Part-66 - acao.org.maacao.org.ma/programmes/1455710432_2.pdf · Part-66 Appendix III — Type training and Examination Standard Part-66 Appendix IV — Experience requirements for

For training purpose only, created: January 2011 Seite 1

This part is addressed to Organisations involved

CONTENTS

66.1

SECTION A — TECHNICAL REQUIREMENTS

SUBPART A — AIRCRAFT MAINTENANCE LICENCE AEROPLANES AND HELICOPTERS66.A.1 Scope66.A.10 Application66.A.15 Eligibility66.A.20 Privileges66.A.25 Basic knowledge requirements66.A.30 Experience requirements66.A.40 Continued validity of the aircraft maintenance licence66.A.45 Type/task training and ratings66.A.55 Evidence of qualification66.A.70 Conversion provisionsSUBPART B — AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS66.A.100 GeneralSUBPART C — COMPONENTS66.A.200 General

SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES

SUBPART A — GENERAL66.B.05 Scope66.B.10 Competent authority66.B.15 Acceptable means of compliance

CONTENTS

Part-66Certifying staff

Certifying staff shall be qualified in accordance with this part

Sources: official journey of EU council (http://eur-lex.europa.eu/en/index.htm)EASA – homepage (http://www.easa.eu.int)

2012

For Training Purpose Only Page 1

CONTENT

66.1

SECTION A — TECHNICAL REQUIREMENTS

SUBPART A — AIRCRAFT MAINTENANCE LICENCE AEROPLANES AND HELICOPTERS66.A.1 Scope66.A.10 Application66.A.15 Eligibility66.A.20 Privileges66.A.25 Basic knowledge requirements66.A.30 Experience requirements66.A.40 Continued validity of the aircraft maintenance licence66.A.45 Type/task training and ratings66.A.55 Evidence of qualification66.A.70 Conversion provisions

SUBPART B — AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS66.A.100 General

SUBPART C — COMPONENTS66.A.200 General


SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES

SUBPART A — GENERAL66.B.05 Scope66.B.10 Competent authority66.B.15 Acceptable means of compliance66.B.20 Record-keeping66.B.25 Mutual exchange of information66.B.30 Exemptions

SUBPART B — ISSUE OF AN AIRCRAFT MAINTENANCE LICENCE66.B.100 Procedure for the issue of an aircraft maintenance licence by the competent authority66.B.105 Procedure for the issue of an aircraft maintenance licence via the Part-145 approved maintenance organisation66.B.110 Procedure for the change of an aircraft maintenance licence to include an additional basic category or subcategory66.B.115 Procedure for the change of an aircraft maintenance licence to include an aircraft type or group66.B.120 Procedure for the renewal of an aircraft maintenance licence validity

SUBPART C — EXAMINATIONS66.B.200 Examination by the competent authority

SUBPART D — CONVERSION OF NATIONAL QUALIFICATIONS66.B.300 General66.B.305 Conversion report for national qualifications66.B.310 Conversion report for approved maintenance organisations authorisationsSUBPART E — EXAMINATION CREDITS 66.B.400 General66.B.405 Examination credit report


SUBPART F — REVOCATION, SUSPENSION OR LIMITATION OF THE AIRCRAFT MAINTENANCE LICENCE66.B.500 Revocation, suspension or limitation of the aircraft maintenance licence

Part-66 Appendix I — Basic Knowledge RequirementsPart-66 Appendix II — Basic Examination StandardPart-66 Appendix III — Type training and Examination StandardPart-66 Appendix IV — Experience requirements for extending a Part-66 Aircraft Maintenance LicencePart-66 Appendix V — Application Form — EASA Form 19Part-66 Appendix VI — Aircraft Maintenance Licence referred to in Annex III (Part-66) — EASA Form 26

AMC Part-66 Appendix I —Aircraft type ratings for Part-66 aircraft Maintenance licenceAMC Part-66 Appendix II — Aircraft Type Practical Experience - List of Task’s


66.1

For the purpose of this Part, the competent authority shall be the authority designated by the Member State to whom a

person applies for the issuance of an aircraft maintenance licence.



SUBPART AAIRCRAFT MAINTENANCE LICENCE

AEROPLANES AND HELICOPTERS


66.A.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

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


66.A.10 Application

a) An application for an aircraft maintenance licence or change to such licence shall be made on an EASA Form 19 in a

manner established by the competent authority and submitted thereto.

b) An application for the change to an aircraft maintenance licence shall be made to the competent authority of the

Member State that first issued the aircraft maintenance licence.

c) In addition to the documents required in points 66.A.10(a), 66.A.10(b) and 66.B.105, as appropriate, the applicant for

additional basic categories or subcategories to an aircraft maintenance licence shall submit his/her current original

aircraft maintenance licence to the competent authority together with EASA Form 19.

d) Where the applicant for change of the basic categories qualifies for such change via the procedure referred to in point

66.B.100 in a Member State other than the Member State in which he/she first qualified, the application shall be sent to

the Member State of first qualification.

e) Where the applicant for change of the basic categories qualifies for such change via the procedure referred to in point

66.B.105 in a Member State other than the Member State in which he/she first qualified, the maintenance organisation

approved in accordance with Annex II (Part-145) shall send the aircraft maintenance licence together with the EASA

Form 19 to the competent authority of the Member State of first qualification for Member State stamp and signature of

the change or reissue of the licence.


AMC 66.A.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 some competent authorities may require such log book to be kept. It is acceptable to cross refer in the EASA Form 19 to

other documents containing information on maintenance.

2. Applicants claiming the maximum reduction in 66.A.30(a) total experience based upon having successfully completed 147.A.200 approved basic training, should include

the Part-147 certificate of recognition for approved basic training.

3. Applicants claiming reduction in 66.A.30(a) total experience based upon having successfully completed technical training in an organisation or institute recognised by

the competent authority as a competent organisation or institute, should include the relevant certificate of successful completion of training.


66.A.15 Eligibility

An applicant for an aircraft maintenance licence shall be at least 18 years of age.


66.A.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 Part-145 organisation.

2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of release to service following

maintenance, including aircraft structure, powerplant 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 Part-145 organisation.


AMC 66.A.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 powerplant 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 Member State will prescribe the conditions under which these tasks

may be 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.

GM 66.A.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 technician - mechanical.

Category B2: Maintenance certifying technician - avionic.

Category C: Base maintenance certifying engineer.


The titles adopted by each competent authority 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 66.A.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.A.20(a)Privileges

1. Tasks permitted by 66.A.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 Part 145 and agreed by the competent authority. Part 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.


66.A.20 Privileges

b) The holder of an aircraft maintenance licence may not exercise certification privileges unless:

1. in compliance with the applicable requirements of Part-M and/or Part-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.

AMC 66.A.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 M.A.801(b)2 or as a combination hereof.

When certifying staff maintains and releases aircraft in accordance with M.A.801(b)2, in certain circumstances this number of days may even be reduced by 50% when

agreed in advance by the competent authority. These circumstances consider the cases where the holder of a Part-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 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.A.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 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 turboshaft 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 66.A.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 66.A.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 (optional);

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: as per article 5 of regulation 2042/2003, this experience requirement does not apply to:

Certifying staff issuing a certificate of release of aircraft as per M.A.607(b);

Pilot-owner certifying tasks according to M.A.803; and

Certifying staff according to 145.A30(j) and Appendix IV of Part-145.

GM 66.A.20(b)3. Privileges

1. Holders of a Part-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.


66.A.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 Part.

The basic knowledge examinations shall be conducted by a training organisation appropriately approved under Part-

147 or by the competent authority.

GM 66.A.25(a) Basic knowledge requirements

The levels of knowledge are directly related to the complexity of certifications appropriate to the particular 66.A.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.


66.A.25 Basic knowledge requirements

b) Full or partial credit against the basic knowledge requirements and associated examination shall be given for any other

technical qualification considered by the competent authority to be equivalent to the knowledge standard of this Part.

Such credits shall be established in accordance with Section B, Subpart E of this Part.

AMC 66.A.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 Part-66.

2. Knowledge gained and examinations passed during previous experiences, for example, in military aviation and civilian apprenticeships will be credited where the

competent authority is satisfied that such knowledge and examinations are equivalent to that required by Appendix I to Part-66.


66.A.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

ii. two years of practical maintenance experience on operating aircraft and completion of training considered

relevant by the competent authority as a skilled worker, in a technical trade; or

iii. one year of practical maintenance experience on operating aircraft and completion of a Part-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 competent authority as a skilled worker, in a technical trade; or

iii. two years of practical maintenance experience on operating aircraft and completion of a Part -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 Part-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 Part-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 Part-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 competent authority, 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.

AMC 66.A.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 Part-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 competent authority, involving the manufacture, repair, overhaul or

inspection of mechanical, electrical or electronic equipment. The training would include the use of tools and measuring devices.


GM 66.A.30(a)

Maintenance experience on operating aircraft means the experience of being involved on maintenance tasks on aircraft which are being operated by airlines, air taxi

organizations, 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.



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 Part.


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 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.

AMC 66.A.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

Part-66 aircraft maintenance licence. The remainder of the experience should have been gained within the 7 year period prior to application.



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 Part as established by the

competent authority. Additional experience of civil aircraft maintenance shall, however, be required to ensure

understanding of the civil aircraft maintenance environment.

AMC 66.A.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.


66.A.40 Continued validity of the aircraft maintenance licence

a) The aircraft maintenance licence becomes invalid five years after its last issue or change, unless the holder submits

his/her aircraft maintenance licence to the competent authority that issued it, in order to verify that the information

contained in the licence is the same as that contained in the competent authority records, pursuant to point 66.B.120.

b) The holder of an aircraft maintenance licence shall complete the relevant parts of EASA Form 19 and submit it with the

holder's copy of the licence to the competent authority that issued the original aircraft maintenance licence, unless the

holder works in a maintenance organisation approved in accordance with Annex II (Part- 145) that has a procedure in

its exposition whereby such organisation may submit the necessary documentation on behalf of the aircraft

maintenance licence holder.

c) Any certification privilege based upon a aircraft maintenance licence becomes invalid as soon as the aircraft

maintenance licence is invalid.

d) The aircraft maintenance licence is only valid (i) when issued and/or changed by the competent authority and (ii) when

the holder has signed the document.

GM 66.A.40 Continued validity of the aircraft maintenance licence

Validity of the Part-66 aircraft maintenance licence is not affected by recency of maintenance experience whereas the validity of the 66.A.20 privileges is affected by

maintenance experience as specified in 66.A.20(a)


66.A.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 Part-145 or Part-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 Part-145 or Part-147

organisation.

AMC 66.A.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 66.A.20 (a) 1.

2. Appropriately approved Part-145 or Part-147 organisation means compliance with the applicable paragraphs of AMC 66.A.45.



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 competent authority or conducted by an

appropriately approved Part-147 maintenance training organisation.



d) Category B1 and B2 approved type training shall include theoretical and practical elements and consist of the

appropriate course in relation to the 66.A.20(a) privileges. Theoretical and practical training shall comply with Appendix

III to this Part.

AMC 66.A.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.

a) The course should also take into account the following:

b) in service experience on the aircraft type;

c) feedback from in-service difficulties/occurrence reporting etc;

d) significant airworthiness directives and/or service bulletins;

e) 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 the critical aspects such as of Fuel Tank Safety (FTS) airworthiness limitation items (ALI) including

Critical Design Configuration Control Limitations (CDCCL).

EASA guidance is provided for training in Appendix IV to AMC to 66.A.45(d).

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 two 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 an Part-147 approval or a direct type course

approval, it should be considered as part of the approved course and as such, its acceptance by the competent authority 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 Part-147 school or other course provider.


Where the practical training element is conducted by a maintenance organisation approved under Part-145, under its own responsibility, its acceptance by the

competent authority 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 Part-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 either

directly for each individual – depending on the individuals 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 of maintenance tasks, which, in the case of a structured OJT, can be tailored to

accommodate the operating profile of the Part-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 Member State. The duration of the practical type training element should take into account

significant differences between types and be acceptable to the Member State. 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.


GM 66.A.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 competent authority prior to the type rating endorsement. It is strongly

recommended that the agreement on the practical training duration be reached before the training starts. For applicants from a Part-145 organisation, the required

duration may be approved through the organisation’s MOE procedures.

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.

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 Part-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 Part-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 Part-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 AMC 66.A.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 Part-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 Member State 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.A.45(d) and (e) Type/task training and ratings

Part-66 Appendix III type training levels are based upon ATA 104 (Air Transport Association) corresponding type training levels.



e) Category C approved type training shall comply with Appendix III to this Part. In the case of a category C person

qualified by holding an academic degree as specified in 66.A.30(a), (5), the first relevant aircraft type theoretical

training shall be at the category B1 or B2 level. Practical training is not required.

AMC 66.A.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.

GM 66.A.45(d) and (e) Type/task training and ratings

Part-66 Appendix III type training levels are based upon ATA 104 (Air Transport Association) corresponding type training levels.



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 Part. The examinations in respect of category B1 or

B2 or C aircraft type ratings shall be conducted by training organisations appropriately approved under Part-147, the

competent authority, or the training organisation conducting the approved type training course.

GM 66.A.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 Part-147, the Member

State or an organisation accepted by the Member State to conduct such examination.



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 Agency 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

aeroplane multiple piston engines — composite structure

aeroplane turbine — single engine

aeroplane turbine — multiple engine

ii. for category B2 or C:

aeroplane

helicopter


AMC 66.A.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.



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 Agency has determined that the aircraft is complex, where paragraph (c) approved type

training is required.

In the case of a category C rating on aircraft other than large aircraft, for a person qualified by holding an academic

degree as specified in point 66.A.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 Annex III (Part-66). The examination shall be conducted by

training organisations appropriately approved in accordance with Annex IV (Part-147) or by the competent

authority.

3. Aircraft type practical experience shall include a representative cross section of maintenance activities relevant to

the category.

AMC 66.A.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 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 records or logbook showing the Appendix II tasks performed by the applicant as specified by the

competent authority.


66.A.55 Evidence of qualification

Personnel exercising certification privileges must produce their licence, as evidence of qualification, if requested by an

authorised person, within 24 hours.


66.A.70 Conversion provisions

a) The holder of a certifying staff qualification valid in a Member State, prior to the date of entry into force of this Part

shall be issued an aircraft maintenance licence without further examination subject to the conditions specified in

66.B.300.

b) A person undergoing a qualification process valid in a Member State, prior to the date of entry into force of this Part

may continue to be qualified. The holder of a qualification gained following such qualification process shall be issued an

aircraft maintenance licence without further examination subject to the conditions specified in 66.B.300

c) Where necessary, the aircraft maintenance licence shall contain technical limitations in relation to the scope of the pre-

existing qualification.

AMC 66.A.70 Conversion provisions

Technical limitations will be deleted, as appropriate, when the person satisfactorily sits the relevant conversion examination and gains relevant experience.

Guidance to 66.A.70 Conversion provisions

For example a technical limitation could be where a person holds a pre Part-66 national licence or authorisation limited to the release of the airframe and engine but not the

electrical power system. This person would be issued with an Part-66 aircraft maintenance licence in the B1 category with a limitation excluding electrical power systems.


