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
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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
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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
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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
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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.
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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
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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.
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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.
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66.A.15 Eligibility
An applicant for an aircraft maintenance licence shall be at least 18 years of age.
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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.
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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.
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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.
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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:
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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;
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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.
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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.
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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.
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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.
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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.
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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.
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66.A.30 Experience requirements
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.
66.A.30 Experience requirements
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.
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66.A.30 Experience requirements
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.
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66.A.30 Experience requirements
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.
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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)
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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.
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66.A.45 Type/task training and ratings
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.
66.A.45 Type/task training and ratings
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.
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66.A.45 Type/task training and ratings
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.
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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.
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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.
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66.A.45 Type/task training and ratings
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.
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66.A.45 Type/task training and ratings
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.
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66.A.45 Type/task training and ratings
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.
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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
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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.
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66.A.45 Type/task training and ratings
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.
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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.
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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.
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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.
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66.A.200 General
Until such time as this Part specifies a requirement for certifying components, the relevant Member State regulation shall
apply.
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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.
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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.
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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.
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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.
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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.
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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.
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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.
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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.
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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.
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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
Aircraft type endorsement should use the standard codes contained in Appendix I.
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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
Aircraft type endorsement should use the standard codes contained in Appendix I.
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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
Aircraft type endorsement should use the standard codes contained in Appendix I.
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.
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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.
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SUBPART CEXAMINATIONS
This subpart provides a procedure for examination conducted by the competent authority.
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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.
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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.
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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.
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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.
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SUBPART DCONVERSION OF NATIONAL QUALIFICATIONS
This Subpart provides the requirements for converting national qualifications to aircraft maintenance licences.
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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.
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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.
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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.
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SUBPART EEXAMINATION CREDITS
This Subpart provides the requirements for granting examination credits in accordance with 66.A.25(b).
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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.
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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.
For Training Purpose Only Page 70
SUBPART FREVOCATION, SUSPENSION OR LIMITATIONOF THE AIRCRAFT MAINTENANCE LICENCE
For Training Purpose Only Page 71
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.
For Training Purpose Only Page 72
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For Training Purpose Only Page 74
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For Training Purpose Only Page 75
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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,+-
For Training Purpose Only Page 79
"3
CVgV]
7 8, 8-
D`]VTf]Rc decfTefcV `W T`_UfTe`cd' dV^ZT`_UfTe`cd R_UZ_df]Re`cd)
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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,+.
For Training Purpose Only Page 80
"3
CVgV]
7 8, 8-
9`_decfTeZ`_ `W NYVRede`_V 8cZUXV6
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9RaRTZe`c ejaVd' T`_decfTeZ`_ R_U Wf_TeZ`_6
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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,+/
For Training Purpose Only Page 81
"3
CVgV]
7 8, 8-
=RTe`cd RWWVTeZ_X ^fefR] Z_UfTeR_TV5 _f^SVc `W efc_d Z_T`Z]' aYjdZTR] dZkV `W T`Z]' aVc^VRSZ]Zej `W T`Z]' a`dZeZ`_ `WT`Z]d hZeY cVdaVTe e` VRTY `eYVc6
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KcR_dW`c^Vc RTeZ`_ f_UVc ]`RU R_U _`(]`RU T`_UZeZ`_d6
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9R]Tf]ReZ`_ `W a`hVc Z_ R eYcVV aYRdV djdeV^6
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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,+0
For Training Purpose Only Page 82
"3
CVgV]
7 8, 8-
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I`eReZ`_ `W ]``a Z_ R ^RX_VeZT WZV]U R_U hRgVW`c^ac`UfTVU6
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-++.I-+/- # <E # -4),+)-++3 # ++.)++, # ,+1
For Training Purpose Only Page 83
"3
CVgV]
7 8, 8-
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7aa]ZTReZ`_ `W ecR_dZde`cd5 T]RddVd `W R^a]ZWZVc $7' 8' 9%6
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For Training Purpose Only Page 84
"3
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For Training Purpose Only Page 85
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For Training Purpose Only Page 86
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For Training Purpose Only Page 87
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For Training Purpose Only Page 88
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For Training Purpose Only Page 89
"3
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For Training Purpose Only Page 90
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For Training Purpose Only Page 91
