster pump. Replace fuel selector. Replace fuel tank cells. Check filters. Flow check system. Check calibration of fuel quantity gauges. Check operation feed/selectors Troubleshoot faulty system. Hydraulics Replace engine driven pump. Replace standby pump. Replace accumulator. Check operation of shut off valve. Check filters. Check indicating systems. Perform functional checks. Troubleshoot faulty system. Ice and rain protection Replace pump. Replace timer. Install wiper motor. Check operation of systems. Troubleshoot faulty system. Indicating/recording systems Replace flight data recorder. Replace cockpit voice recorder. Replace clock. Replace master caution unit. Replace FDR. Perform FDR data retrieval.
SECTION 2 CAR 66
Rev 00 2-111 01 July 2011
Troubleshoot faulty system. Implement ESDS procedures Inspect for HIRF requirements Landing Gear Build up wheel. Replace main wheel. Replace nose wheel. Replace shimmy damper. Rig nose wheel steering. Replace shock strut seals. Replace brake unit. Replace brake control valve. Bleed brakes. Test anti skid unit. Test gear retraction. Change bungees. Adjust micro switches. Charge struts. Troubleshoot faulty system. Test outbrake system Lights Repair/replace rotating beacon. Repair/replace landing lights. Repair/replace navigation lights. Repair/replace interior lights. Repair/replace emergency lighting system. Perform emergency lighting system checks. Troubleshoot faulty system Navigation Calibrate magnetic direction indicator. Replace airspeed indicator. Replace altimeter. Replace air data computer. Replace VOR unit. Replace ADI. Replace HSI. Check pitot static system for leaks. Check operation of directional gyro. Functional check weather radar. Functional check doppler. Functional check TCAS. Functional check DME Functional check ATC Transponder Functional check flight director system. Functional check inertial nav system. Complete quadrantal error correction of ADF system. Update flight management system database. Check calibration of pitot static instruments.
Check calibration of pressure altitude reporting system. Troubleshoot faulty system Check marker systems Compass replacement direct/indirect Check Satcom Check GPS Test AVM Oxygen Inspect on board oxygen equipment. Purge and recharge oxygen system. Replace regulator. Replace oxygen generator. Test crew oxygen system. Perform auto oxygen system deployment check. Troubleshoot faulty system. Pneumatic systems Replace filter. Replace compressor. Recharge dessicator. Adjust regulator. Check for leaks. Troubleshoot faulty system. Vacuum systems Replace vacuum pump. Check/replace filters. Adjust regulator. Troubleshoot faulty system. Water/Waste Replace water pump. Replace tap. Replace toilet pump. Troubleshoot faulty system. Central Maintenance System Retrieve data from CMU. Replace CMU. Perform Bite check. Troubleshoot faulty system. Airborne Auxiliary power Install APU. Inspect hot section. Troubleshoot faulty system.
SECTION 2 CAR 66
Rev 00 2-112 01 July 2011
Structures Sheet metal repair. Fibre glass repair. Wooden repair. Fabric repair. Recover fabric control surface. Treat corrosion. Apply protective treatment. DoorsRig/adjust locking mechanism. Adjust air stair system. Check operation of emergency exits. Test door warning system. Troubleshoot faulty system. Windows Replace windshield. Replace window. Repair transparency. Wings Skin repair. Recover fabric wing. Replace tip. Replace rib. Check incidence/rig. Propeller Assemble prop after transportation. Replace propeller. Replace governor. Adjust governor. Perform static functional checks. Check operation during ground run. Check track. Check setting of micro switches. Dress out blade damage. Dynamically balance prop. Troubleshoot faulty system. Main Rotors Install rotor assembly. Replace blades. Replace damper assembly. Check track. Check static balance. Check dynamic balance. Troubleshoot.
Rotor Drive Replace mast. Replace drive coupling. Replace clutch/freewheel unit Replace drive belt. Install main gearbox. Overhaul main gearbox. Check gearbox chip detectors. Tail Rotors Install rotor assembly. Replace blades. Troubleshoot. Tail Rotor Drive Replace bevel gearbox. Replace universal joints. Overhaul bevel gearbox. Install drive assembly. Check chip detectors. Rotorcraft flight controls Install swash plate. Install mixing box. Adjust pitch links. Rig collective system. Rig cyclic system. Rig anti-torque system. Check controls for assembly and locking. Check controls for operation and sense. Troubleshoot faulty system. Power Plant Build up ECU. Replace engine. Repair cooling baffles. Repair cowling. Adjust cowl flaps. Repair faulty wiring. Troubleshoot. Piston Engines Remove/install reduction gear. Check crankshaft run-out. Check tappet clearance. Check compression. Extract broken stud.