SUBPART BAIRCRAFT OTHER THAN

AEROPLANES AND HELICOPTERS


66.A.100 General

Until such time as this Part specifies a requirement for certifying staff of aircraft other than aeroplanes and helicopters, the

relevant Member State regulation shall apply.


SUBPART CCOMPONENTS


66.A.200 General

Until such time as this Part specifies a requirement for certifying components, the relevant Member State regulation shall

apply.



SUBPART AGENERAL


66.B.05 Scope

This section establishes the administrative requirements to be followed by the competent authorities in charge of the

application and the enforcement of Section A of this Part.


66.B.10 Competent authority

a) General

The Member State shall designate a competent authority with allocated responsibilities for the issuance, continuation,

change, suspension or revocation of aircraft maintenance licences. This competent authority shall establish an

organisational structure and documented procedures for ensuring compliance with Annex III (Part-66).

b) Resources

The competent authority shall be appropriately staffed to carry out the requirements of this Part.

c) Procedures

The competent authority shall establish procedures detailing how compliance with this Part is accomplished.

The procedures shall be reviewed and amended to ensure continued compliance.


66.B.15 Acceptable means of compliance

The Agency shall develop acceptable means of compliance that the Member States may use to establish compliance with this

Part. When the acceptable means of compliance are complied with, the related requirements of this Part shall be considered

as met.


66.B.20 Record-keeping

a) The competent authority shall establish a system of record-keeping that allows adequate traceability of the process to

issue, revalidate, change, suspend or revoke each aircraft maintenance licence.

b) The records for the oversight of the Part shall include:

1. the application for an aircraft maintenance licence or change to that licence, including all supporting

documentation;

2. a copy of the aircraft maintenance licence including any changes;

3. copies of all relevant correspondence;

4. details of any exemption and enforcement actions;

5. any report from other competent authorities relating to the aircraft maintenance licence holder;

6. records of examinations conducted by the competent authority;

7. aircraft maintenance licence conversion reports;

8. examination credit reports.

c) Records referred to in paragraph (b), 1. to 5. shall be kept at least five years after the end of the licence validity.

d) Records referred to in paragraph (b), 6. shall be kept at least five years.

e) Records referred to in paragraph (b), 7. and 8. shall be kept for an unlimited period.


66.B.25 Mutual exchange of information

a) In order to contribute to the improvement of air safety, the competent authorities shall participate in a mutual

exchange of all necessary information in accordance with Article 11 of the basic Regulation.

b) Without prejudice to the competencies of the Member States, in the case of a potential safety threat involving several

Member States, the concerned competent authorities shall assist each other in carrying out the necessary oversight

action.


66.B.30 Exemptions

All exemptions granted in accordance with Article 10, 3. of the basic Regulation shall be recorded and retained by the

competent authority.


SUBPART BISSUE OF AN AIRCRAFT MAINTENANCE

LICENCE

This Subpart provides the procedures to be followed by the competent authority to issue or vary or to permit continuity of the aircraft maintenance licence.


66.B.100 Procedure for the issue of an aircraft maintenance licence by the competent

authority

a) On receipt of EASA Form 19 and any supporting documentation, the competent authority shall verify EASA Form 19 for

completeness and ensure that the experience claimed meets the requirement of this Part.

b) The competent authority shall verify an applicant's examination status and/or confirm the validity of any credits to

ensure that all required modules of Appendix I have been met as required by this Part.

c) When satisfied that the applicant meets the standards of knowledge and experience required by this Part, the

competent authority shall issue the relevant aircraft maintenance licence to the applicant. The same information shall

be kept on competent authority file.

AMC 66.B.100 Procedure for the issue of an aircraft maintenance licence by the competent authority

1. Applicants claiming credit against the 66.A.30(a) total experience requirement by virtue of 66.A.30(d) non-civil aircraft maintenance experience, may only be granted

such credit where the Member State has recognised such non-civil aircraft maintenance experience. The competent authority in recognising non-civil aircraft

maintenance experience will have specified who within the non-civil environment may make a statement that the applicant has met relevant maintenance experience.

The applicant should include a detailed statement of such maintenance experience signed by the non-civil maintenance authority in accordance with the conditions

specified in the competent authority’s letter of recognition.

2. The competent authority should check that the experience record satisfies above paragraphs in terms of content and the countersigning signature.

AMC 66.B.100 to 115

Aircraft type endorsement should use the standard codes contained in Appendix I.


66.B.105 Procedure for the issue of an aircraft maintenance licence via the Part-145

approved maintenance organisation

a) A Part-145 maintenance organisation which has been authorised to carry out this activity by the competent authority

may prepare the aircraft maintenance licence on behalf of the competent authority or make recommendations to the

competent authority regarding the application from an individual for a aircraft maintenance licence so that the

competent authority may prepare and issue such licence.

b) The Part-145 maintenance organisation shall ensure compliance with 66. B.100 (a) and (b). In all cases, the competent

authority shall issue the aircraft maintenance licence to the applicant.


AMC 66.B.105 Procedure for the issue of an aricraft maintenance licence via the Part-145 approved maintenance

organisation

1. The maintenance organisation approved under Part 145 procedure should be included in the organisation’s exposition and audited by the Member State at least once

in each 12 month period.

2. Applicants claiming the maximum reduction in -66.A.30(a) total experience based upon having successfully completed a 147.A.200 approved basic training course,

should include the Part-147 certificate of recognition for approved basic training.

3. Applicants claiming reduction in -66.A.30(a) total experience based upon having successfully completed technical training in an organisation or institute recognised by

the competent authorityas a competent organisation or institute, should include the relevant certificate of successful completion of training.

4. Applicants claiming credit against the -66.A.30(a) total experience requirement by virtue of -66.A.30(d) non-civil aircraft maintenance experience, may only claim such

credit where the competent authority has recognised such non-civil aircraft maintenance experience. The competent authority in recognising non-civil aircraft

maintenance experience will have specified who within the non-civil environment may make a statement that the applicant has gained the relevant maintenance

experience. The applicant should include a detailed statement of such maintenance experience signed by the non-civil maintenance authority in accordance with the

conditions specified in the competent authority letter of recognition.

5. The Part 145 organisation should check that the experience record has been countersigned by the maintenance organisation approved under Part 145 except for the

non-civil aircraft maintenance experience specified above.

6. The maintenance organisation approved under Part 145 may keep the experience record of applicants in a different form from that of application EASA Form 19 but

such different form or manner should be acceptable to the competent authority.

AMC 66.B.100 to 115



66.B.110 Procedure for the change of an aircraft maintenance licence to include an

additional basic category or subcategory

a) At the completion of the procedures specified in points 66.B.100 or 66.B.105, the competent authority shall endorse the

additional basic category or subcategory on the aircraft maintenance licence by stamp and signature or reissue the

licence.

b) The competent authority record system shall be changed accordingly.

AMC 66.B.110 Procedure for the amendment of an aircraft maintenance licence to include an additional basic

category or subcategory

In the case of computer generated licences, the licence should be reissued.

AMC 66.B.100 to 115



66.B.115 Procedure for the change of an aircraft maintenance licence to include an

aircraft type or group

On receipt of a satisfactory EASA Form 19 and any supporting documentation demonstrating compliance with the applicable

type rating and/or group rating requirements and the accompanying aircraft maintenance licence, the competent authority

shall either endorse the applicant's aircraft maintenance licence with the aircraft type or group or reissue the said licence to

include the aircraft type or group. The competent authority record system shall be changed accordingly.

AMC 66.B.115 Procedure for the amendment of an aircraft maintenance licence to include an aircraft type or

group

Where aircraft type training is covered by more than one course, for example airframe and engine courses, the competent authority should ensure prior to the type rating

endorsement that the content of the courses fully covers the scope of the license category. In this case, it is important that the interface is addressed.

In the case of differences training for a similar type, the competent authority should be satisfied that the candidates previous qualification supplemented by the differences

training is acceptable as regards the type endorsement.

Determination of compliance with the practical elements can be demonstrated by provision of the detailed practical training records or logbook or, where available by an Part-

147 training certificate covering the practical training element.

AMC 66.B.100 to 115


GM 66.B.115

Where the maintenance organisation approved under Part-145 conducts the practical training, it should confirm to the competent authority that the trainee has been assessed

and has successfully completed the practical elements of type training course to satisfy the requirements of 66.A.45(c). The competent authority is required to agree on how the

practical elements are assessed, for example under a procedure as agreed by the competent authority or on a case by case basis.


66.B.120 Procedure for the renewal of an aircraft maintenance licence validity

a) The competent authority shall compare the holder's aircraft maintenance licence with the competent authority records

and verify any pending revocation, suspension or change action pursuant to point 66.B.500. If the documents are

identical and no action is pending pursuant to point 66.B.500, the holder's copy shall be renewed for five years and the

file endorsed accordingly.

b) If the competent authority records are different from the aircraft maintenance licence held by the licence holder:

1. the competent authority shall investigate the reasons for such differences and may choose not to renew the aircraft

maintenance licence;

2. the competent authority shall inform the licence holder and any known maintenance organisation approved in

accordance with Annex I (Part-M) Subpart F or Annex II (Part-145) that may be directly affected of such fact;

3. the competent authority shall, if necessary, take action in accordance with point 66.B.500 to revoke, suspend or

change the licence in question.

AMC 66.A.120

The competent authority should not carry out any investigation to ensure that the licence holder is in current maintenance practice as this is not a condition for the renewal of a

licence. Ensuring the continued validity of the certification privileges is a matter for the approved Part-145 / Subpart-F maintenance organization or the certifying staff in

accordance with M.A.801(b)2.

For the purpose of ensuring the continued validity of the certification privileges the competent authority may, when periodically reviewing the organizations in accordance with

145.B.30 or M.B.604, or during on the spot checks, request the licence holder for documentary evidence of compliance with 66.A.20(b) when exercising certification privileges.


SUBPART CEXAMINATIONS

This subpart provides a procedure for examination conducted by the competent authority.


66.B.200 Examination by the competent authority

a) All examination questions shall be kept in a secure manner prior to an examination, to ensure that candidates will not

know which particular questions will form the basis of the examination. The competent authority shall nominate those

persons who control the questions to be used for each examination.

b) The competent authority shall appoint examiners who shall be present during all examinations to ensure the integrity

of the examination.

c) Basic examinations shall follow the standard specified in Appendix I and II to this Part.

d) Type examinations must follow the standard specified in Appendix III to this Part.

e) New essay questions shall be raised at least every six months and used questions withdrawn or rested from use. A

record of the questions used shall be retained in the records for reference.

f) All examination papers shall be handed out at the start of the examination to the candidate and handed back to the

examiner at the end of the allotted examination time period. No examination paper may be removed from the

examination room during the allotted examination time period.

g) Apart from specific documentation needed for type examinations, only the examination paper may be available to the

candidate during the examination.

h) Examination candidates shall be separated from each other so that they cannot read each other's examination papers.

They may not speak to any person other than the examiner.

i) Candidates who are proven to be cheating shall be banned from taking any further examination within 12 months of

the date of the examination in which they were found cheating.


GM 66.B.200 Examination by the competent authority

1. Questions may be prepared in the national language but the use of aviation English is recommended wherever possible.

2. The primary purpose of essay questions is to determine that the candidate can express themselves in a clear and concise manner and can prepare a concise technical

report for the maintenance record, which is why only a few essay questions are required.

3. Oral type questions may not be used as the primary means of examination because of the difficulty in establishing consistency of standards between examiners or day

to day.

Nothing however prevents the competent authority from meeting potential certifying staff for the purpose of ensuring they understand their obligations and

responsibilities in the application of maintenance Parts.

4. For pass mark purposes, the essay questions should be considered as separate from the multiple choice questions.

5. Multiple choice question (MCQ) generation.

The following principles should be observed when developing multiple choice question:

a) The examination should measure clearly formulated goals. Therefore the field and depth of knowledge to be measured by each question should be fully identified.

b) All the questions should be of the multiple choice type with three alternative answers.

c) Questions that require specialised knowledge of specific aircraft types, should not be asked in a basic licence examination.

d) The use of abbreviations and acronyms should be generally avoided. However were needed, only internationally recognized abbreviations and acronyms should be

used. In case of doubt use the full form, e.g. angle of attack = 12 degrees instead of a= 12°.

e) Questions and answers should be formulated as simply as possible: the examination is not a test of language. Complex sentences, unusual grammar and double

negatives should be avoided.

f) A question should comprise one complete positive proposition. No more than 3 different statements should appear among the suggested responses otherwise the

candidate may be able to deduce the correct answer by eliminating the unlikely combinations of statements.

g) Questions should have only one true answer.

h) The correct answer should be absolutely correct and complete or, without doubt, the most preferable. Responses that are so essentially similar that the choice is a

matter of opinion rather than a matter of fact should be avoided. The main interest in MCQs is that they can be quickly performed: this is not achieved if doubt exists

about the correct answer.

i) The incorrect alternatives should seem equally plausible to anyone ignorant of the subject. All of the alternatives should be clearly related to the question and be of

similar vocabulary, grammatical structure and length. In numerical questions, the incorrect answers should correspond to procedural errors such as corrections applied

in the wrong sense or incorrect unit conversions: they should not be mere random numbers.


j) Calculators are not allowed during examination. Therefore all calculations should be feasible without a calculator. Where a question involves calculations not feasible

without a calculator, such as 10 , then the question should specify the approximate value of 10 .

k) Questions should be referred to Part-66 Appendix I examination syllabus.

6. Essay question generation

a) The purpose of the essay is to allow the competent authority to determine if candidates can express themselves in a clear and concise manner in the form of a written

response, in a technical report format using the technical language of the aviation industry. The essay examination also allows to assess, in part, the technical

knowledge retained by the individual and with a practical application relevant to a maintenance scenario.

b) Questions should be written so as to be broad enough to be answered by candidates for all licence category or sub-categories (Cat A, B1 & B2) and comply with the

following general guidelines.

the question topic selected should be generic, applicable to mechanical as well as avionic licence categories and have a common technical difficulty level as

indicated in Part -66, Appendix I.

cover technology applicable to most areas of aircraft maintenance. - reflects common working practises.

it is not type or manufacturer specific and avoids subjects which are rarely found in practice.

when drafting a question there is need to ensure consideration is given to the limited practical experience that most candidates will have.

c) In order that the questions and the marking procedures are as consistent as possible, each question and model answer, with the required key areas required (see

below) should be reviewed independently by at least 2 technical staff.

d) When raising questions the following should be considered:

each essay question will have a time allowance of 20 minutes.

a complete A4 side is provided for each question and answer, if required the answer can be extended onto the reverse side of the page.

the question should be such that the answer expected will be at the level shown for that subject in the module syllabus.

the question should not be ambiguous but should seek a broad reply rather than be limited in scope for answer.

the question should lend itself to be written in a technical report style, in a logical sequence (beginning , middle and end), containing the applicable and

relevant technical words needed in the answer.

do not ask for drawings/sketches to support the essay.

the question must be relevant to the category and level of difficulty listed in the syllabus, e.g. a description of a typical general aviation system may not be

acceptable for a typical commercial aeroplane.

subject to obvious constraints in relation to the topic being addressed the question should have a strong bias towards the practical maintenance of a

system/component and the answer should show an understanding of normal and deteriorated conditions of an aircraft and its systems.