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For Training Purpose Only Page 92
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For Training Purpose Only Page 93
"3
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For Training Purpose Only Page 94
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For Training Purpose Only Page 95
"3
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For Training Purpose Only Page 96
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For Training Purpose Only Page 97
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For Training Purpose Only Page 98
"3
CVgV]
7, 8,), 8-
GcZ^Rcj T`_ec`]d5 RZ]Vc`_' V]VgRe`c' cfUUVc' da`Z]Vc6
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For Training Purpose Only Page 99
"3
CVgV]
7, 8,), 8-
KjcVd6
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For Training Purpose Only Page 100
"3
CVgV]
7- 8,)- 8-
9`_ec`] fdZ_X V]Vg`_d' cfUUVcgRe`cd6
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8`f_URcj ]RjVc T`_ec`] fdZ_X' g`ceVi XV_VcRe`cd' deR]]hVUXVd `c ]VRUZ_X VUXV UVgZTVd6
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For Training Purpose Only Page 101
"3
CVgV]
7- 8,)- 8-
CR_UZ_X XVRc' aj]`_' T`_ec`] dfcWRTV R_U YZXY ]ZWe*UcRXReeRTY^V_ed)
,,).). F_MNUXU^Q]^ "3G3 --# , - #
9`_decfTeZ`_6
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8ReeVcZVd @_deR]]ReZ`_ R_U FaVcReZ`_6
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For Training Purpose Only Page 102
"3
CVgV]
7- 8,)- 8-
$S% , , #
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For Training Purpose Only Page 103
"3
CVgV]
7- 8,)- 8-
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For Training Purpose Only Page 104
"3
CVgV]
7.
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9`cZ`]Zd VWWVTe R_U T`^aV_dReZ`_6
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8]RUV ;R^aVcd5 =f_TeZ`_ R_U T`_decfTeZ`_6
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For Training Purpose Only Page 105
"3
CVgV]
7.
7/
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For Training Purpose Only Page 106
"3
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For Training Purpose Only Page 107
"3
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For Training Purpose Only Page 108
"3
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For Training Purpose Only Page 109
"3
CVgV]
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For Training Purpose Only Page 110
"3
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For Training Purpose Only Page 111
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For Training Purpose Only Page 112
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>Rd T`fa]VU*WcVV efcSZ_V R_U XVRc T`fa]VU efcSZ_Vd6
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7ccR_XV^V_ed' UcZgV djdeV^d' cVUfTeZ`_ XVRcZ_X'T`fa]Z_Xd' T`_ec`] djdeV^d)
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For Training Purpose Only Page 113
"3
CVgV]
7 8, 8-
9`_WZXfcReZ`_ `W WZcVhR]]d' T`h]Z_Xd' RT`fdeZT aR_V]d'
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,0)-+ 7QZM AZW\MK\QWV Da[\MU[ , - #
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Gc`TVUfcVd W`c deRceZ_X R_U Xc`f_U cf_(fa6
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KcV_U $Z_T]fUZ_X `Z] R_R]jdZd' gZScReZ`_ R_U S`c`dT`aV%^`_Ze`cZ_X6
@_daVTeZ`_ `W V_XZ_V R_U T`^a`_V_ed e` TcZeVcZR' e`]VcR_TVdR_U UReR daVTZWZVU Sj V_XZ_V ^R_fWRTefcVc6
9`^acVdd`c hRdYZ_X*T]VR_Z_X6
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,0)-- 6VOQVM D\WZIOM IVL AZM[MZ^I\QWV # - #
GcVdVcgReZ`_ R_U UVacVdVcgReZ`_ W`c eYV V_XZ_V R_U RTTVd(d`cZVd*djdeV^d)
DF;LC< ,1) G@JKFE <E>@E<
CVgV]
7 8, 8-
,1), 7]VLIUMV\IT[ , - #
DVTYR_ZTR]' eYVc^R] R_U g`]f^VecZT VWWZTZV_TZVd6
FaVcReZ_X acZ_TZa]Vd # - dec`\V' / dec`\V' Fee` R_U;ZVdV]6
GZde`_ UZda]RTV^V_e R_U T`^acVddZ`_ cReZ`6
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G`hVc TR]Tf]ReZ`_ R_U ^VRdfcV^V_e6
=RTe`cd RWWVTeZ_X V_XZ_V a`hVc6
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7TTVdd`cj XVRcS`i6
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KjaVd' T`_decfTeZ`_ R_U acZ_TZa]Vd `W `aVcReZ`_6
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For Training Purpose Only Page 114
"3
CVgV]
7 8, 8-
,1)/)- 8`QX UZVQO_U[Z ^d^_QY^ , - #
KjaVd' T`_decfTeZ`_ R_U acZ_TZa]Vd `W `aVcReZ`_)
,1)/). 7XQO_][ZUO QZSUZQ O[Z_][X , - #
FaVcReZ`_ `W V_XZ_V T`_ec`] R_U WfV] ^VeVcZ_X djdeV^dZ_T]fUZ_X V]VTec`_ZT V_XZ_V T`_ec`] $=7;<9%6
JjdeV^d ]Rj(`fe R_U T`^a`_V_ed)
,1)0 D\IZ\QVO IVL ;OVQ\QWV Da[\MU[ , - #
JeRceZ_X djdeV^d' acV(YVRe djdeV^d6
DRX_Ve` ejaVd' T`_decfTeZ`_ R_U acZ_TZa]Vd `W `aVcReZ`_6
@X_ZeZ`_ YRc_VddVd' daRc\ a]fXd6
C`h R_U YZXY eV_dZ`_ djdeV^d)
,1)1 ;VL]K\QWV$ 6`PI][\ IVL 4WWTQVO Da[\MU[ , - #
9`_decfTeZ`_ R_U `aVcReZ`_ `W5 Z_UfTeZ`_ djdeV^dZ_T]fUZ_X R]eVc_ReV RZc djdeV^d6
<iYRfde djdeV^d' V_XZ_V T``]Z_X djdeV^d # RZc R_U]ZbfZU)
,1)2 D]XMZKPIZOQVO'E]ZJWKPIZOQVO , - #
GcZ_TZa]Vd R_U afca`dV `W dfaVcTYRcXZ_X R_U Zed VWWVTed `_V_XZ_V aRcR^VeVcd6
9`_decfTeZ`_ R_U `aVcReZ`_ `W dfaVcTYRcXZ_X*efcS`(TYRcXZ_X djdeV^d6
JjdeV^ eVc^Z_`]`Xj6
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,1)3 =]JZQKIV\[ IVL 7]MT[ , - #
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,1)4 =]JZQKI\QWV Da[\MU[ , - #
JjdeV^ `aVcReZ`_*]Rj(`fe R_U T`^a`_V_ed)