SECTION 2 CAR 66
Rev 00 2-113 01 July 2011
Install helicoil. Perform ground run. Establish/check reference RPM. Troubleshoot. Turbine Engines Replace module. Hot section inspection. Engine ground run. Establish reference power. Trend monitoring/gas path analysis. Troubleshoot. Fuel and control, piston Replace engine driven pump. Adjust AMC. Adjust ABC. Install carburettor/injector. Adjust carburettor/injector. Clean injector nozzles. Replace primer line. Check carburettor float setting. Troubleshoot faulty system. Fuel and control, turbine Replace FCU. Replace engine driven pump. Clean/test fuel nozzles. Clean/replace filters. Adjust FCU. Troubleshoot faulty system. Ignition systems, piston Change magneto. Change ignition vibrator. Change plugs. Test plugs. Check H.T. leads. Install new leads. Check timing. Check system bonding. Troubleshoot faulty system. Ignition systems, turbine Check glow plugs/igniters. Check H.T. leads. Check ignition unit. Replace ignition unit. Troubleshoot faulty system.
Engine Controls Rig thrust lever. Rig RPM control. Rig mixture HP cock lever. Rig power lever. Check control sync (multi-eng) Check controls for correct assembly and locking. Check controls for range and sense of operation. Adjust pedestal micro-switches. Troubleshoot faulty system. Engine Indicating Replace engine instruments(s). Replace oil temperature bulb. Replace thermocouples. Check calibration. Troubleshoot faulty system. Exhaust, piston Replace exhaust gasket. Inspect welded repair. Pressure check cabin heater muff. Troubleshoot faulty system. Exhaust, turbine Change jet pipe. Change shroud assembly. Install trimmers. Oil Change oil. Check filter(s) Adjust pressure relief valve. Replace oil tank. Replace oil pump. Replace oil cooler. Replace firewall shut off valve. Perform oil dilution. Troubleshoot faulty system. Starting Replace starter. Replace start relay. Replace start control valve. Check cranking speed.
SECTION 2 CAR 66
Rev 00 2-114 01 July 2011
Troubleshoot faulty system. Turbines, piston engines Replace PRT. Replace turbo-blower. Replace heat shields. Replace waste gate. Adjust density controller. Engine water injection
Replace water/methanol pump. Flow checks water/methanol system. Adjust water/methanol control unit. Check fluid for quality. Troubleshoot faulty system Accessory gear boxes Replace gearbox. Replace drive shaft. Check chip detector.
SECTION 3 CAR 66
Rev 00 3-1 01 July 2011
SECTION 3
GUIDANCE MATERIAL
GM 66.20(a) Privileges 1. The following titles shown against each category designator below are intended to provide a
readily understandable indication of the job function:
Category A: Line maintenance certifying mechanic.
Category B1: Maintenance certifying Engineer - mechanical.
Category B2: Maintenance certifying Engineer - avionic.
Category C: Base maintenance certifying engineer.
The titles adopted by the GCAA may differ from those shown to reflect titles used in the national language for the above functions but the designators A, B1, B2 and C are required by CAR 66.20.
2. Individual aircraft maintenance licence holders need not be restricted to a single category.
Provided that each qualification requirement is satisfied, any combination of categories may be granted.
GM 66.20(a) Privileges 1. Tasks permitted by CAR 66.20 (a) 1. to be certified under the category A certification
authorisation as part of minor scheduled maintenance or simple defect rectification are as specified in CAR 145 and agreed by the GCAA. CAR 145 contains a typical example list of such tasks.
2. For the purposes of category A minor scheduled line maintenance means any minor check up to
but not including the A check where functional tests can be carried out by the aircrew to ensure system serviceability. In the case of an aircraft type not controlled by a maintenance programme based upon the A/B/C/D check principle, minor scheduled line maintenance means any minor check up to and including the weekly check or equivalent.
3. The category B1 licence also permits the certification of work involving avionic systems, providing
the serviceability of the system can be established by a simple self-test facility, other on-board test systems/equipment or by simple ramp test equipment. Defect rectification involving test equipment which requires an element of decision making in its application - other than a simple go/no-go decision - cannot be certified. The category B2 will need to be qualified as category A in order to carry out simple mechanical tasks and be able to make certifications for such work.
4. The category C certification authorisation permits certification of scheduled base maintenance by
the issue of a single certificate of release to service for the complete aircraft after the completion of all such maintenance. The basis for this certification is that the maintenance has been carried out by competent mechanics and both category B1 and B2 staff have signed for the maintenance under their respective specialisation. The principal function of the category C certifying staff is to ensure that all required maintenance has been called up and signed off by the category B1 and B2 staff before issue of the certificate of release to service. Category C personnel who also hold category B1 or B2 qualifications may perform both roles in base maintenance.