Variations on alternative possible answers which have not been thought of, may have to be taken into account to aid the examiner when marking. If considered

relevant, the model answer should be amended to include these new points.


e) Because of the difficulty in marking an essay answer using key points only, there is a need for the way in which the report was written to be assessed and taken into

consideration.

f) The total points for each question will add up to 100 and will need to reflect both the combination of the technical (key point) element and the report style element.

g) Each key point will be graded upon its importance and have point weighting allocated to it . The total weight will represent 60% of the mark.

h) Key points are the ‘important elements’ that may be knowledge or experience-based and will include other maintenance orientated factors such as relevant safety

precautions or legislative practices if applicable. Excessive reference to the need for MM referral or safety checks may be considered wasteful.

i) The question answer will be analysed for the clarity and manner in which the essay report is presented and have a weighting allocated to it which will represent 40% of

the mark.

j) The answer should show the candidate's ability to express himself in technical language. This includes readability of the language, basic grammar and use of

terminology.

k) The report starts in the beginning and has logical process to reach a conclusion.

l) Supporting diagrams should not be encouraged but if used should supplement the answer and not replace the need for a broad text answer.

m) The report should not be indexed, itemised or listed.

n) Within reason the candidate should not be penalised for incorrect spelling.

o) A zero mark should only be given in exceptional circumstances. Even if the student misunderstands the question and gives an answer to a different question, a

sympathetic mark even if only for the report style should be given, this could up to the maximum percentage allowed.

p) The two allocated marks should be added together and written into the answer paper.

q) If a question answer resulting in a borderline failure is principally due to “written report errors,” the paper should be discussed and the mark agreed if possible with

another examiner.


SUBPART DCONVERSION OF NATIONAL QUALIFICATIONS

This Subpart provides the requirements for converting national qualifications to aircraft maintenance licences.


66.B.300 General

a) The competent authority may only perform the conversion specified in 66. A.70 in accordance with a conversion report

prepared pursuant to paragraph 66.B.305 or 66.B.310, as applicable.

b) The conversion report shall be either developed by the competent authority or approved by the competent authority.


66.B.305 Conversion report for national qualifications

The report shall describe the scope of each type of qualification and show to which aircraft maintenance licence it will be

converted, which limitation will be added and the Part-66 module/subjects on which examination is needed to ensure

conversion to the aircraft maintenance licence without limitation, or to include an additional (sub-) category. The report shall

include a copy of the existing regulation defining the licence categories and scopes.

AMC 66.B.305 Conversion report for national qualifications

The scope of the national qualifications and the Part-66 licence should be compared on the basis of a detailed analysis of the national and Part-66 basic qualification standards.

The report should identify where a difference between the two standards exists. The report should show where such a difference would lead to a limitation on the Part-66

licence.


66.B.310 Conversion report for approved maintenance organisations authorisations

For each approved maintenance organisation concerned, the report shall describe the scope of each type of authorisation and

show to which aircraft maintenance licence it will be converted, which limitation will be added and the module/- subjects on

which examination is needed to convert to the licence, or to include an additional (sub-)category. The report shall include a

copy of the relevant approved maintenance organisation's procedures for the qualification of certifying staff, on which the

conversion process is based.

AMC 66.B.310 Conversion report for approved maintenance organisations authorisations

The scope of the approved maintenance organisation authorisation and the Part-66 licence should be compared on the basis of a detailed analysis of the Organisations

procedures defining the scope of the authorisation, the scope of work of the organisation and the aircraft type qualifications held by the individuals or groups or individuals. The

report should identify where a difference between the two scopes exists. The report should show where such a difference would lead to a limitation on the Part-66 licence.


SUBPART EEXAMINATION CREDITS

This Subpart provides the requirements for granting examination credits in accordance with 66.A.25(b).


66.B.400 General

a) The competent authority may only grant examination credit on the basis of an examination credit report prepared in

accordance with 66.B.405.

b) The examination credit report must be either developed by the competent authority or approved by the competent

authority.


66.B.405 Examination credit report

a) For each technical qualification concerned the report shall identify the subject matter and knowledge levels contained

in Appendix I to this Part relevant to the particular category being compared.

b) The report shall include a statement of compliance against each subject stating where, in the technical qualification,

the equivalent standard can be found. If there is no equivalent standard for the particular subject, the report shall state

such facts.

c) Based upon paragraph (b) comparison, the report shall indicate for each technical qualification concerned the Appendix

I subject matters subject to examination credits.

d) Where the national qualification standard is changed, the report shall be amended as necessary.


SUBPART FREVOCATION, SUSPENSION OR LIMITATIONOF THE AIRCRAFT MAINTENANCE LICENCE


66.B.500 Revocation, suspension or limitation of the aircraft maintenance licence

The competent authority shall suspend, limit or revoke the aircraft maintenance licence where it has identified a safety issue

or if it has clear evidence that the person has carried out or been involved in one or more of the following activities:

1. obtaining the aircraft maintenance licence and/or the certification privileges by falsification of submitted documentary

evidence.

2. failing to carry out requested maintenance combined with failure to report such fact to the organisation or person who

requested the maintenance.

3. failing to carry out required maintenance resulting from own inspection combined with failure to report such fact to the

organisation or person for whom the maintenance was intended to be carried out.

4. negligent maintenance.

5. falsification of the maintenance record.

6. issuing a certificate of release to service knowing that the maintenance specified on the certificate of release to service

has not been carried out or without verifying that such maintenance has been carried out.

7. carrying out maintenance or issuing a certificate of release to service when adversely affected by alcohol or drugs.

8. issuing certificate of release to service while not in compliance with this part.


Part-66 Appendix I

Basic knowledge requirements


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"3

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7 8, 8-

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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,.-


"3

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7 8, 8-


79 a`hVc XV_VcReZ`_6


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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,..


"3

CVgV]

7 8, 8-

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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,./


"3

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7 8, 8-

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"3

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7 8, 8-

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"3

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7 8, 8-

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"3

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7 8, 8-

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"3

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7 8, 8-

@_eVcacVeReZ`_ `W V_XZ_V a`hVc `feafe R_U aRcR^VeVcd6

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7 8, 8-

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8]RUV V]V^V_e eYV`cj6

?ZXY*]`h S]RUV R_X]V' cVgVcdV R_X]V' R_X]V `W ReeRT\' cèR(eZ`_R] daVVU6

GcàV]]Vc d]Za6

7VcÙj_R^ZT' TV_ecZWfXR]' R_U eYcfde W`cTVd6

K`cbfV6

IV]ReZgV RZcW]`h `_ S]RUV R_X]V `W ReeRT\6

MZScReZ`_ R_U cVd`_R_TV)

,2)- AZWXMTTMZ 4WV[\Z]K\QWV , - #

9`_decfTeZ`_ ^VeYÙd R_U ^ReVcZR]d fdVU Z_ h`ÙV_'T`â`dZeV R_U ^VeR] acàV]]Vcd6

8]RUV deReZ`_' S]RUV WRTV' S]RUV dYR_\' S]RUV SRT\ R_U YfSRddV^S]j6

=ZiVU aZeTY' T`_ec`]]RS]V aZeTY' T`_deR_e daVVUZ_XacàV]]Vc6

GcàV]]Vc*daZ__Vc Z_deR]]ReZ`_)

,2). AZWXMTTMZ AQ\KP 4WV\ZWT , - #

JaVVU T`_ec`] R_U aZeTY TYR_XV ^VeYÙd' ^VTYR_ZTR] R_UV]VTecZTR]*V]VTec`_ZT6

=VReYVcZ_X R_U cVgVcdV aZeTY6

FgVcdaVVU acèVTeZ`_)

,2)/ AZWXMTTMZ DaVKPZWVQ[QVO # - #

Jj_TYc`_ZdZ_X R_U dj_TYcàYRdZ_X VbfZa^V_e)

,2)0 AZWXMTTMZ ;KM AZW\MK\QWV , - #

=]fZU R_U V]VTecZTR] UV(ZTZ_X VbfZa^V_e)

,2)1 AZWXMTTMZ >IQV\MVIVKM , . #

JeReZT R_U Uj_R^ZT SR]R_TZ_X6

8]RUV ecRT\Z_X6

7ddVdd^V_e `W S]RUV UR^RXV' Vc`dZ`_' T`cc`dZ`_' ZâRTe

UR^RXV' UV]R^Z_ReZ`_6

GcàV]]Vc ecVRe^V_e*cVaRZc dTYV^Vd6

GcàV]]Vc V_XZ_V cf__Z_X)

,2)2 AZWXMTTMZ D\WZIOM IVL AZM[MZÎ\QWV , - #

GcàV]]Vc acVdVcgReZ`_ R_U UVacVdVcgReZ`_

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,.4


Part-66 Appendix II

Basic Examination Standard


6 8 3� Fuuj sin} � NN� �Gfxnh� J } frnsfynts� Xyfsifwi�� nx� frj sij i� fx� ktqqt| x?�

-n.� utnsy� 7 38 � nx� wj uqfhj i� g~ � ymj � ktqqt| nsl?�

�7 38 3� Xzgoj hy� R tizqj � 8 � J qj hywnhfq�Kzsifrj syfqx?�

H fyj ltw~ � F2 7 5 � rzqyn2 hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� 7 : � rnszyj x3�

H fyj ltw~ � G6 2 : 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� ; : � rnszyj x3�

H fyj ltw~ � G7 2 : 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� ; : � rnszyj x3�@�

-nn.� utnsyx� 7 36 < � fsi� 7 36 = � fwj � wj uqfhj i� g~ � ymj � ktqqt| nsl?�

�7 36 < 3� Xzgoj hy� R tizqj � 6 ; � Unxyts� J slnsj ?�

H fyj ltw~ � F2 : 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� ; : � rnszyj x3�

H fyj ltw~ � G6 2 < 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� > 5 � rnszyj x3�

H fyj ltw~ � G7 2 S tsj 3�

7 36 = 3� Xzgoj hy� R tizqj � 6 < � Uwtuj qqj w?�

H fyj ltw~ � F2 7 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� 7 : � rnszyj x3�

H fyj ltw~ � G6 2 8 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� 9 5 � rnszyj x3�

H fyj ltw~ � G7 2 S tsj 3�@�

6 9 3� Fuuj sin} � [ � nx� wj uqfhj i� g~ � ymj � ktqqt| nsl?

�Fuujsin} � [

Fuuqnhfynts� Ktwr� � � J FXF� Ktwr� 6 >

6 3� Ymnx� fuuj sin} � htsyfnsx� fs� j } fruqj � tk� ymj � ktwr� zxj i� ktw� fuuqnhfynts� ktw� ymj � fnwhwfky� rfnsyj sfshj � qnhj shj �wj kj wwj i� yt� ns� Fssj } � NNN� -Ufwy2 ; ; .3

7 3� Ymj � htruj yj sy� fzymtwny~ � tk� ymj � R j rgj w� Xyfyj � rf~ � rtink~ � ymj � J FXF� Ktwr� 6 > � tsq~ � yt� nshqzij � fiinyntsfq�nsktwrfynts� sj hj xxfw~ � yt� xzuutwy� ymj � hfxj � | mj wj � ymj � S fyntsfq� wj vznwj rj syx� uj wrny� tw� wj vznwj � ymj � fnwhwfky�rfnsyj sfshj � qnhj shj � nxxzj i� ns� fhhtwifshj � | nym� Fssj } � NNN� -Ufwy2 ; ; .� yt� gj � zxj i� tzyxnij � ymj � wj vznwj rj sy� tk�Fssj } � NN� -Ufwy2 6 9 : .� ktw� sts2htrrj whnfq� fnw� ywfsxutwy� uzwutxj x3

foQ� 9 5 4 9 5 � T kknhnfq�Otzwsfq�tk�ymj �J zwtuj fs�Z snts� 6 8 37 37 5 6 5


"3

3\\QZPUc <<

3I[QK 6ÌUQVI\QWV D\IVLIZL

,) JeR_URcUZdReZ`_ 8RdZd =`c <iR^Z_ReZ`_d

,),) 7]] SRdZT ViR^Z_ReZ`_d ^fde SV TRccZVU `fe fdZ_X eYV ^f]eZ(TY`ZTVbfVdeZ`_ W`c^Re R_U VddRj bfVdeZ`_d Rd daVTZWZVU SV]`h)

,)-) <RTY ^f]eZ(TY`ZTV bfVdeZ`_ ^fde YRgV eYcVV R]eVc_ReZgV R_dhVcd `W hYZTY`_]j `_V ^fde SV eYV T`ccVTe R_dhVc R_U eYV TR_UZUReV ^fde SV R]]`hVU R

eZ^V aVc ^Ùf]V hYZTY Zd SRdVU fa`_ R _`^Z_R] RgVcRXV `W 20 dVT`_UdaVc bfVdeZ`_)

,).) <RTY VddRj bfVdeZ`_ cVbfZcVd eYV acVaRcReZ`_ `W R hcZeeV_ R_dhVc R_U eYVTR_UZUReV ^fde SV R]]`hVU -+ ^Z_feVd e` R_dhVc VRTY dfTY bfVdeZ`_)

,)/) JfZeRS]V VddRj bfVdeZ`_d ^fde SV UcRWeVU R_U VgR]fReVU fdZ_X eYV

\_`h]VUXV dj]]RSfd Z_ GRce(11 7aaV_UZi @ DÙf]Vd 2' 4 R_U ,+)

,)0) <RTY bfVdeZ`_ hZ]] YRgV R ^ÙV] R_dhVc UcRWeVU W`c Ze' hYZTY hZ]] R]d`Z_T]fUV R_j \_`h_ R]eVc_ReZgV R_dhVcd eYRe ^Rj SV cV]VgR_e W`c èYVcdfSUZgZdZ`_d)

,)1) KYV ^ÙV] R_dhVc hZ]] R]d` SV Sc`\V_ U`h_ Z_e` R ]Zde `W eYV Zâ`ceR_ea`Z_ed \_`h_ Rd BVj G`Z_ed)

,)2) KYV aRdd ^Rc\ W`c VRTY GRce(11 ^Ùf]V R_U dfS(^Ùf]V ^f]eZ(TY`ZTVaRce `W eYV ViR^Z_ReZ`_ Zd 20 !)