,1),+ 6VOQVM ;VLQKI\QWV Da[\MU[ , - #
<_XZ_V daVVU6
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9``]R_e eV^aVcRefcV6
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,1),, AW_MZXTIV\ ;V[\ITTI\QWV , - #
9`_WZXfcReZ`_ `W WZcVhR]]d' T`h]Z_Xd' RT`fdeZT aR_V]d'V_XZ_V ^`f_ed' R_eZ(gZScReZ`_ ^`f_ed' Y`dVd' aZaVd'WVVUVcd' T`__VTe`cd' hZcZ_X ]``^d' T`_ec`] TRS]Vd R_Uc`Ud' ]ZWeZ_X a`Z_ed R_U UcRZ_d)
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Gc`TVUfcVd W`c deRceZ_X R_U Xc`f_U cf_(fa6
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For Training Purpose Only Page 115
"3
CVgV]
7 8, 8-
@_eVcacVeReZ`_ `W V_XZ_V a`hVc `feafe R_U aRcR^VeVcd6
@_daVTeZ`_ `W V_XZ_V R_U T`^a`_V_ed5 TcZeVcZR' e`]VcR_TVd'R_U UReR daVTZWZVU Sj V_XZ_V ^R_fWRTefcVc)
,1),. 6VOQVM D\WZIOM IVL AZM[MZ^I\QWV # - #
GcVdVcgReZ`_ R_U UVacVdVcgReZ`_ W`c eYV V_XZ_V R_U RTTVd(d`cZVd*djdeV^d)
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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\' c`eR(eZ`_R] daVVU6
Gc`aV]]Vc d]Za6
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K`cbfV6
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MZScReZ`_ R_U cVd`_R_TV)
,2)- AZWXMTTMZ 4WV[\Z]K\QWV , - #
9`_decfTeZ`_ ^VeY`Ud R_U ^ReVcZR]d fdVU Z_ h``UV_'T`^a`dZeV R_U ^VeR] ac`aV]]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_Xac`aV]]Vc6
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,2). AZWXMTTMZ AQ\KP 4WV\ZWT , - #
JaVVU T`_ec`] R_U aZeTY TYR_XV ^VeY`Ud' ^VTYR_ZTR] R_UV]VTecZTR]*V]VTec`_ZT6
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,2)/ AZWXMTTMZ DaVKPZWVQ[QVO # - #
Jj_TYc`_ZdZ_X R_U dj_TYc`aYRdZ_X VbfZa^V_e)
,2)0 AZWXMTTMZ ;KM AZW\MK\QWV , - #
=]fZU R_U V]VTecZTR] UV(ZTZ_X VbfZa^V_e)
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8]RUV ecRT\Z_X6
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Gc`aV]]Vc acVdVcgReZ`_ R_U UVacVdVcgReZ`_
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For Training Purpose Only Page 116
6 8 3� Fuuj sin} � NN� �Gfxnh� J } frnsfynts� Xyfsifwi�� nx� frj sij i� fx� ktqqt| x?�
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H fyj ltw~ � F2 7 5 � rzqyn2 hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� 7 : � rnszyj x3�
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H fyj ltw~ � G7 2 : 5 � rzqyn2hmtnhj � fsi� 5 � j xxf~ � vzj xyntsx3� Ynrj � fqqt| j i� ; : � rnszyj x3�@�
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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
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For Training Purpose Only Page 118
"3
3\\QZPUc <<
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,).) <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`_)
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,)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)
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daVTZWZVU Z_ aRcRXcRaY ,),-) 7 WRZ]VU ^`Uf]V ^Rj _`e SV cVeR\V_ W`cRe ]VRde 4+ URjd W`]]`hZ_X eYV UReV `W eYV WRZ]VU ^`Uf]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 ^`Uf]V hYV_ eYV WRZ]VU ^`Uf]V ^Rj SVcVeR\V_ RWeVc .+ URjd)
,),-) KYV 0 jVRc eZ^V aVcZ`U daVTZWZVU Z_ aRcRXcRaY ,),, U`Vd _`e Raa]j e`eY`dV ^`Uf]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_`eYVc dfTY TReVX`cj `c dfSTReVX`cj ViR^Z_ReZ`_)
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9ReVX`cj 8,(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU
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9ReVX`cj 8-(.+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU/+ ^Z_feVd)
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9ReVX`cj 8,(0+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU
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For Training Purpose Only Page 119
"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)
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9ReVX`cj 7(E`_V)
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-0 ^Z_feVd)
9ReVX`cj 8-(/+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU0+ ^Z_feVd)
-)0) JfS[VTe D`Uf]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 D`Uf]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)
9ReVX`cj 8-(1+ ^f]eZ(TY`ZTV R_U + VddRj bfVdeZ`_d) KZ^V R]]`hVU20 ^Z_feVd)
-)2) JfS[VTe D`Uf]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 D`Uf]V 3 8RdZT 7Vc`Uj_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 D`Uf]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 # ++.)++, # ,/,
For Training Purpose Only Page 120
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-),+) JfS[VTe D`Uf]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 D`Uf]V ,,R KfcSZ_V 7Vc`a]R_V 7Vc`Uj_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 D`Uf]V ,,S GZde`_ 7Vc`a]R_V 7Vc`Uj_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 D`Uf]V ,- ?V]ZT`aeVc 7Vc`Uj_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 D`Uf]V ,. 7ZcTcRWe 7Vc`Uj_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 D`Uf]V ,/ Gc`af]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 D`Uf]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 D`Uf]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 # ++.)++, # ,/-
For Training Purpose Only Page 121
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-),3) JfS[VTe D`Uf]V ,2 Gc`aV]]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 # ++.)++, # ,/.