SECTION 3 CAR 66
Rev 00 3-2 01 July 2011
GM AMC 66.20(b)3 Privileges 1. Holders of a CAR 66 aircraft maintenance licence may not exercise certification privileges unless
they have a general knowledge of the language used within the maintenance environment including knowledge of common aeronautical terms in the language. The level of knowledge should be such that the licence holder is able to:
- read and understand the instructions and technical manuals in use within the organisation; - make written technical entries and any maintenance documentation entries, which can be
understood by those with whom they are normally required to communicate; - read and understand the maintenance organisation procedures; - communicate at such a level as to prevent any misunderstanding when exercising
certification privileges. 2. In all cases, the level of understanding should be compatible with the level of certification
privileges exercised. GM 66.25(a) Basic knowledge requirements The levels of knowledge are directly related to the complexity of certifications appropriate to the particular CAR 66.1 category, which means that category A should demonstrate a limited but adequate level of knowledge, whereas category B1 and B2 should demonstrate a complete level of knowledge in the appropriate subject modules. Category C certifying staff should meet the relevant level of knowledge for B1 or B2. GM 66.30(a) Basic knowledge requirements Maintenance experience on operating aircraft means the experience of being involved in maintenance tasks on aircraft which are being operated by airlines, air taxi organisations, etc. The point being to gain sufficient experience in the environment of commercial maintenance as opposed to only the training school environment. Such experience may be combined with approved training so that periods of training can be intermixed with periods of experience rather like the apprenticeship. GM 66.40 Continued validity of the aircraft maintenance licence Validity of the CAR 66 aircraft maintenance licence is not affected by recency of maintenance experience whereas the validity of the CAR 66.20 privileges is affected by maintenance experience as specified in CAR 66.20(a) GM 66.45(d) Type/task training and ratings 1. The required duration of practical training should be accepted on a case by case basis by the
GCAA prior to the type rating endorsement. It is strongly recommended that the agreement on the practical training duration be reached before the training starts.
2. While it is not feasible to establish a formula giving the required training duration in all cases, the
following may be used as a guideline:
(a) For a first type training course with no recent recorded maintenance experience four months practical training is required.
SECTION 3 CAR 66
Rev 00 3-3 01 July 2011
(b) Some factors that may lead to a reduction in the maximum duration of 4 months practical training required are as follows:
- experience on aircraft type of a similar technology, construction and systems including
engines; - recency on type; - the quantity of the practical experience. For example experience gained will depend upon
the environment e.g. line maintenance environment with one aircraft per week would permit limited experience compared with the constant base maintenance check environment;
- the quality of the practical experience. The type of tasks carried out. These tasks should
reflect, at a minimum, those tasks specified by the practical training needs matrix developed by the organisation approved under CAR 147.
3. The minimum two weeks practical training is normally required for all type training courses. This
includes the addition of similar type ratings on a CAR 66 licence (differences courses). There may be cases where the practical differences training required is less than two weeks for example an engineer with a CAR 66 type license in category B2 on an Airbus A330 with PW 4000 engines who takes a differences course to an Airbus A330 with Rolls Royce Trent engines. It should be noted however that while CAR 66.45(d) specifies a practical training duration between 2 weeks and 4 months, in the case of a structured OJT performed at line stations, due to the availability of aircraft its duration may need be subsequently extended in order to fulfil the required list of supervised tasks.
4. Except in those cases where the CAR 147 organisation determines the practical training required
it is the responsibility of the maintenance organisation to determine that the duration of practical training is commensurate with the candidates’ recency and experience. However, in either case the GCAA should ensure that the practical training is of sufficient duration before adding a type rating. Limited avionics system training should be included in the category B1 type training as the B1 privileges include the replacement of avionic line replaceable units. Electrical systems should be included in both type training categories.
GM 66.45(d) and (e) Type/task training and ratings CAR 66 Appendix III type training levels are based upon ATA 104 (Air Transport Association) corresponding type training levels. GM 66.45(f) Type/task training and ratings The examinations in respect of category B1 or B2 or C aircraft type ratings may be conducted by training organisations appropriately approved under CAR 147, the GCAA or an organisation accepted by the GCAA to conduct such examination. Guidance to CAR 66.70 Conversion provisions For example a technical limitation could be where a person holds a pre CAR 66 licence or authorisation limited to the release of the airframe and engine but not the electrical power system. This person would be issued with a CAR 66 aircraft maintenance licence in the B1 category with a limitation excluding electrical power systems.