,)3) KYV aRdd ^Rc\ W`c VRTY VddRj bfVdeZ`_ Zd 20 ! Z_ eYRe eYV TR_UZUReVdR_dhVc ^fde T`_eRZ_ 20 ! `W eYV cVbfZcVU \Vj a`Z_ed RUUcVddVU Sj eYVbfVdeZ`_ R_U _` dZX_ZWZTR_e Vcc`c cV]ReVU e` R_j cVbfZcVU \Vj a`Z_e)

,)4) @W VZeYVc eYV ^f]eZ(TY`ZTV aRce `_]j `c eYV VddRj aRce `_]j Zd WRZ]VU' eYV_ ZeZd `_]j _VTVddRcj e` cVeR\V eYV ^f]eZ(TY`ZTV `c VddRj aRce' Rd RaacàcZReV)

,),+) GV_R]ej ^Rc\Z_X djdeV^d ^fde _è SV fdVU e` UVeVc^Z_V hYVeYVc RTR_UZUReV YRd aRddVU)

,),,) 7]] GRce(11 ^Ùf]Vd eYRe ^R\V fa R T`â]VeV GRce(11 RZcTcRWe ^RZ_(eV_R_TV ]ZTV_TV TReVX`cj `c dfSTReVX`cj ^fde SV aRddVU hZeYZ_ R 0jVRc eZ^V aVcZÙ `W aRddZ_X eYV WZcde ^Ùf]V ViTVae Z_ eYV TRdV

daVTZWZVU Z_ aRcRXcRaY ,),-) 7 WRZ]VU ^Ùf]V ^Rj _è SV cVeR\V_ W`cRe ]VRde 4+ URjd W`]]`hZ_X eYV UReV `W eYV WRZ]VU ^Ùf]V ViR^Z_ReZ`_'ViTVae Z_ eYV TRdV `W R GRce(,/2 Raac`gVU ^RZ_eV_R_TV ecRZ_Z_X `cXR_Z(

dReZ`_ hYZTY T`_UfTed R T`fcdV `W cVecRZ_Z_X eRZ]`cVU e` eYV WRZ]VUdfS[VTed Z_ eYV aRceZTf]Rc ^Ùf]V hYV_ eYV WRZ]VU ^Ùf]V ^Rj SVcVeR\V_ RWeVc .+ URjd)

,),-) KYV 0 jVRc eZ^V aVcZÙ daVTZWZVU Z_ aRcRXcRaY ,),, U`Vd _è Raa]j eèY`dV ^Ùf]Vd hYZTY RcV T`^^`_ e` ^`cV eYR_ `_V GRce(11 RZcTcRWe^RZ_eV_R_TV ]ZTV_TV TReVX`cj `c dfSTReVX`cj R_U hYZTY hVcV acVgZ`fd]jaRddVU Rd aRce `W R_èYVc dfTY TReVX`cj `c dfSTReVX`cj ViR^Z_ReZ`_)

-) HfVdeZ`_ Ef^SVcd W`c eYV GRce(11 7aaV_UZi @ DÙf]Vd

-),) JfS[VTe DÙf]V , DReYV^ReZTd5

9ReVX`cj 7(,1 ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-+ ^Z_feVd)

9ReVX`cj 8,(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU

/+ ^Z_feVd)

9ReVX`cj 8-(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU/+ ^Z_feVd)

-)-) JfS[VTe DÙf]V - GYjdZTd5

9ReVX`cj 7(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU/+ ^Z_feVd)

9ReVX`cj 8,(0+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU

10 ^Z_feVd)

9ReVX`cj 8-(0+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU10 ^Z_feVd)

-).) JfS[VTe DÙf]V . <]VTecZTR] =f_UR^V_eR]d5

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/+


"3

9ReVX`cj 7( + ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-0 ^Z_feVd)

9ReVX`cj 8,(0+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU10 ^Z_feVd)


-)/) JfS[VTe DÙf]V / <]VTec`_ZT =f_UR^V_eR]d5

9ReVX`cj 7(E`_V)

9ReVX`cj 8,(-+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU

-0 ^Z_feVd)

9ReVX`cj 8-(/+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU0+ ^Z_feVd)

-)0) JfS[VTe DÙf]V 0 ;ZXZeR] KVTY_ZbfVd*<]VTec`_ZT @_decf^V_e JjdeV^d5

9ReVX`cj 7(,1 ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-+ ^Z_feVd)

9ReVX`cj 8,), " 8,).(/+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^VR]]`hVU 0+ ^Z_feVd)

9ReVX`cj 8,)- " 8,)/(-+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^VR]]`hVU -0 ^Z_feVd)

9ReVX`cj 8-(2+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU4+ ^Z_feVd)

-)1) JfS[VTe DÙf]V 1 DReVcZR]d R_U ?RcUhRcV5

9ReVX`cj 7(0+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU10 ^Z_feVd)

9ReVX`cj 8,(2+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU4+ ^Z_feVd)


-)2) JfS[VTe DÙf]V 2 DRZ_eV_R_TV GcRTeZTVd5

9ReVX`cj 7(2+ ^f]eZ(TY`ZTV R_U - VddRj bfVdeZ`_d) KZ^V R]]`hVU4+ ^Z_feVd a]fd /+ ^Z_feVd)

9ReVX`cj 8,(3+ ^f]eZ(TY`ZTV R_U - VddRj bfVdeZ`_d) KZ^V R]]`hVU,++ ^Z_feVd a]fd /+ ^Z_feVd)

9ReVX`cj 8-(1+ ^f]eZ(TY`ZTV R_U - VddRj bfVdeZ`_d) KZ^V R]]`hVU20 ^Z_feVd a]fd /+ ^Z_feVd)

-)3) JfS[VTe DÙf]V 3 8RdZT 7VcÙj_R^ZTd5

9ReVX`cj 7(-+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-0 ^Z_feVd)

9ReVX`cj 8,(-+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-0 ^Z_feVd)

9ReVX`cj 8-(-+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-0 ^Z_feVd)

-)4) JfS[VTe DÙf]V 4 ?f^R_ WRTe`cd5

9ReVX`cj 7(-+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU-0 ^Z_feVd a]fd -+ ^Z_feVd)

9ReVX`cj 8,(-+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU-0 ^Z_feVd a]fd -+ ^Z_feVd)

9ReVX`cj 8-(-+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU-0 ^Z_feVd a]fd -+ ^Z_feVd)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/,


"3

-),+) JfS[VTe DÙf]V ,+ 7gZReZ`_ CVXZd]ReZ`_5

9ReVX`cj 7(.+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU/+ ^Z_feVd a]fd -+ ^Z_feVd)

9ReVX`cj 8,(/+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU0+ ^Z_feVd a]fd -+ ^Z_feVd)

9ReVX`cj 8-(/+ ^f]eZ(TY`ZTV R_U , VddRj bfVdeZ`_) KZ^V R]]`hVU0+ ^Z_feVd a]fd -+ ^Z_feVd)

-),,) JfS[VTe DÙf]V ,,R KfcSZ_V 7Vcà]R_V 7VcÙj_R^ZTd' JecfTefcVd R_UJjdeV^d5

9ReVX`cj 7(,++ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,-0 ^Z_feVd)

9ReVX`cj 8,(,.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,10 ^Z_feVd)

9ReVX`cj 8-(E`_V)

-),-) JfS[VTe DÙf]V ,,S GZde`_ 7Vcà]R_V 7VcÙj_R^ZTd' JecfTefcVd R_UJjdeV^d5

9ReVX`cj 7(2+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU4+ ^Z_feVd)

9ReVX`cj 8,(,++ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,-0 ^Z_feVd)

9ReVX`cj 8-(E`_V)

-),.) JfS[VTe DÙf]V ,- ?V]ZTàeVc 7VcÙj_R^ZTd' JecfTefcVd R_U JjdeV^d5

9ReVX`cj 7(4+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,,0 ^Z_feVd)

9ReVX`cj 8,(,,0 ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,/0 ^Z_feVd)

9ReVX`cj 8-(E`_V)

-),/) JfS[VTe DÙf]V ,. 7ZcTcRWe 7VcÙj_R^ZTd' JecfTefcVd R_U JjdeV^d5

9ReVX`cj 7(E`_V)

9ReVX`cj 8,(E`_V)

9ReVX`cj 8-(,.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU,10 ^Z_feVd)

-),0) JfS[VTe DÙf]V ,/ Gcàf]dZ`_5

9ReVX`cj 7(E`_V)

9ReVX`cj 8,(E`_V)

9ReVX`cj 8-(-0 ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU.+ ^Z_feVd)

-),1) JfS[VTe DÙf]V ,0 >Rd KfcSZ_V <_XZ_V5

9ReVX`cj 7(1+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU20 ^Z_feVd)

9ReVX`cj 8,(4+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU

,,0 ^Z_feVd)

9ReVX`cj 8-(E`_V)

-),2) JfS[VTe DÙf]V ,1 GZde`_ <_XZ_V5

9ReVX`cj 7(+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU

10 ^Z_feVd)

9ReVX`cj 8,(+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU4+ ^Z_feVd)

9ReVX`cj 8-(E`_V)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/-


"3

-),3) JfS[VTe DÙf]V ,2 GcàV]]Vc5

9ReVX`cj 7(+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU-0 ^Z_feVd)

9ReVX`cj 8,(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU/+ ^Z_feVd)

9ReVX`cj 8-(E`_V)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/.


Part-66 Appendix III

Type Training and Examination Standard


"3

3\\QZPUc <<<

EaXM \ZIQVQVO IVL 6ÌUQVI\QWV D\IVLIZL

,) Gd\Q _]MUZUZS XQaQX^

KYV eYcVV ]VgV]d ]ZdeVU SV]`h UVWZ_V eYV `S[VTeZgVd eYRe R aRceZTf]Rc ]VgV] `WecRZ_Z_X Zd Z_eV_UVU e` RTYZVgV)

C V g V ] , > V _ V c R ] W R ^ Z ] Z R c Z d R e Z ` _

7 ScZVW `gVcgZVh `W eYV RZcWcR^V' djdeV^d R_U a`hVca]R_ed Rd `fe]Z_VU Z_eYV JjdeV^d ;VdTcZaeZ`_ JVTeZ`_ `W eYV 7ZcTcRWe DRZ_eV_R_TV DR_fR])

,) 9`fcdV `S[VTeZgVd5 La`_ T`â]VeZ`_ `W eYV T`fcdV' eYV defUV_e hZ]] SVRS]V e` ZUV_eZWj dRWVej acVTRfeZ`_d cV]ReVU e` eYV RZcWcR^V' Zed djdeV^d R_Ua`hVca]R_e

-) @UV_eZWj ^RZ_eV_R_TV acRTeZTVd Zâ`ceR_e e` eYV RZcWcR^V' Zed djdeV^d R_Ua`hVca]R_e

.) ;VWZ_V eYV XV_VcR] ]Rj`fe `W eYV RZcTcRWe#d ^R[`c djdeV^d

/) ;VWZ_V eYV XV_VcR] ]Rj`fe R_U TYRcRTeVcZdeZTd `W eYV a`hVca]R_e

0) @UV_eZWj daVTZR] e``]Z_X R_U eVde VbfZa^V_e fdVU hZeY eYV RZcTcRWe

C V g V ] - IR ^ a R _ U e c R _ d Z e

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9`fcdV `S[VTeZgVd5 @_ RUUZeZ`_ e` eYV Z_W`c^ReZ`_ T`_eRZ_VU Z_ eYV CVgV] ,>V_VcR] =R^Z]ZRcZdReZ`_ T`fcdV' Re eYV T`â]VeZ`_ `W eYZd CVgV] - IRâ R_UKcR_dZe ecRZ_Z_X' eYV defUV_e hZ]] SV RS]V e`5

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.) ;VdTcZSV djdeV^d R_U RZcTcRWe YR_U]Z_X aRceZTf]Rc]j RTTVdd' a`hVc RgRZ](

RSZ]Zej R_U d`fcTVd)

/) @UV_eZWj eYV ]`TReZ`_d `W eYV acZ_TZaR] T`â`_V_ed)

0) <ia]RZ_ eYV _`c^R] Wf_TeZ`_Z_X `W VRTY ^R[`c djdeV^' Z_T]fUZ_X eVc^Z(

_`]`Xj R_U _`^V_T]RefcV)

1) GVcW`c^ eYV ac`TVUfcVd W`c cRâ R_U ecR_dZe dVcgZTZ_X Rdd`TZReVU hZeYeYV RZcTcRWe W`c eYV W`]]`hZ_X djdeV^d5 =fV]' G`hVc G]R_ed' ?jUcRf]ZTd'CR_UZ_X >VRc' NReVc*NRdeV' FijXV_)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,//


"3

2) ;V^`_decReV ac`WZTZV_Tj Z_ fdV `W TcVh cVa`ced R_U `_(S`RcU cVa`ceZ_XdjdeV^d $^Z_`c ec`fS]VdY`èZ_X% R_U UVeVc^Z_V RZcTcRWe RZch`ceYZ_Vdd aVceYV D<C*9;C)

3) @UV_eZWj R_U fdV RaacàcZReV U`Tf^V_eReZ`_)

4) C`TReV eY`dV ac`TVUfcVd W`c cVa]RTV^V_e `W T`â`_V_ed W`c cRâ R_UecR_dZe RTeZgZeZVd ZUV_eZWZVU Z_ `S[VTeZgV -)

C V g V ] . C Z _ V R _ U S R d V ^ R Z _ e V _ R _ T V e c R Z _ Z _ X

;VeRZ]VU UVdTcZaeZ`_' àVcReZ`_' T`â`_V_e ]`TReZ`_' cV^`gR]*Z_deR]]ReZ`_R_U SZeV R_U ec`fS]VdY`èZ_X ac`TVUfcVd e` ^RZ_eV_R_TV ^R_fR] ]VgV])

9`fcdV `S[VTeZgVd5 @_ RUUZeZ`_ e` eYV Z_W`c^ReZ`_ T`_eRZ_VU Z_ CVgV] , R_UCVgV] - ecRZ_Z_X' Re eYV T`â]VeZ`_ `W CVgV] @@@ CZ_V R_U 8RdV DRZ_eV_R_TVecRZ_Z_X' eYV defUV_e hZ]] SV RS]V e`5

$R% GVcW`c^ djdeV^' V_XZ_V' T`â`_V_e R_U Wf_TeZ`_R] TYVT\d Rd daVTZWZVUZ_ eYV ^RZ_eV_R_TV ^R_fR])

$S% 9`ccV]ReV Z_W`c^ReZ`_ W`c eYV afca`dV `W ^R\Z_X UVTZdZ`_d Z_ cVdaVTe `WWRf]e UZRX_`dZd R_U cVTeZWZTReZ`_ e` ^RZ_eV_R_TV ^R_fR] ]VgV])

$T% ;VdTcZSV ac`TVUfcVd W`c cVa]RTV^V_e `W T`â`_V_ed f_ZbfV e` RZcTcRWeejaV)

-) Gd\Q _]MUZUZS ^_MZPM]P

KjaV ecRZ_Z_X ^fde Z_T]fUV R eYV`cVeZTR] R_U acRTeZTR] V]V^V_e)

-),) K Y V ` c V e Z T R ] V ] V ^ V _ e

7d R ^Z_Z^f^ eYV V]V^V_ed Z_ eYV Jj]]RSfd SV]`h eYRe RcV daVTZWZT e` eYVRZcTcRWe ejaV ^fde SV T`gVcVU) 7UUZeZ`_R] V]V^V_ed Z_ecÙfTVU UfV e` eVTY(_`]`XZTR] TYR_XVd dYR]] R]d` SV Z_T]fUVU)

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CVgV]]Z_X R_U hVZXYZ_X

K`hZ_X R_U eRiZZ_X

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JVcgZTZ_X

JeR_URcU acRTeZTVd(`_]j ejaV aRceZTf]Rc

8- ^Ùf]V(dRWVej ZeV^d*^VTYR_ZTR] Z_eVcWRTV

8, ^Ùf]V(dRWVej ZeV^d*RgZ`_ZTd Z_eVcWRTV

7Vcà]R_Vd

efcSZ_V

7Vcà]R_Vd

aZde`_

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aZde`_

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8, 9 8, 9 8, 9 8, 9 8-

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7ZcWcR^V JecfTefcV . , . , # # # # ,

=fdV]RXV ;``cd . , . , # # # # #

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/0


"3

7Vcà]R_Vd

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efcSZ_V

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aZde`_

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8, 9 8, 9 8, 9 8, 9 8-

=fdV]RXV . , . , # # # # #

=fdV]RXV NZ_U`hd . , . , # # # # #

NZ_Xd . , . , # # # # #

JeRSZ]ZdVcd . , . , # # # # #

=]ZXYe 9`_ec`] JfcWRTVd . , . , # # # # #

ERTV]]Vd*Gj]`_d . , . , # # # # #

Q`_R] " JeReZ`_ @UV_eZWZTReZ`_ JjdeV^d , , , , , , , , ,

7Zc Jfaa]j . , . , . , . , ,

7Zc 9`_UZeZ`_Z_X . , . , . , . , ,

GcVddfcZdReZ`_ . , # # # # # # ,

JRWVej " NRc_Z_X ;VgZTVd . , # # # # # # ,

@_decf^V_e JjdeV^d . , . , . , . , .