For Training Purpose Only Page 122
"3
3\\QZPUc <<<
EaXM \ZIQVQVO IVL 6`IUQVI\QWV D\IVLIZL
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C V g V ] , > V _ V c R ] W R ^ Z ] Z R c Z d R e Z ` _
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,) 9`fcdV `S[VTeZgVd5 La`_ T`^a]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 Z^a`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
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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`^a]VeZ`_ `W eYZd CVgV] - IR^a R_UKcR_dZe ecRZ_Z_X' eYV defUV_e hZ]] SV RS]V e`5
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RSZ]Zej R_U d`fcTVd)
/) @UV_eZWj eYV ]`TReZ`_d `W eYV acZ_TZaR] T`^a`_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 cR^a 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 # ++.)++, # ,//
For Training Purpose Only Page 124
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2) ;V^`_decReV ac`WZTZV_Tj Z_ fdV `W TcVh cVa`ced R_U `_(S`RcU cVa`ceZ_XdjdeV^d $^Z_`c ec`fS]VdY``eZ_X% R_U UVeVc^Z_V RZcTcRWe RZch`ceYZ_Vdd aVceYV D<C*9;C)
3) @UV_eZWj R_U fdV Raac`acZReV U`Tf^V_eReZ`_)
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$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`^a`_V_ed f_ZbfV e` RZcTcRWeejaV)
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8]RUV ecRT\Z_X R_U gZScReZ`_ R_R]jdZd # # # # . , . , #
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For Training Purpose Only Page 125
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7Vc`a]R_Vd
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7Zc Jfaa]j . , . , . , . , ,
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GcVddfcZdReZ`_ . , # # # # # # ,
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# , # # # # # # .
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?jUcRf]ZT G`hVc . , . , . , . , ,
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G`]NUZQ 7ZSUZQ^2
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@_]Ve . , # # . , # # #
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For Training Purpose Only Page 126
"3
7Vc`a]R_Vd
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=7;<9 - , # # - , # # .
7Zc JjdeV^d . , # # . , # # #
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<_XZ_V @_UZTReZ_X JjdeV^d . , # # . , # # .
G`hVc 7fX^V_eReZ`_ JjdeV^d . , # # # # # # #
KfcS`(ac`a <_XZ_Vd . , # # # # # # #
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<_XZ_V D`_Ze`cZ_X R_U >c`f_U FaVcReZ`_ . , # # . , # # #
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For Training Purpose Only Page 127
"3
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For Training Purpose Only Page 128
"3
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For Training Purpose Only Page 129
Part-66 Appendix IV
Experience requirement for extending a part-66 Aircraft maintenance licence
For Training Purpose Only Page 130
"3
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For Training Purpose Only Page 131
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For Training Purpose Only Page 133
Part-66 Appendix VI
Aircraft Maintenance Licence referred to in Annex III (Part-66)
For Training Purpose Only Page 136
6 : 3� ymj � ktqqt| nsl� Fuuj sin} � [ N� nx� fiij i?
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7 3� Ymj �ithzrj sy�rzxy�gj �uwnsyj i�ns�ymj �xyfsifwinxj i�ktwr�xmt| s�gzy�rf~ �gj �wj izhj i�ns�xn� j �yt�fhhtrrtifyj �nyx� htruzyj w� lj sj wfynts� nk� ij xnwj i3� \ mj s� ymj � xn� j � nx� wj izhj i� hfwj � xmtzqi� gj � j } j whnxj i� yt� j sxzwj � xzkknhnj sy�xufhj � nx� f{fnqfgqj � ns� ymtxj � uqfhj x� | mj wj � tkknhnfq� xj fqx4xyfrux� fwj � wj vznwj i3� H truzyj w� lj sj wfyj i� ithzrj syx�sj j i� sty� mf{j � fqq� ymj � gt} j x� nshtwutwfyj i� | mj s� fs~ � xzhm� gt} � wj rfnsx� gqfsp� xt� qtsl� fx� ymj � ithzrj sy� hfs�hqj fwq~ � gj � wj htlsnxj i� fx� fs� fnwhwfky� rfnsyj sfshj � qnhj shj � nxxzj i� ns� fhhtwifshj � | nym� Fssj } � NNN� -Ufwy2 ; ; . 3�
8 3� Ymj �ithzrj sy�rf~ �gj �uwnsyj i�ns�ymj �J slqnxm�tw�ymj �tkknhnfq�qfslzflj �tk�ymj �R j rgj w�Xyfyj �htshj wsj i1�j } hj uy�ymfy�nk�ymj �tkknhnfq�qfslzflj �tk�ymj �R j rgj w�Xyfyj �htshj wsj i�nx�zxj i1�f�xj htsi�J slqnxm�htu~ �rzxy�gj �fyyfhmj i�ktw� fs~ � qnhj shj � mtqij w� ymfy� | twpx� tzyxnij � ymfy� R j rgj w� Xyfyj � yt� j sxzwj � zsij wxyfsinsl� ktw� ymj � uzwutxj � tk�rzyzfq� wj htlsnynts3�
9 3� J fhm� qnhj shj � mtqij w� rzxy� mf{j � f� zsnvzj � qnhj shj � szrgj w� gfxj i� zuts� f� S fyntsfq� nij synknj w� fsi� fs� fqumf2 �szrj wnh� ij xnlsfytw3�
: 3� Ymj �ithzrj sy�rf~ �mf{j �ymj �uflj x�ns�fs~ �twij w�fsi�sj j i�sty�mf{j �xtrj �tw�fs~ �in{nij w�qnsj x�fx�qtsl�fx�ymj �nsktwrfynts� htsyfnsj i� nx� utxnyntsj i� xzhm� ymfy� j fhm� uflj � qf~ tzy�hfs� hqj fwq~ �gj � nij synknj i� | nym� ymj � ktwrfy� tk�ymj � j } fruqj � tk� ymj � fnwhwfky�rfnsyj sfshj � qnhj shj � htsyfnsj i� mj wj ns3�
; 3� Ymj � ithzrj sy� rf~ � gj � uwj ufwj i� -n.� g~ � ymj � htruj yj sy� fzymtwny~ � tk� ymj � R j rgj w� Xyfyj � tw� -nn.� g~ � fs~ � rfnsyj sfshj � twlfsnxfynts�fuuwt{j i�ns� fhhtwifshj �| nym� Fssj } � NN� -Ufwy2 6 9 : .� nk� ymj � htruj yj sy� fzymtwny~ �flwj j x�xt�fsi�xzgoj hy�yt�f�uwthj izwj �ij {j qtuj i�fx�ufwy�tk�ymj �rfnsyj sfshj �twlfsnxfynts�j } utxnynts�wj kj wwj i�yt�ns�utnsy�6 9 : 3F3< 5 � tk� Fssj } � NN� -Ufwy2 6 9 : . 1� j } hj uy�ymfy� ns� fqq�hfxj x�ymj � htruj yj sy� fzymtwny~ �tk� ymj � R j rgj w� Xyfyj � | nqq�nxxzj � ymj � ithzrj sy3�
< 3� Ymj � uwj ufwfynts� tk� fs~ � hmfslj � yt� fs� j } nxynsl� fnwhwfky� rfnsyj sfshj � qnhj shj � rf~ � gj � hfwwnj i� tzy� -n.� g~ � ymj �htruj yj sy�fzymtwny~ �tk�ymj �R j rgj w�Xyfyj �tw� -nn.�fs~ �rfnsyj sfshj �twlfsnxfynts�fuuwt{j i�ns�fhhtwifshj �| nym�Fssj } �NN�-Ufwy2 6 9 : .�nk�ymj �htruj yj sy�fzymtwny~ �flwj j x�xt�fsi�xzgoj hy�yt�f�uwthj izwj �ij {j qtuj i�fx�ufwy�tk�ymj �rfnsyj sfshj �twlfsnxfynts�j } utxnynts�wj kj wwj i�yt�ns�utnsy�6 9 : 3F3< 5 �tk�Fssj } � NN� -Ufwy2 6 9 : .1� j } hj uy�ymfy�ns�fqq�hfxj x� ymj � htruj yj sy� fzymtwny~ � tk� ymj � R j rgj w� Xyfyj � | nqq� hmfslj � ymj � ithzrj sy3�
= 3� Ymj �fnwhwfky�rfnsyj sfshj �qnhj shj �tshj �nxxzj i�nx�wj vznwj i�yt�gj �pj uy�g~ �ymj �uj wxts�yt�| mtr�ny�fuuqnj x�ns�ltti�htsinynts� fsi� | mt� xmfqq� wj rfns� fhhtzsyfgqj � ktw� j sxzwnsl� ymfy� st� zsfzymtwnxj i� j sywnj x� fwj � rfij 3�
> 3� Kfnqzwj � yt� htruq~ � | nym� ufwflwfum� = � rf~ � ns{fqnifyj � ymj � ithzrj sy� fsi� htzqi� qj fi� yt� ymj � mtqij w� sty� gj nsl�uj wrnyyj i�yt�mtqi�fs~ �hj wynknhfynts�fzymtwnxfynts�uzwxzfsy�yt�utnsy�6 9 : 3F38 : �tk�Fssj } �NN�-Ufwy2 6 9 : .�fsi�rf~ �wj xzqy� ns� uwtxj hzynts� zsij w� sfyntsfq� qf| 3�
6 5 3� Ymj �fnwhwfky�rfnsyj sfshj �qnhj shj �ij qn{j wj i�ns�fhhtwifshj �| nym�Fssj } �NNN�-Ufwy2 ; ; .�nx�wj htlsnxj i�ns�fqq�R j rgj w�Xyfyj x� fsi� ny� nx� sty� sj hj xxfw~ � yt� j } hmfslj � ymj � ithzrj sy� | mj s� | twpnsl� ns� fstymj w� R j rgj w� Xyfyj 3�
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For Training Purpose Only Page 137
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For Training Purpose Only Page 138
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For Training Purpose Only Page 139
AMC-66 Appendix I
Aircraft type ratings for Part-66 aircraft Maintenance licence
For Training Purpose Only Page 140
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
For Training Purpose Only Page 141
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.