7gZ`_ZTd JjdeV^d - , - , - , - , .

<]VTecZTR] G`hVc . , . , . , . , .

<bfZa^V_e " =fc_ZdYZ_Xd . , . , . , . , #

<]VTec`_ZT <^VcXV_Tj <bfZa) IVbfZc) "9RSZ_ <_eVceRZ_^V_e <bfZa^V_e

# , # # # # # # .

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Jjd) FaVcReZ`_5 <]VTecZTR]*=]j(Sj(NZcV . , # # # # # # .

=fV] JjdeV^d . , . , . , . , ,

?jUcRf]ZT G`hVc . , . , . , . , ,

@TV " IRZ_ GcèVTeZ`_ . , . , . , . , ,

CR_UZ_X >VRc . , . , . , . , ,

CZXYed . , . , . , . , .

FijXV_ . , . , # # # # ,

G_Vf^ReZT*MRTff^ . , . , . , . , ,

NReVc*NRdeV . , . , # # # # ,

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<_XZ_V GVcW`c^R_TV . , # # . , # # ,

@_]Ve . , # # . , # # #

9`âcVdd`cd . , # # . , # # #

9`^SfdeZ`_ JVTeZ`_ . , # # . , # # #

KfcSZ_V JVTeZ`_ . , # # . , # # #

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/1


"3

7Vcà]R_Vd

efcSZ_V

7Vcà]R_Vd

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8, 9 8, 9 8, 9 8, 9 8-

<iYRfde . , # # . , # # #

8VRcZ_Xd R_U JVR]d . , # # . , # # #

CfScZTR_ed R_U =fV]d . , # # . , # # #

CfScZTReZ`_ JjdeV^d . , # # . , # # #

=fV] JjdeV^d . , # # . , # # ,

<_XZ_V T`_ec`]d . , # # . , # # ,

=7;<9 - , # # - , # # .

7Zc JjdeV^d . , # # . , # # #

JeRceZ_X " @X_ZeZ`_ JjdeV^d . , # # . , # # #

<_XZ_V @_UZTReZ_X JjdeV^d . , # # . , # # .

G`hVc 7fX^V_eReZ`_ JjdeV^d . , # # # # # # #

KfcS`(acà <_XZ_Vd . , # # # # # # #

KfcS`(dYRWe <_XZ_Vd # # # # . , # # #

7fiZ]ZRcj G`hVc L_Zed $7GLd% . , # # # # # # ,

G`hVca]R_e @_deR]]ReZ`_ . , # # . , # # #

=ZcV GcèVTeZ`_ JjdeV^d . , # # . , # # ,

<_XZ_V D`_Ze`cZ_X R_U >c`f_U FaVcReZ`_ . , # # . , # # #

<_XZ_V Je`cRXV R_U GcVdVcgReZ`_ . , # # . , # # #

CU^_[Z 7ZSUZQ^2

<_XZ_V GVcW`c^R_TV # # . , # # . , ,

<_XZ_V 9`_decfTeZ`_ # # . , # # . , ,

<_XZ_V =fV] JjdeV^d # # . , # # . , ,

9RcSfcVee`cd # # . , # # . , #

=fV] Z_[VTeZ`_ djdeV^d # # . , # # . , #

<_XZ_V T`_ec`]d . , # # . , # # ,

=7;<9 # # - , # # - , .

JeRceZ_X R_U @X_ZeZ`_ JjdeV^d # # . , # # . , #

@_UfTeZ`_' <iYRfde R_U 9``]Z_X JjdeV^d # # . , # # . , #

JfaVcTYRcXZ_X*KfcS`TYRcXZ_X # # . , # # . , #

CfScZTR_ed R_U =fV]d # # . , # # . , #

CfScZTReZ`_ JjdeV^d # # . , # # . , #

<_XZ_V @_UZTReZ`_ JjdeV^d # # . , # # . , .

G`hVca]R_e @_deR]]ReZ`_ # # . , # # . , #

<_XZ_V D`_Ze`cZ_X R_U >c`f_U FaVcReZ`_ # # . , # # . , #

<_XZ_V Je`cRXV R_U GcVdVcgReZ`_ # # . , # # . , #

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/2


"3

7Vcà]R_Vd

efcSZ_V

7Vcà]R_Vd

aZde`_

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8, 9 8, 9 8, 9 8, 9 8-

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GcàV]]Vc # >V_VcR] . , . , # # # # ,

GcàV]]Vc 9`_decfTeZ`_ . , . , # # # # #

GcàV]]Vc GZeTY 9`_ec`] . , . , # # # # #

GcàV]]Vc Jj_TYc`_ZdZ_X . , . , # # # # #

GcàV]]Vc <]VTec`_ZT T`_ec`] - , - , # # # # .

GcàV]]Vc @TV GcèVTeZ`_ . , . , # # # # #

GcàV]]Vc DRZ_eV_R_TV . , . , # # # # #

-)-) G c R T e Z T R ] V ] V ^ V _ e

KYV acRTeZTR] ecRZ_Z_X V]V^V_e ^fde T`_dZde `W eYV aVcW`c^R_TV `W cVacVdV_(eReZgV ^RZ_eV_R_TV eRd\d R_U eYVZc RddVdd^V_e' Z_ `cUVc e` ^VVe eYVW`]]`hZ_X `S[VTeZgVd5

$R% <_dfcV dRWV aVcW`c^R_TV `W ^RZ_eV_R_TV' Z_daVTeZ`_d R_U c`feZ_V h`c\RTT`cUZ_X e` eYV ^RZ_eV_R_TV ^R_fR] R_U èYVc cV]VgR_e Z_decfTeZ`_dR_U eRd\d Rd RaacàcZReV W`c eYV ejaV `W RZcTcRWe' W`c ViRâ]V ec`fS]V(dY`èZ_X' cVaRZcd' RU[fde^V_ed' cVa]RTV^V_ed' cZXXZ_X R_U Wf_TeZ`_R]TYVT\d dfTY Rd V_XZ_V cf_' VeT' ZW cVbfZcVU)

$S% 9`ccVTe]j fdV R]] eVTY_ZTR] ]ZeVcRefcV R_U U`Tf^V_eReZ`_ W`c eYV RZcTcRWe)

$T% 9`ccVTe]j fdV daVTZR]Zde*daVTZR] e``]Z_X R_U eVde VbfZa^V_e' aVcW`c^cV^`gR] R_U cVa]RTV^V_e `W T`â`_V_ed R_U ^Ùf]Vd f_ZbfV e` ejaV'Z_T]fUZ_X R_j `_(hZ_X ^RZ_eV_R_TV RTeZgZej)

.) Gd\Q _]MUZUZS QcMYUZM_U[Z ^_MZPM]P

NYVcV RZcTcRWe ejaV ecRZ_Z_X Zd cVbfZcVU' eYV ViR^Z_ReZ`_ ^fde SV hcZeeV_R_U T`â]j hZeY eYV W`]]`hZ_X5

,) =`c^Re `W eYV ViR^Z_ReZ`_ Zd `W eYV ^f]eZa]V(TY`ZTV ejaV) <RTY ^f]eZa]V(TY`ZTV bfVdeZ`_ ^fde YRgV eYcVV R]eVc_ReZgV R_dhVcd `W hYZTY `_]j `_V^fde SV eYV T`ccVTe R_dhVc) KYV eZ^V W`c R_dhVcZ_X Zd SRdVU fa`_ R_`^Z_R] RgVcRXV `W ,-+ dVT`_Ud aVc ]VgV] . bfVdeZ`_ R_U 20 dVT`_Ud aVc]VgV] , `c - bfVdeZ`_)

-) KYV ViR^Z_ReZ`_ ^fde SV `W eYV T]`dVU S``\ ejaV) E` cVWVcV_TV ^ReVcZR]Zd aVc^ZeeVU) 7_ ViTVaeZ`_ hZ]] SV ^RUV W`c eYV TRdV `W ViR^Z_Z_X R 8,`c 8- TR_UZUReV#d RSZ]Zej e` Z_eVcacVe eVTY_ZTR] U`Tf^V_ed)

.) KYV _f^SVc `W bfVdeZ`_d ^fde SV Re ]VRde `_V bfVdeZ`_ aVc Y`fc `WZ_decfTeZ`_ dfS[VTe e` R ^Z_Z^f^ `W eh` bfVdeZ`_d aVc Jj]]RSfddfS[VTe) KYV T`âVeV_e RfeY`cZej `W eYV DV^SVc JeReV hZ]] RddVdd_f^SVc R_U ]VgV] `W bfVdeZ`_d `_ R dRâ]Z_X SRdZd hYV_ Raac`gZ_XeYV T`fcdV)

/) KYV ViR^Z_ReZ`_ aRdd ^Rc\ Zd 20 !)

0) GV_R]ej ^Rc\Z_X Zd _è e` SV fdVU e` UVeVc^Z_V hYVeYVc R TR_UZUReV YRdaRddVU)

1) <_U `W ^Ùf]V aYRdV ViR^Z_ReZ`_d TR__è SV fdVU Rd aRce `W eYV WZ_R]ViR^Z_ReZ`_ f_]Vdd eYVj T`_eRZ_ eYV T`ccVTe _f^SVc R_U ]VgV] `WbfVdeZ`_d cVbfZcVU)

/) Gd\Q QcMYUZM_U[Z ^_MZPM]P

NYVcV ejaV ecRZ_Z_X Zd _è cVbfZcVU' eYV ViR^Z_ReZ`_ ^fde SV `cR]' hcZeeV_ `cacRTeZTR] RddVdd^V_e SRdVU' `c R T`^SZ_ReZ`_ eYVcV`W)

FcR] ViR^Z_ReZ`_ bfVdeZ`_d ^fde SV àV_)

NcZeeV_ ViR^Z_ReZ`_ bfVdeZ`_d ^fde SV VddRj ejaV `c ^f]eZa]V(TY`ZTVbfVdeZ`_d)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/3


"3

GcRTeZTR] RddVdd^V_e ^fde UVeVc^Z_V R aVcd`_#d T`âVeV_TV e` aVcW`c^ ReRd\)

<iR^Z_ReZ`_ dfS[VTed ^fde SV `_ R dRâ]V `W dfS[VTed UcRh_ Wc`âRcRXcRaY - ejaV ecRZ_Z_X*ViR^Z_ReZ`_ dj]]RSfd' Re eYV Z_UZTReVU ]VgV])

KYV ViR^Z_ReZ`_ ^fde V_dfcV eYRe eYV W`]]`hZ_X `S[VTeZgVd RcV ^Ve5

$R% GcàVc]j UZdTfdd hZeY T`_WZUV_TV eYV RZcTcRWe R_U Zed djdeV^d)

$S% <_dfcV dRWV aVcW`c^R_TV `W ^RZ_eV_R_TV' Z_daVTeZ`_d R_U c`feZ_V h`c\RTT`cUZ_X e` eYV ^RZ_eV_R_TV ^R_fR] R_U èYVc cV]VgR_e Z_decfTeZ`_dR_U eRd\d Rd RaacàcZReV W`c eYV ejaV `W RZcTcRWe' W`c ViRâ]V ec`fS]V(dY`èZ_X' cVaRZcd' RU[fde^V_ed' cVa]RTV^V_ed' cZXXZ_X R_U Wf_TeZ`_R]TYVT\d dfTY Rd V_XZ_V cf_' VeT' ZW cVbfZcVU)

$T% 9`ccVTe]j fdV R]] eVTY_ZTR] ]ZeVcRefcV R_U U`Tf^V_eReZ`_ W`c eYV RZcTcRWe)

$U% 9`ccVTe]j fdV daVTZR]Zde*daVTZR] e``]Z_X R_U eVde VbfZa^V_e' aVcW`c^cV^`gR] R_U cVa]RTV^V_e `W T`â`_V_ed R_U ^Ùf]Vd f_ZbfV e` ejaV'Z_T]fUZ_X R_j `_(hZ_X ^RZ_eV_R_TV RTeZgZej)

7 hcZeeV_ cVa`ce ^fde SV ^RUV Sj eYV ViR^Z_Vc e` Via]RZ_ hYj eYVTR_UZUReV YRd aRddVU `c WRZ]VU)

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,/4


Part-66 Appendix IV

Experience requirement for extending a part-66 Aircraft maintenance licence


"3

3\\QZPUc <I

6`XMZQMVKM ZMY]QZMUMV\[ NWZ M`\MVLQVO I AIZ\%.. 2QZKZIN\ >IQV\MVIVKM=QKMVKM

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KYV ViaVcZV_TV ^fde SV acRTeZTR] ^RZ_eV_R_TV ViaVcZV_TV `_ àVcReZ_X RZcTcRWe Z_eYV dfSTReVX`cj cV]VgR_e e` eYV Raa]ZTReZ`_)

KYV ViaVcZV_TV cVbfZcV^V_e hZ]] SV cVUfTVU Sj 0+ ! ZW eYV Raa]ZTR_e YRdT`â]VeVU R_ Raac`gVU GRce(,/2 T`fcdV cV]VgR_e e` eYV dfSTReVX`cj)

K`5

=c`^57, 7- 7. 7/ 8,), 8,)- 8,). 8,)/ 8-

7, 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd - jVRcd 1 ^`_eYd - jVRcd , jVRc - jVRcd

7- 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd - jVRcd 1 ^`_eYd - jVRcd , jVRc - jVRcd

7. 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd - jVRcd , jVRc - jVRcd 1 ^`_eYd - jVRcd

7/ 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd - jVRcd , jVRc - jVRcd 1 ^`_eYd - jVRcd

8,), E`_V 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd , jVRc

8,)- 1 ^`_eYd E`_V 1 ^`_eYd 1 ^`_eYd - jVRcd - jVRcd 1 ^`_eYd - jVRcd

8,). 1 ^`_eYd 1 ^`_eYd E`_V 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd , jVRc

8,)/ 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd E`_V - jVRcd 1 ^`_eYd - jVRcd - jVRcd

8- 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd 1 ^`_eYd , jVRc , jVRc , jVRc , jVRc

-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,0+


Part-66 Appendix V

Application Form an Example of Licence Format


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Part-66 Appendix VI

Aircraft Maintenance Licence referred to in Annex III (Part-66)


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AMC-66 Appendix I

Aircraft type ratings for Part-66 aircraft Maintenance licence


APPENDIX I AIRCRAFT TYPE RATINGS

FOR PART-66 AIRCRAFT MAINTENANCE LICENCE The following aircraft type ratings should be used to ensure a common standard throughout the Member States. 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 and its Implementing Rules Regulation 1702/2003, this list is only intended for the maintenance purposes. In order to keep this list current and type ratings consistent, such information should be first passed on to the Agency at [email protected] in case a Member State needs to issue a type rating that is not included in this list. Notes: Note 1. For aeroplanes in lists 1 and 2, and helicopters in lists 11, 12 and 13, the table of Appendix I include 3 columns:

o column 1: TC holder designation o column 2: aircraft model and, when available, the aircraft commercial designation, o column 3: aircraft designation for endorsement on the Part-66 licence.

Only the designations in column 3 should be used for endorsing ratings on Part-66 licences. In the tables of the remaining lists 3 to 10 the TC holder designation is added. Note 2. When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the AML licences may be modified at next renewal or when the licence is re-issued. 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 Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for type examinations and group ratings

6 Aeroplane single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings

7 Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for type examinations and group ratings

8 Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE-WS), eligible for type examinations and group ratings


mailto:[email protected]

9 Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for

type examinations and group ratings

10 Aeroplane 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 engines (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 ratings in column 3 should be used for endorsing individual type ratings on Part-66 licences.

Note: aircraft STC data are not included in this table.


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

N 262 A Frégate

N 262 B Frégate

AIRBUS

N 262 C Frégate

Nord 262 (Turbomeca Bastan)

SN 601 Corvette Aerospatiale SSN-601 (PWC JT15D)

A300 B1

A300 B2-1A

A300 B2-1C

A300 B2K-3C

A300 B2-202

A300 B2-203

A300 B4-2C

A300 B4-102

A300 B4-103

A300 B4-203

A300 C4-203

A300 F4-203

Airbus A300 basic model (GE CF6)

A300 B2-320

A300 B4-120

A300 B4-220

Airbus A300 basic model (PW JT9D)

A300 B4-601

A300 B4-603

A300 B4-605 R

A300 F4-605 R

A300 C4-605 R Variant F

Airbus A300-600 (GE CF6)

A300 B4-622

A300 B4-622 R

A300 F4-622 R

Airbus A300-600 (PW 4000)

A300 B4-620

A300 C4-620

Airbus A300-600 (PW JT9D)

A310-304

A310-308

A310-203

A310-221

A310-203 C

Airbus A310 (GE CF6)

A310-324

A310-325

A310-322

AIRBUS

A310-222

Airbus A310 (PW 4000)


3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial

Designation

A310-204

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 (IAE 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 RB 211 Trent 700)

A340-210 series

A340-310 series

Airbus A340 (CFM56)

A340-540 series

A340-640 series

Airbus A340 (RR RB 211 Trent 500)

A380-840 series Airbus A380 (RR RB 211 Trent 900)

A380-860 series Airbus A380 (EA GP7200)

AIRBUS

A300F4-608ST Beluga Airbus A300-600ST (GE CF6) One-Eleven 200 series

One-Eleven 300 series


AIRBUS


Airbus UK (BAC) 1-11 (RRD Spey)

L-410 M/UVP

L-410 UVP-E

L-410 UVP-E9

AIRCRAFT INDUSTRIES

L-410 UVP-E20

Turbolet Let L-410 (Walter M601)



Designation

L-410 UVP-E20 CARGO

L-410 UVP-E-LW

L-410 UVP-LW

L-420 Let L-420 (Walter M601)

ALENIA AERONAUTICA

C-27J Alenia C-27 (Allison/RR AE2100)

AN-26 ANTONOV

AN-26B

Antonov AN26 (Ivchenko AI-24)

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 72-211

ATR 72-212

ATR 72-100/200 series (PWC PW120)

ATR 42-400

ATR 42-500 42-500

ATR 42-500 42-600

ATR 72-212 A 72-500

ATR-GIE Avions de Transport Régional

ATR 72-212 A 72-600

ATR 42-400/500/72-212A (PWC PW120)

BAe 146 Series 100 BAE SYSTEMS

BAe 146 Series 200

BAe 146/ AVRO 146-RJ (Honeywell ALF500 Series)



Designation

BAe 146 Series 300

AVRO 146-RJ70

AVRO 146-RJ85

AVRO 146-RJ100

AVRO 146-RJ115

HS.748 Series 1

HS.748 Series 2

HS 748 Series 2A

HS 748 Series 2B

HS748 (RRD Dart)

HP.137 Jetstream Mk.1 Jetstream 1

HP.137 Jetstream Mk.1 Jetstream 2

HP.137 (Turbomeca Astazou)

Jetstream 200 Jetstream 200 (Turbomeca Astazou)

Jetstream 3101 Jetstream 31

Jetstream 3201 Jetstream 32/32EP

Jetstream 31/32 (Honeywell TPE331)

Jetstream 4100

Jetstream 4101

Jetstream 41 (Honeywell TPE331)

BAe ATP ATP (PWC PW120)

B707-100 Long Body

B707-100B Long Body

B707-100B Short Body

B707-300B Series

B707-300C Series

B720

B720B

Boeing 707/720 (PW JT3D)

B707-200

B707-200B

B707-300 Series

Boeing 707 (PW JT4)

B707-400 Series Boeing 707 (RR Conway)

B727 Series

THE BOEING COMPANY

B727-100 Series

Boeing 727 (PW JT8D)



Designation

B727C Series

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

B737-700C

B737-800

B737-900

B737-900ER

Boeing 737-600/700/800/900 (CFM56)

B747-100B Boeing 747-100 (RR RB211 )

B747-100

B747-100B

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)

THE BOEING COMPANY

B747-200B Boeing 747-200/300 (RR RB211)



Designation

B747-200F

B747-200C

B747SP Boeing 747SP (RR RB211)

B747-300 Boeing 747-200/300 (RR RB211)

B747-400

B747-400D

B747-400F/SF(BCF)/LCF

Boeing 747-400 (GE CF6)

B747-400


Boeing 747-400 (PW 4000)

B747-400


Boeing 747-400 (RR RB211)

B747-8I Intercontinental

B747-8F Freighter

Boeing 747-8 (GE GEnx)

B757-200

B757-200PF

B757-300

Boeing 757-200/300 (PW 2000)

B757-200

B757-200PF

B757-200CB

B757-300

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

Boeing 767-200/300/400 (GE CF6)



Designation

B767-300F

B767-400ER

B777-200

B777-200LR

B777-300ER

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 RB 211 Trent 1000)

B787-8 Dreamliner

Boeing 787-8 (GEnx)

CL-215-1A10 Canadair CL-215 (PW R2800)

CL-215-6B11 (CL-215T Variant)

Canadair CL-215 (PWC PW120)

CL-215-6B11 (CL-415 Variant)

Canadair CL-415 (PWC PW123)

BD-100-1A10 Challenger 300 Bombardier BD-100-1A10 (Honeywell AS907)

BD-700-1A10 Global Express

BD-700-1A11 Global 5000

Bombardier BD-700 Series (RRD BR710)

CL600-1A11 Challenger 600 Bombardier CL-600-1A11 (Honeywell ALF502)

CL-600-2A12 (601 Variant)

Challenger 601

CL-600-2B16 (601-3A Variant)

Challenger 601-3A

CL-600-2B16 (601-3R Variant)

Challenger 601-3R

Bombardier CL-600-2A12/-2B16 (variant CL 601/601-3A/3R) (GE CF34)

CL-600-2B16 (CL 604 Variant)

Challenger-604 (MSN < 5701)

CL-600-2B16 (CL 604 Variant)

Challenger-605 (MSN > 5701)

Bombardier CL-600-2B16 (variant CL 604) (GE CF34)

BOMBARDIER

CL-600-2B19 Regional Jet Series 100

Bombardier CL-600-2B19 (GE CF34)



Designation

CL-600-2C10 Regional Jet Series 700/701/702

CL-600-2D15 Regional Jet Series 705

CL-600-2D24 Regional Jet Series 900

CL-600-2E25 Regional Jet Series 1000

Bombardier CL-600-2C10/-2D15/-2D24/-2E25 (GE CF34)

DHC-8-101 DHC-8 Series 100










Bombardier DHC-8-100/200/300 (PWC PW 120)




Bombardier DHC-8-400 (PWC PW150)

SD3-30 Variant 200

SD3-60 Variant 200

SD3-SHERPA Variant 200

SHORT BROTHERS

PLC

SD3-60 SHERPA Variant 200

Shorts SD3 Series-30/SD3-60 (PWC PT6)

C-212-CB Aviocar

C-212-CC Aviocar

C-212-CD Aviocar

C-212-CE Aviocar

C-212-CF Aviocar

C-212-DD Aviocar

C-212-DF Aviocar

C-212-EE Aviocar

C-212-VA Aviocar

CASA C-212 (Honeywell TPE331)

C-212-DE Aviocar CASA C-212 (PWC PT6)

EADS CASA

CN-235 CASA CN-235 (GE CT7)



Designation

CN-235-100

CN-235-200

CN-235-300

CASA CN-235 (GE CT7) EADS CASA

C-295 CASA C-295 (PWC PW127)

525B Citation Jet CJ3

525C Citation Jet CJ4

Cessna 525B/C (Williams FJ 44)

550 Citation Bravo

560 Citation Encore

560 Citation Encore +

Cessna 550/560 (PWC PW530/535)

550 Citation II

S550 Citation S/II

560 Citation V

560 Citation Ultra

Cessna 550/560 (PWC JT15D)

560XL Citation Excel

560 XLS Citation XLS

560 XLS+ Citation XLS+

Cessna 560XL/XLS (PWC PW545)

650 Citation III - VI IV

650 Citation VII

Cessna 650 (Honeywell TFE731)

680 Sovereign Cessna 680 (PWC PW306)

CESSNA AIRCRAFT Company

750 Citation X Cessna 750 (RR Corp AE3007C)

DASSAULT AVIATION

Falcon 10 Falcon 10 (Honeywell TFE731)



Designation

Fan Jet Falcon (Basic) Fan Jet Falcon

Fan Jet Falcon Series C

Fan Jet Falcon Series D

Fan Jet Falcon Series E

Fan Jet Falcon Series F

Falcon 20 (GE CF700)

Mystère Falcon 20-C5

Mystère Falcon 20-D5

Mystère Falcon 20-E5

Mystère Falcon 20-F5

Falcon 20-5 (Honeywell TFE731)

Fan Jet Falcon Series G

Mystère Falcon 200

Mystère Falcon 20GF

Falcon 200 (Honeywell ATF 3-6)

Mystère Falcon 50 Falcon 50 (Honeywell TFE731)

Mystère Falcon 50 F50EX Falcon 50EX (Honeywell TFE731)

Mystère Falcon 900

Mystère Falcon 900 F900B

Falcon 900 (Honeywell TFE731)

Mystère Falcon 900 F900C Falcon 900C (Honeywell TFE731)

Falcon 900EX Falcon 900EX (Honeywell TFE731)

Falcon 900EX F900EX EASy

Falcon 900EX F900DX

Falcon 900EX F900LX

Falcon 900EX EASy (Honeywell TFE731)

Falcon 2000 Falcon 2000 (CFE 738)

Falcon 2000EX Falcon 2000EX (PWC PW308)

Falcon 2000EX F2000EX EASy

Falcon 2000EX F2000DX

Falcon 2000EX F2000LX

Falcon 2000EX EASy (PWC PW308)

Falcon 7X Falcon 7X (PWC PW307A)

228-100 series RUAG Aerospace

GmbH (DORNIER)

228-200 series

Dornier 228 (Honeywell TPE331)



Designation

328-100 series Dornier 328-100 (PWC PW119)

328-300 series Dornier 328-300 (PWC PW306)

EMB-120 Brasilia

EMB-120RT Brasilia

EMB-120ER Brasilia

EMB-120FC Brasilia

EMB-120QC Brasilia

Embraer EMB-120 (PWC PW110 Series)

EMB-135ER

EMB-135LR

EMB-135BJ Legacy 600 Legacy 650

EMB-145

EMB-145ER

EMB-145EU

EMB-145EP

EMB-145LR

EMB-145LU

EMB-145MP

EMB-145MK

Embraer EMB-135/145 (RR Corp AE3007A)

ERJ-170-100 STD ERJ-170

ERJ 170-100 LR ERJ-170

ERJ 170-200 STD ERJ-175

ERJ 170-200 LR ERJ-175

ERJ 190-100 STD ERJ-190

ERJ 190-100 LR ERJ-190

ERJ-190-100SR ERJ-190

ERJ 190-100 IGW ERJ-190 AR

ERJ 190-100 ECJ Lineage 1000

ERJ 190-200 STD ERJ-195

ERJ 190-200 LR ERJ-195

ERJ 190-200 IGW ERJ-195 AR

Embraer ERJ-170/190 (GE CF34)

EMBRAER

EMB-505 Phenom 300 Embraer EMB-505 (PWC PW535)



Designation

F-27A to -M

FH-227

FH-227B

FH-227C

FH-227D

(FOKKER-FAIRCHILD) MARYLAND

AIR INDUSTRIES

FH-227E

F27 Mark 100 Friendship







Fokker F27 / Fairchild F-27/FH-227 (RRD Dart)

F27 Mark 050 Fokker 50



Fokker 50/60 Series (PWC PW 125/127)

F28 Mark 1000 Fellowship

F28 Mark 1000C Fellowship



F28 Mark 3000C Fellowship

F28 Mark 3000R Fellowship

FOKKER SERVICES

F28 Mark 3000RC Fellowship

Fokker F28 Series (RRD Spey)



Designation

F28 Mark 4000 Fellowship Fokker F28 Series (RRD Spey)


FOKKER SERVICES


Fokker 70/100 (RRD Tay)

1125 Westwind Astra

Astra SPX

G100 Gulfstream 100

Gulfstream (IAI) 100/1125/Astra SPX (Honeywell TFE731)

Gulfstream G150 Gulfstream G150 Gulfstream (IAI) G150 (Honeywell TFE731)

GULFSTREAM AEROSPACE

LP (GALP) c/o Israel Aircraft

Industries

Gulfstream 200 / Galaxy Galaxy 200 Gulfstream (IAI) 200/Galaxy (PWC PW306)

G-159 Gulfstream I Gulfstream G-159 (RRD Dart)

G-1159 Gulfstream II

G-1159A Gulfstream IIB

G-1159B Gulfstream III

Gulfstream G-1159 Series (RRD Spey)

G-IV/GIV-SP Gulfstream G-IV/GIV-SP

GIV (G300) Gulfstream G300

GIV (G400) Gulfstream G400

Gulfstream G-IV Series (RRD Tay)

GIV-X (G450) Gulfstream G450

GIV-X (G350) Gulfstream G350

Gulfstream GIV-X Series (RRD Tay)

GULFSTREAM AEROSPACE Corporation

GV Gulfstream GV Gulfstream GV basic model (RRD BR710)



Designation

GV-SP (G550) Gulfstream G550

GV-SP (G500) Gulfstream G500

Gulfstream GV-SP Series (RRD BR710)

HS.125 series 700 "Hawker Siddeley"

BAe.125 series 800

Hawker 800

DH.125 series 1 "Hawker Siddeley"



HS.125 series F3 "Hawker Siddeley"

BH.125 series 400 "Beechcraft Hawker"






BAe 125 Series /700/800 (Honeywell TFE731)

Hawker 750 Hawker 750

Hawker 800XP Hawker 800XP


HAWKER BEECHCRAFT Corporation


BAe 125 Series 750/800XP/850XP/900XP (Honeywell TFE731)