For Training Purpose Only Page 142
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)
For Training Purpose Only Page 143
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
One-Eleven 400 series
AIRBUS
One-Eleven 500 series
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)
For Training Purpose Only Page 144
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 145
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 146
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 147
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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
B747-400F/SF(BCF)/LCF
Boeing 747-400 (PW 4000)
B747-400
B747-400F/SF(BCF)/LCF
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)
For Training Purpose Only Page 148
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 149
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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
DHC-8-102 DHC-8 Series 100
DHC-8-103 DHC-8 Series 100
DHC-8-106 DHC-8 Series 100
DHC-8-201 DHC-8 Series 200
DHC-8-202 DHC-8 Series 200
DHC-8-301 DHC-8 Series 300
DHC-8-311 DHC-8 Series 300
DHC-8-314 DHC-8 Series 300
DHC-8-315 DHC-8 Series 300
Bombardier DHC-8-100/200/300 (PWC PW 120)
DHC-8-400 DHC-8 Series 400
DHC-8-401 DHC-8 Series 400
DHC-8-402 DHC-8 Series 400
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)
For Training Purpose Only Page 150
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 151
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 152
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 153
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
Designation
F-27A to -M
FH-227
FH-227B
FH-227C
FH-227D
(FOKKER-FAIRCHILD) MARYLAND
AIR INDUSTRIES
FH-227E
F27 Mark 100 Friendship
F27 Mark 200 Friendship
F27 Mark 300 Friendship
F27 Mark 400 Friendship
F27 Mark 500 Friendship
F27 Mark 600 Friendship
F27 Mark 700 Friendship
Fokker F27 / Fairchild F-27/FH-227 (RRD Dart)
F27 Mark 050 Fokker 50
F27 Mark 0502 Fokker 50
F27 Mark 0604 Fokker 60
Fokker 50/60 Series (PWC PW 125/127)
F28 Mark 1000 Fellowship
F28 Mark 1000C Fellowship
F28 Mark 2000 Fellowship
F28 Mark 3000 Fellowship
F28 Mark 3000C Fellowship
F28 Mark 3000R Fellowship
FOKKER SERVICES
F28 Mark 3000RC Fellowship
Fokker F28 Series (RRD Spey)
For Training Purpose Only Page 154
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
Designation
F28 Mark 4000 Fellowship Fokker F28 Series (RRD Spey)
F28 Mark 0100 Fokker 100
FOKKER SERVICES
F28 Mark 0070 Fokker 70
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)
For Training Purpose Only Page 155
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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"
DH.125 series 3 "Hawker Siddeley"
HS.125 series 3 "Hawker Siddeley"
HS.125 series F3 "Hawker Siddeley"
BH.125 series 400 "Beechcraft Hawker"
DH.125 series 400 "Hawker Siddeley"
HS.125 series F400 "Hawker Siddeley"
BH.125 series 600 "Beechcraft Hawker"
HS.125 series 600 "Hawker Siddeley"
HS.125 series F600 "Hawker Siddeley"
BAe 125 Series /700/800 (Honeywell TFE731)
Hawker 750 Hawker 750
Hawker 800XP Hawker 800XP
Hawker 850XP Hawker 850XP
HAWKER BEECHCRAFT Corporation
Hawker 900XP Hawker 900XP
BAe 125 Series 750/800XP/850XP/900XP (Honeywell TFE731)
For Training Purpose Only Page 156
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
Designation
DH.125 series 1 "Hawker Siddeley"
HS.125 series 1 "Hawker Siddeley"
DH.125 series 3 "Hawker Siddeley"
HS.125 series 3 "Hawker Siddeley"
HS.125 series F3 "Hawker Siddeley"
DH.125 series 400 "Hawker Siddeley"
HS.125 series 400 "Hawker Siddeley"
BH.125 series 400 "Beechcraft Hawker"
HS.125 series F400 "Hawker Siddeley"
BH.125 series 600 "Beechcraft Hawker"
HS.125 series 600 "Hawker Siddeley"
HS.125 series F600 "Hawker Siddeley"
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)
For Training Purpose Only Page 157
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 158
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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)
For Training Purpose Only Page 159
3 Type rating endorsement 1. TC holder 2 Aeroplanes Model Commercial
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
DC-9-82 (MD-82) Series
DC-9-83 (MD-83) Series
DC-9-87 (MD-87) Series
McDONNELL DOUGLAS
Corporation
MD-88
MD-80 Series (PW JT8D)
For Training Purpose Only Page 160
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)
For Training Purpose Only Page 161
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)
For Training Purpose Only Page 162
2. Aeroplanes of 5700 kg and below, requiring type training and individual type