Designation













BAe 125 Series (RR Viper)

BAe.125 series 1000A/B

Hawker 1000

BAe 125 Series 1000 (PWC PW305)

300 Super King Air

300LW Super King Air

B300 Super King Air 350

B300C Super King Air 350 C

Beech 300 Series (PWC PT6)

400 Beechjet Beech 400 / Mitsubishi MU-300 (PWC JT15)



Designation

400A Beechjet (Hawker 400XP)

400T Beechjet

MU-300 Diamond I/IA

MU-300-10 Diamond II

1900 Airliner

1900C Airliner

1900D Airliner

Beech 1900 (PWC PT6)

4000 Hawker 4000 Hawker 4000 (PWC PW308)

IAI 1121 Jetcommander

IAI 1121A Jetcommander

IAI 1121B Jetcommander

IAI 1123 Commodore Jet

IAI 1121/1123 (GE CJ610)F

IAI 1124 Westwind

ISRAEL AIRCRAFT

INDUSTRIES

IAI 1124A Westwind

IAI 1124 (Honeywell TFE731)

KELOWNA (Convair)

440 Convair 580 (RR Corp 501)

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 CJ610)

LEARJET

31 / 31A Learjet 31 (Honeywell TFE731)



Designation

35 / 35A

36 / 36A

Learjet 35/36 (Honeywell TFE731)

Learjet 45 LJ45

Learjet 40 LJ45

Learjet Model 45 (Honeywell TFE731)

55 / 55B / 55C Learjet 55 (Honeywell TFE731) Learjet 60 LJ60

Upgraded Learjet 60 LJ60XR

Learjet 60 (PWC PW305)

1329-25 JetStar II Lockheed 1329 (Honeywell TFE731)

1329-23A

1329-23D JetStar

1329-23E JetStar (-8 version)

Lockheed 1329 PW (PW JT12)

Model 188C Electra

Model L-188 Electra

Lockheed 188 (RR Corp 501)

382 Hercules

382B Hercules

382E Hercules

382F Hercules

382G Hercules

Lockheed 382 (RR Corp 501)

382J Hercules II Lockheed 382 (RR AE2100)

L-1011-385-1 TriStar

L-1011-385-1-14 TriStar

LOCKHEED MARTIN

Corporation

L-1011-385-1-15 TriStar

Lockheed L-1011 (RR RB211)



Designation

L-1011-385-3 TriStar

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 10/20/30 DC-8 (PW JT4A)

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




McDONNELL DOUGLAS

Corporation

MD-88

MD-80 Series (PW JT8D)


1. TC holder 2 Aeroplanes Model Commercial

Designation 3 Type rating endorsement

MD-90 (IAE V2500) MD-90 Series

717-200 MD 717-200 (RRD BR700-715)

DC-10-10

DC-10-10F

DC-10-15

DC-10-30

DC-10-30F

DC-10/MD-10 (GE CF6)

DC-10-40 DC-10 (PW JT9D)

DC-10-40F

MD-11 MD-11 (GE CF6)

MD-11F

MD-11 MD-11 (PW 4000)

SA227-AT

SA227-TT

Fairchild SA227 Series (Honeywell TPE331)

M7 AEROSPACE

SA227-CC

SA227-DC

SA227-AC Swearingen Metro

SA227-BC Swearingen Metro

SA227-PC Swearingen Metro Fairchild SA227 Series (PWC PT6)

PZL M28 00 POLSKIE ZAKLADY LOTNICZE

PZL M28 02

PZL M 28 (PWC PT6)


Annex to ED Decision 2010/011/R 14/12/2010

1. TC holder 2 Aeroplanes Model Commercial Designation

3 Type rating endorsement

PZL M28 05

NA-265-65 Sabreliner NA-265 (Honeywell TFE731)

NA-265-80 Sabreliner NA-265 (GE CF700)

NA-265

NA-265-20

NA-265-30

NA-265-40

NA-265-60

NA-265-65

NA-265-70

SABRELINER Corporation

NA-265-80

Sabreliner NA-265 (PW JT12)

340A(SF340A) Saab-Fairchild 340A

340B

Saab (SF) 340 (GE CT7) SAAB AB, SAAB

Aerosystems

2000 Saab 2000 (RR Corp AE2100)

TUPOLEV PSC TU 204-120CE Tupolev TU 204 (RR RB211)

DHC-7-1

DHC-7-100

DHC-7-101

DHC-7-102

DHC-7-103

DHC-7-110

VIKING AIR

DHC-7-111

De Havilland DHC-7 (PWC PT6)


2. Aeroplanes of 5700 kg and below, requiring type training and individual type

rating (A-tr) 1 TC Holder 2 Aeroplanes

Model Commercial Designation


AERO VODOCHODY Ae 270 Aero Ae-270 (PWC PT6)

L-410M Turbolet

L-410 UVP Turbolet

L-410 UVP-LW L-410 UVP-FG

AIRCRAFT INDUSTRIES

L-410 UVP-E-LW

Let L-410 LW (Walter M601)

425 Corsair / Conquest I Cessna 425 (PWC PT6) 441 Cessna 441 (Honeywell TPE331) 500 Citation / Citation I Cessna 500 (PWC JT15D)

Cessna 500/501/551 (PWC JT15D) 501 Citation 551 Citation II

Cessna 500/501/551 (PWC JT15D) Cessna 500/501/551 (PWC JT15D)

510 Cessna 510 (PWC PW615) 525 Citation Jet CJ1


525A Citation Jet CJ2 Cessna 525/525A (Williams FJ 44)

DORNIER Seastar

Seastar CD2 Dornier Seastar CD2 (PWC PT6)

ECLIPSE AEROSPACE Inc.

EA500 Eclipse EA500 (PWC PW610)

EMB-110P1 Bandeirante

EMB-110P2 Bandeirante Embraer EMB-110 (PWC PT6)

EMB-121A Xingu I

EMB-121A1 Xingu II

EMB-121V Xingu III

Embraer EMB-121 (PWC PT6)

EMBRAER Empresa Brasileira de Aeronautica

EMB-500 Phenom 100 Embraer EMB-500 (PWC PW617) EXTRA Flugzeugproduktions- und Vertiebs GmbH

EA 400-500 Extra EA-400-500 (RR Corp 250)

65-90 King Air 65-A90 King Air 65-A90-1 King Air 65-A90-4 King Air 65-A90-2 King Air B90 King Air C90 King Air C90A King Air C90GT King Air C90GTi King Air E90 King Air F90 King Air

HAWKER BEECHCRAFT Corporation H90 King Air



1 TC Holder 2 Aeroplanes



200/A200

200C/A200C

200CT/A200CT

200T

B200

B200C

B200CT

B200T

B200GT

B200CGT


99

99A

A99 Airliner

A99A Airliner

B99 Airliner

C99 Airliner

100 King Air

A100 King Air

A100A/C King Air

Beech 99/100 Series (PWC PT6)

B100 Beech B100 (Honeywell TPE331)

HAWKER BEECHCRAFT Corporation (cont.)

390 Premier 1, 1A Beech 390

(Williams FJ44)

ISRAEL AIRCRAFT Industries

Arava 101B Arava 101B (PWC PT6)

LEARJET

LJ 23 Learjet 23 (GE CJ610)

SA226-T

SA226-TC

SA226-AT

M7 AEROSPACE

SA226-T(B)

Fairchild SA226 (Honeywell TPE331)

MU-2B

MU-2B-10

MU-2B-20

MU-2B-125

MU-2B-30

MU-2B-35

MU-2B-2540

MU-2B-36

MITSUBISHI Heavy Industries

MU-2B-2660

Mitsubishi MU-2B (Honeywell TPE331)

P.166 DP1 Piaggio P166 (PWC PT6)

P180 Avanti

PIAGGIO Aero Industries

P180 Avanti II Piaggio P180 Avanti/Avanti II (PWC PT6)



List 2

1 TC Holder 2 Aeroplanes Model Commercial Designation


PC-12 PC-12/45

PC-12/47

PILATUS AIRCRAFT

PC-12/47E

Pilatus PC-12 (PWC PT6)

PA-42-1000 Cheyenne 400LS Piper PA-42 (Honeywell TPE-331) PA-42 Cheyenne III

PA-42-720 PA-42-720R

Cheyenne IIIA Piper PA-42 (PWC PT6)

PIPER AIRCRAFT

PA-46-500TP Malibu Meridian Piper PA-46-500TP (PWC PT6) REIMS AVIATION

F 406 Caravan II Reims-Cessna F 406 (PWC PT6)

TBM 700 A

TBM 700 B

TBM 700 C1

TBM 700 C2

SOCATA

TBM 700 N TBM 850

Socata TBM 700/850 (PWC PT6)

680-T

680-V

680-W

681

690

690A

690B

690C

690D

695

695A

TWIN COMMANDER AIRCRAFT Corporation

695B

Twin Commander 680/681/690/695 Series (Honeywell TPE331)

DHC-6-1 Twin Otter DHC-6-100/110 Twin Otter DHC-6-200/210 Twin Otter DHC-6-300/310/320

Twin Otter

VIKING AIR (Bombardier) (De Havilland)

DHC-6-400 Twin Otter

De Havilland DHC-6 (PWC PT6)

AP68TP300 Spartacus

AP68TP600 Viator

Vulcanair AP68TP Series (RR Corp 250)

SF600

VULCANAIR

SF600A Vulcanair SF600 (RR Corp 250)


3. Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below, eligible for

type examinations and manufacturer 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 (Islander) (RR Corp 250)

RUAG Aerospace Services GmbH DORNIER

Dornier Do 28 Series (PWC PT6)

DORNIER Dornier Do 28 (Walter M601)

Fairchild SA26-T (PWC PT6) M7 AEROSPACE (Fairchild-Swearingen Corp)

Fairchild SA26 AT(Honeywell TPE331)

PIPER AIRCRAFT Corporation Piper PA-31T Series (PWC PT6)

SHORT BROTHERS Shorts SC7 (Honeywell TPE331)


http://en.wikipedia.org/wiki/Fairchild_(aircraft_manufacturer)

4. Aeroplanes single turbine engine (ASTE) of 5700 kg and below, eligible for type

examinations and group ratings TC holder Type rating endorsement

Air Tractor AT-302 (Lycoming LTP-101) AIR TRACTOR

Air Tractor AT-400/500/600/800 Series (PWC PT6)

ZLIN AIRCRAFT INDUSTRIES Zlin Z-37 T Series (Walter M601)

ALENIA AERMACCHI Aermacchi SF260TP (RR Corp 250)

ALLIED AG CAT Productions

Grumman G-164 (PWC PT6)

Cessna (Soloy) 206/207 (RR Corp 250)

Cessna 208 Series (PWC PT6)


Cessna 210 (RR Corp 250)

EADS PZL PZL-106 BT (Walter M601) EADS PZL “WARSZAWA-OKECIE”

EADS PZL PZL-106 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 PC-6 Series (PWC PT6)

Pilatus PC-6 Series (Turbomeca Astazou)

PILATUS AIRCRAFT

Pilatus PC-6 Series (Honeywell TPE 331)

THRUSH AIRCRAFT Ayres S2R Series (PWC PT6)

VIKING AIR (Bombardier) (De Havilland)

DeHavilland DHC-2 (PWC PT6)


5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for

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)

Britten-Norman BN2 Islander (Lycoming)

Britten-Norman BN2A Series Trislander (Lycoming)

B-N GROUP (Britten-Norman)

Britten-Norman BN2B Series (Lycoming)

Cessna 310/320 Series (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 AIRCRAFT Company/ REIMS AVIATION

Cessna T303 (Continental) GENERAL AVIA Costruzioni Aeronautiche

General Avia F20 Series (Lycoming)

Beech 50 Series (Lycoming) Beech 55 Series (Continental) Beech 56 Series (Lycoming) Beech 58 Series (Continental) Beech 58P (Continental) Beech 58TC (Continental) Beech 60 Series (Lycoming) Beech 65-80 Series (Lycoming) Beech 76 (Lycoming)


Beech 95 Series (Lycoming)

OMA SUD SPA Sky Technolgies SKYCAR (Lycoming)

PIAGGIO Aero Industries

Piaggio P166 (Lycoming)

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 AIRCRAFT

Piper PA-44 Series (Lycoming) PZL MIELEC PZL-M20 (PZL)



List 5

TC holder Type rating endorsement RUAG Aerospace Services GmbH Do 28/128 Series (Lycoming) SOCATA Grumman GA-7 (Lycoming)

STOL AIRCRAFT Corporation

Republic UC-1 (Lycoming)

TECNAM Costruzioni Aeronautiche

Tecnam P2006T (Rotax)

Commander 685 (Continental)

Commander 500 Series/680 Series (Lycoming)

TWIN COMMANDER AIRCRAFT Corporation

Rockwell 700 (Lycoming) Vulcanair P.68 Series (Lycoming) VULCANAIR

Vulcanair F600A (Lycoming)


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 AT-250/300 (PW R985)

Air Tractor AT-301/401/501 (PW R1340)

AIR TRACTOR

Air Tractor AT-401 (PZL-3S) Air Transport Group Holdings, Inc

Lake C/LA Series (Lycoming)

Aermacchi AL60 (Continental) Aermacchi AL60 (Lycoming) SIAI-Marchetti S.205/S.208 (Lycoming) SIAI-Marchetti S.205 (Franklin)

ALENIA AERMACCHI

Aermacchi SF260 Series (Lycoming) Grumman G-164 (Continental) Grumman G-164 (Jacobs)

ALLIED AG CAT Productions

Grumman G-164 (PW R Series) Robin HR 100 series (Lycoming) Robin HR 100 series (Continental) Robin R 1180 series (Lycoming)

APEX Aircraft (ALPHA) CEAPR

Robin R 3000 series (Lycoming) ALPHA AVIATION (APEX Aircraft) Robin HR 200/ R 2000 series (Lycoming) ARV Aviation ARV 1 Super 2 (Hewland)

Bölkow BO 208 (Continental) BÖLKOW

Bölkow BO 209 (Lycoming) Commander 112 (Lycoming) COMMANDER PREMIER AIRCRAFT

CO. Commander 114 (Lycoming) Beagle B.121 series 1 (Continental) DE HAVILLAND

Support Beagle B.121 series 2/3 (Lycoming)

DYNAC AEROSPACE Corporation Aerocommander 100 (Lycoming)

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 (Thielert) 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)


Type rating endorsement TC holder

Cessna 188 (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)

OA7 Optica Series (Lycoming) FLS AEROSPACE

Club Sprint/Sprint 160 (Lycoming) FUJI Heavy Industries Fuji FA-200 Series (Lycoming) GARDAN Gardan GY 80 (Lycoming) GENERAL AVIA Costruzioni Aeronautiche General Avia F.22 (Lycoming)

GIPPSLAND Aeronautics Gippsland GA8 (Lycoming) 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 IAROM

IAROM IAR-46 (Rotax)

INTERCEPTOR AIRCRAFT Corporation

Aerocommander 200 (Continental)

LAKE AIRCRAFT Lake 250 (Lycoming) LAVIA ARGENTINA S.A. (LAVIASA) Piper PA-25 Series (Lycoming)

Maule M4 (Continental) Maule M4 (Franklin) Maule M5 (Lycoming) Maule M5 (Franklin) Maule M5 (Continental) Maule M6 (Lycoming) Maule M7 Series (Lycoming)

MAULE AEROSPACE TECHNOLOGY

Maule MX-7 (Lycoming) Meteor FL53 (Continental) Meteor FL54 (Continental)

METEOR

Meteor FL55 (Lycoming) Mooney M20B to M20S/M22 (Lycoming) MOONEY AIRPLANE Company

Mooney M20 (Continental) PILATUS AIRCRAFT Pilatus PC-6 Series (Lycoming)

Piper PA-22 Series (Lycoming) Piper PA-24 Series (Lycoming) Piper PA-28 Series (Lycoming) Piper PA-28 Series (Continental)

PIPER AIRCRAFT PIPER AIRCRAFT Piper PA-28 Series (Thielert)


Type rating endorsement TC holder

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)

(cont.

Piper PA-46 Series (Lycoming)

SKY Int ENTREPRISE Aviat Husky A (Lycoming) PZL-101A Gawron (Ivchenko) PZL-104A Wilga (Ivchenko) PZL-104 Wilga Series (PZL) PZL M 18 (PZL) PZL M 26 (Lycoming)

EADS PZL "WARSZAWA-OKECIE"

PZL-104 Wilga (Lycoming)

REGAL AIR, Inc. REGAL AIR 305 Seris (Continental)

REVO, Inc. REVO C/LA-4 Series (Lycoming)

SOCATA MS 880/885/890 (Continental) SOCATA MS 881 (Potez) SOCATA MS 883/886/887 (Lycoming) SOCATA MS 892/893 / PZL Koliber (Lycoming) SOCATA MS 894 / PZL Koliber (Franklin) SOCATA Rallye 100 (Continental) SOCATA Rallye Series (Continental)

SOCATA Rallye 110ST (Lycoming) SOCATA Rallye Series (Lycoming)

SOCATA Rallye 150 (Lycoming) SOCATA Rallye 180T (Lycoming) SOCATA Rallye 235 (Lycoming) SOCATA ST10 (Lycoming)

SOCATA TB Series (Lycoming)

SOCATA TB 9 (Lycoming) SOCATA TB 10 (Lycoming) SOCATA TB 20 (Lycoming) SOCATA TB 21 (Lycoming)

SOCATA

SOCATA TB 200 (Lycoming) SYMPHONY AIRCRAFT Industries Symphony OMF-100-160 (Lycoming)

Tecnam P92 (Rotax) TECNAM Costruzioni Aeronautiche

Tecnam P96/P2002/P2004 (Rotax)

THRUSH Aircraft

Ayres S2R (PW R-985)

Grumman/American AA-1/-1A Series (Lycoming) TRUE FLIGHT Holdings

Grumman/American AA-5/AG-5B Series (Lycoming)

Partenavia P.64 (Lycoming) VULCANAIR

Partenavia P.66 (Lycoming)



List 6

TC holder Type rating endorsement CERVA CE43 (Lycoming) WASSMER

CERVA CE44 (Continental) Yakovlev YAK-18T (Vedeneyev) YAKOVLEV

Yakovlev YAK-54/55/55M (Vedeneyev) Zlin Z-42 Series (LOM) Zlin Z-43 (LOM) Zlin Z-50 (LOM) Zlin Z-50L Series (Lycoming) Zlin Z-26 Series (LOM) Zlin Z-26 Series (Walter Minor/M Avia) Zlin Z-143 L (Lycoming) Zlin Z-242 L (Lycoming)

ZLIN AIRCRAFT (MORAVAN AVIATION)

Zlin Z-526 L (Lycoming)


7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for


No aircraft in this list.


8. Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE-

WS), eligible for type examinations and group ratings TC holder Type rating endorsement

Bellanca 14-19 Series (Continental) ALEXANDRIA Aircraft

Bellanca 17-30/17-31 Series (Continental) Robin ATL / ATL S (JPX 4T60) APEX CEAPR

Robin ATL L (Limbach L2000) APEX Dyn’Aero CAP 10 (Lycoming)

Robin DR 220 series (Continental) Robin DR 250 series (Lycoming) Robin DR 300 series (Lycoming) Robin DR 400 series (Lycoming) Robin DR 400RP (Porsche)

APEX CEAPR

Robin DR 400RP (Thielert) Champion 7 Series (Continental) Champion 7 Series (Lycoming)

AMERICAN CHAMPION BELLANCA Aircraft Corporation

Champion 8 Series (Lycoming) Klemm K1.107/F.207 (Continental) BÖLKOW

Bölkow F.207 (Lycoming) Mooney M20/M20A (Lycoming) MOONEY AIRPLANE Company

Mooney M18L (Continental) NIPPER Nipper T-66 (Stark)

RF 6B (Continental) EIS RENE FOURNIER RF 6B (Lycoming) SCHEIBE Flugzeugbau SF 23 Series (Continental)

Pitts S-1 Series (Lycoming) SKY INTERNATIONAL

Pitts S-2 Series (Lycoming)

Skyfox Aviation Ltd CA25 Series (Rotax)

SLINGSBY Aviation Slingsby T67 Series (Lycoming)

EIS GmbH SPORTAVIA PUETZER

RS 180 (Lycoming)

Taylorcraft 19 Series (Continental) TAYLORCRAFT 2000

Taylorcraft F21/F22/F22A Series (Lycoming)

VULCANAIR Partenavia P57 (Lycoming) WACO Aircraft Company Waco YMF (Jacobs)

WA40 Series (Lycoming) WA41 (Lycoming)

WASSMER

WA4/21 Series (Lycoming)


9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for


TC holder Type rating endorsement

Diamond DA42 Series (Thielert) DIAMOND AIRCRAFT Industries

Diamond DA42 Series (Austro Engine)


10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible for

type examinations and group ratings TC holder Type rating endorsement

CAP 20/21 (Lycoming) APEX Dyn’Aero

CAP 230 Series (Lycoming)

AQUILA Technische Entwicklungen Aviation by Excellence AG

Aquila AT01 (Rotax)

CESSNA AIRCRAFT Company (COLUMBIA)

Cessna C300/C350/C400 (Continental)

Cirrus SR20 (Continental) CIRRUS Design Corporation

Cirrus SR22 Series (Continental) Diamond DA20/DV20 (Rotax) Diamond DA20 (Continental) Diamond DA40 (Lycoming) Diamond DA40 D (Thielert)

DIAMOND AIRCRAFT Industries

Diamond DA40 (Austro Engine) AIRCRAFT Design and Certification (WD) D4 Fascination (Rotax)

Extra EA-300 Series (Lycoming) EXTRA Flugzeugproduktions- und Vertriebs-GmbH 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

Ruschmeyer R90-230RG (Lycoming)

SEASTAR CORP TSC Series (Lycoming)

Sukhoi SU-29 (Vedeneyev) Sukhoi SU-31 (Vedeneyev) Sukhoi SU-26 (Vedeneyev)

SUKHOI

Sukhoi Su-29/31 (MGA) SLINGSBY AVIATION Slingsby T67A/T67B/T67C/T67M Series (Lycoming)


11. Multi-engine helicopters (MEH), requiring type training and individual type

rating

1 TC Holder 2 Helicopter Model Commercial Designation


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 / AW139 (PWC PT6)

EH101-500 Series

EH101-510 Series

AGUSTA

EH101-300

Agusta/Westland EH-101 (GE CT7)

AGUSTA AB 212

212 Bell 212 / Agusta AB212 (PWC PT6)

214ST Bell 214ST(GE CT7) 412

412EP

BELL HELICOPTER TEXTRON

412CF

AB 412 AGUSTA

AB 412 EP

Bell 412 / Agusta AB412 (PWC PT6)

427 Bell 427 (PWC PW207D)

222

222B

222U

Bell 222 (Honeywell LTS 101)

230 230 Executive 230 Utility 230 EMS

Bell 230 (RR Corp 250)



BELL HELICOPTER CANADA

430 Bell 430 (RR Corp 250)

COLUMBIA HELICOPTERS

234 234UT

Boeing 234 (Honeywell 5512)

ERICKSON AIR-CRANE EAC S-64F

Erickson S-64 (PW JFTD 12)

SA 330 F EUROCOPTER

SA 330 G

Eurocopter SA 330 (Turbomeca Turmo)


1 TC Holder 2 Helicopter



SA 330 J

AS 332 C

AS 332 L

AS 332 C1

AS 332 L1

Eurocopter AS 332 (Turbomeca Makila 1A/1A1)

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)

AS 355 N

AS 355 NP

Eurocopter AS 355 (Turbomeca Arrius 1)

SA 365 N 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

Dauphin

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)

BO 105 A

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 EC 135 (PWC PW206)

EC 135 T1 Series

EC 135 T2 Series

EC 635 T1

EUROCOPTER DEUTSCHLAND GMBH

EC 635 T2 Series

Eurocopter EC 135 (Turbomeca Arrius 2B)



List 11



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 EC145 Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1)

KAMOV KA-32A/T

Kamov Ka 32 (Klimov)

MD HELICOPTERS, INC. MD900

MD Helicopters MD900 (PWC PW206/207)

W-3A PZL-ŚWIDNIK

W-3AS

PZL-Swidnik W-3A/W-3AS (Rzeszow PZL-10W)

AS61N AGUSTA

AS61NI

S-61N

S-61NM

Agusta AS61N/Sikorsky S-61N (GE CT58)

S-58 BT to JT Sikorsky S-58 (PWC PT6T) S-76A Sikorsky S-76A (RR Corp 250) S-76A S-76A+

S-76A S-76A++ Sikorsky S-76A (Turbomeca Arriel 1)

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 S-76C (Turbomeca Arriel 2)

SIKORSKY AIRCRAFT

S-92A Sikorsky S-92A (GE CT7-8)


12. Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings 1 TC Holder 2 Helicopter



A119 AGUSTA

AW119 MkII Koala

Agusta A119/ Agusta AW119MkII (PWC PT6)

214B

BELL HELICOPTER TEXTRON

214B-1

Bell 214 (Honeywell T5508)

BELL HELICOPTER CANADA 407

Bell 407 (RR Corp 250)

AB 204 B Series AGUSTA

AB 205 A1

204B BELL HELICOPTER TEXTRON, INC. 205A-1

Agusta AB204, AB205 / Bell 204, 205 (Honeywell T53)

AB 206A AGUSTA AB 206B

BELL HELICOPTER TEXTRON CANADA LIMITED

206 series from A to L

Agusta AB206 / Bell 206 (RR Corp 250)

480 THE ENSTROM HELICOPTER CORPORATION 480B

Enstrom 480 (RR Corp 250)

AS 350

AS 350 B1

AS 350 B2

AS 350 BA

AS 350 BB

Eurocopter AS 350 (Turbomeca Arriel 1)

AS 350 B3

Écureuil

Eurocopter AS 350 (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)

EUROCOPTER

SA 342 J Gazelle Eurocopter SA 342 J (Turbomeca Astazou XIV)



List 12



SA 360C Dauphin Eurocopter SA 360 (Turbomeca Astazou XVIIIA)

SE 3160

SA 316 B

EUROCOPTER (CONT.)

SA 316 C

Alouette III Eurocopter SA 316 B/SA 316 C (Turbomeca Artouste)

KAMAN AEROSPACE CORPORATION K-1200

Kaman K-1200 (Honeywell T5317)

369 H series MD HELICOPTERS INC. (MDHI)

369 D to FF

S.E.I SERVIZI ELICOTTERISTICI ITALIANI

NH-500D

MD Helicopters 369 Series / SEI NH-500D (RR Corp 250)

600N MD HELICOPTERS INC. (MDHI) 500N S.E.I SERVIZI ELICOTTERISTICI ITALIANI

AMD-500N

MD Helicopters 500N/600N /AMD500N (RR Corp 250)

PZL-ŚWIDNIK SW-4 PZL SW-4 (RR Corp 250)

SCHWEIZER AIRCRAFT CORPORATION

269D Schweizer 269D (RR Corp 250)


13. Helicopters – Single piston engines (HSPE), eligible for type examinations and group ratings 1 TC Holder 2 Helicopter 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)

F-28 series THE ENSTROM HELICOPTER CORPORATION 280 series

Enstrom F-28/280 (Lycoming)

SEI (BREDA-NARDI) NH 300C

269A

269B

269C

SCHWEIZER AIRCRAFT CORPORATION

269C-1

Model 300C Schweizer / Breda Nardi (Hughes) 269/300 (Lycoming)

R22

R22 ALPHA

R22 BETA

R22 MARINER

R44

ROBINSON HELICOPTER COMPANY

R44 II

Robinson R22/R44 Series (Lycoming)

SIKORSKY AIRCRAFT S-58 A to J Sikorsky S-58 (Wright Cyclone)


AMC Part-66 Appendix II

Aircraft Type Practical Experience

List of Task’s


APPENDIX II

Aircraft Type Practical ExperienceList of Tasks


Appendix II - Aircraft type practical experience list of tasksTime limits/Maintenance checks

100 hour check (general aviationaircraft).“B” or “C” check (transport categoryaircraft).Review records for compliance withairworthiness directives.Review records for compliance withcomponent life limits.Procedure for Inspection followingheavy landing.Procedure for Inspection followinglightning strike.

Dimensions/Areas

Locate component(s) by stationnumber.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 systemPerform 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 airconditioning/heating systemCheck operation of pressurisationsystemTroubleshoot faulty system

Auto flight

Install servos.Rig bridle cablesReplace 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 systemCheck flight management systemsCheck stability augmentation system

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 ofpassenger address system.Functionally check audio integratingsystem.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 carpetsReplace crew seats.Replace passenger seats.Check inertia reels.Check seats/belts for security.Check emergency equipment.Check ELT for compliance withregulations.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 detectionsystems

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 unitReplace flat acuatorAdjust trim tab.Adjust control cable tension.


Check control range and sense ofmovement.Check for correct assembly andlocking.Troubleshoot faulty system.

Fuel

Replace booster pump.Replace fuel selector.Replace fuel tank cells.Check filters.Flow check system.Check calibration of fuel quantitygauges.Check operation feed/selectorsTroubleshoot 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.Troubleshoot faulty system.Implement ESDS proceduresInspect 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 lightingsystem.Perform emergency lighting systemchecks.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 DMEFunctional check ATC TransponderFunctional check flight directorsystem.Functional check inertial nav system.Complete quadrantal error correctionof ADF system.Update flight management systemdatabase.Check calibration of pitot staticinstruments.Check calibration of pressure altitudereporting system.


Troubleshoot faulty systemCheck marker systemsCompass replacement direct/indirectCheck SatcomCheck GPSTest AVM

Oxygen

Inspect on board oxygen equipment.Purge and recharge oxygen system.Replace regulator.Replace oxygen generator.Test crew oxygen system.Perform auto oxygen systemdeployment 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.

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 unitReplace 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 andlocking.Check controls for operation andsense.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.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/ignitors.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 assemblyand locking.Check controls for range and sense ofoperation.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.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 check 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.


Part-66 - acao.org.maacao.org.ma/programmes/1455710432_2.pdf · Part-66 Appendix III — Type training and Examination Standard Part-66 Appendix IV — Experience requirements for

Documents

Part-66 - acao.org.maacao.org.ma/programmes/1455710432_2.pdf · Part-66 Appendix III — Type training and Examination Standard Part-66 Appendix IV — Experience requirements for