rating (A-tr) 1 TC Holder 2 Aeroplanes
Model Commercial Designation
3 Type rating endorsement
AERO VODOCHODY Ae 270 Aero Ae-270 (PWC PT6)
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
CESSNA AIRCRAFT Company
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
Beech 90 Series (PWC PT6)
For Training Purpose Only Page 163
1 TC Holder 2 Aeroplanes
Model Commercial Designation
3 Type rating endorsement
200/A200
200C/A200C
200CT/A200CT
200T
B200
B200C
B200CT
B200T
B200GT
B200CGT
Beech 200 Series (PWC PT6)
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)
For Training Purpose Only Page 164
Annex to ED Decision 2010/011/R 14/12/2010
List 2
1 TC Holder 2 Aeroplanes Model Commercial Designation
3 Type rating endorsement
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)
For Training Purpose Only Page 165
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)
For Training Purpose Only Page 166
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 AIRCRAFT Company
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)
For Training Purpose Only Page 167
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)
HAWKER BEECHCRAFT Corporation
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)
For Training Purpose Only Page 168
Annex to ED Decision 2010/011/R 14/12/2010
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)
For Training Purpose Only Page 169
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)
For Training Purpose Only Page 170
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)
HAWKER BEECHCRAFT Corporation
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)
For Training Purpose Only Page 171
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)
For Training Purpose Only Page 172
Annex to ED Decision 2010/011/R 14/12/2010
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)
For Training Purpose Only Page 173
7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for
type examinations and group ratings
No aircraft in this list.
For Training Purpose Only Page 174
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)
For Training Purpose Only Page 175
9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for
type examinations and group ratings
TC holder Type rating endorsement
Diamond DA42 Series (Thielert) DIAMOND AIRCRAFT Industries
Diamond DA42 Series (Austro Engine)
For Training Purpose Only Page 176
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)
For Training Purpose Only Page 177
11. Multi-engine helicopters (MEH), requiring type training and individual type
rating
1 TC Holder 2 Helicopter Model Commercial Designation
3 Type rating endorsement
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)
427 Bell 427 (PWC PW207D)
429 Bell 429 (PWC PW207D)
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)
For Training Purpose Only Page 178
1 TC Holder 2 Helicopter
Model Commercial Designation
3 Type rating endorsement
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)
For Training Purpose Only Page 179
Annex to ED Decision 2010/011/R 14/12/2010
List 11
1 TC Holder 2 Helicopter Model Commercial Designation
3 Type rating endorsement
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)
For Training Purpose Only Page 180
12. Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings 1 TC Holder 2 Helicopter
Model Commercial Designation
3 Type rating endorsement
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)
For Training Purpose Only Page 181
Annex to ED Decision 2010/011/R 14/12/2010
List 12
1 TC Holder 2 Helicopter Model Commercial Designation
3 Type rating endorsement
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)
For Training Purpose Only Page 182
13. Helicopters – Single piston engines (HSPE), eligible for type examinations and group ratings 1 TC Holder 2 Helicopter 3 Type rating endorsement
Model Commercial Designation
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)
For Training Purpose Only Page 183
AMC Part-66 Appendix II
Aircraft Type Practical Experience
List of Task’s
For Training Purpose Only Page 184
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
For Training Purpose Only Page 186
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.
For Training Purpose Only Page 187
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.
For Training Purpose Only Page 188
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
For Training Purpose Only Page 189
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.
For Training Purpose Only Page 190
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.
For Training Purpose Only Page 191