text: AMC & GM to Part-66 Issue 2, Amendment 8

text: Annex II to ED Decision 2023/019/R Page 1 of 148

text: Annex II to ED Decision 2023/019/R Page 2 of 148

text: Annex II to ED Decision 2023/019/R Page 3 of 148

text: Annex II to ED Decision 2023/019/R Page 4 of 148

text: Annex II to ED Decision 2023/019/R Page 5 of 148

text: Annex II to ED Decision 2023/019/R Page 6 of 148

text: Annex II to ED Decision 2023/019/R Page 7 of 148

text: Annex II to ED Decision 2023/019/R Page 8 of 148

text: Annex II to ED Decision 2023/019/R Page 9 of 148

text: Annex II to ED Decision 2023/019/R Page 10 of 148

text: Annex II to ED Decision 2023/019/R Page 11 of 148

text: Annex II to ED Decision 2023/019/R Page 12 of 148

text: Annex II to ED Decision 2023/019/R Page 13 of 148

text: Annex II to ED Decision 2023/019/R Page 14 of 148

text: A1 B1

text: B2 B3 A3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 15 of 148

text: A1 B1

text: B2 B3 A3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 16 of 148

text: A1 B1

text: B2 B3 A3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 17 of 148

text: A1 B1

text: B2 B3 A3 B2L A4

text: A3 B3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 18 of 148

text: A3 B3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 19 of 148

text: A3 B3 B2L A4

text: Annex II to ED Decision 2023/019/R Page 20 of 148

text: Annex II to ED Decision 2023/019/R Page 21 of 148

text: Annex II to ED Decision 2023/019/R Page 22 of 148

text: Annex II to ED Decision 2023/019/R Page 23 of 148

text: Annex II to ED Decision 2023/019/R Page 24 of 148

text: Annex II to ED Decision 2023/019/R Page 25 of 148

text: Annex II to ED Decision 2023/019/R Page 26 of 148

text: Annex II to ED Decision 2023/019/R Page 27 of 148

text: Annex II to ED Decision 2023/019/R Page 28 of 148

text: Annex II to ED Decision 2023/019/R Page 29 of 148

text: Annex II to ED Decision 2023/019/R Page 30 of 148

text: Annex II to ED Decision 2023/019/R Page 31 of 148

text: Annex II to ED Decision 2023/019/R Page 32 of 148

text: Annex II to ED Decision 2023/019/R Page 33 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 34 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 35 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 36 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 37 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 38 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 39 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 40 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 41 of 148

text: SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 42 of 148

text: Annex II to ED Decision 2023/019/R Page 43 of 148

text: Annex II to ED Decision 2023/019/R Page 44 of 148

text: Annex II to ED Decision 2023/019/R Page 45 of 148

text: Annex II to ED Decision 2023/019/R Page 46 of 148

text: Annex II to ED Decision 2023/019/R Page 47 of 148

text: C/N: Communication and Navigation; Ins.: Instruments; A/F: Autoflight; Sur.: Surveillance; A/S: Airframe and Systems LEVEL MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES

text: Annex II to ED Decision 2023/019/R Page 48 of 148

text: Annex II to ED Decision 2023/019/R Page 49 of 148

text: Annex II to ED Decision 2023/019/R Page 50 of 148

text: Annex II to ED Decision 2023/019/R Page 51 of 148

text: Annex II to ED Decision 2023/019/R Page 52 of 148

text: Annex II to ED Decision 2023/019/R Page 53 of 148

text: Annex II to ED Decision 2023/019/R Page 54 of 148

text: Annex II to ED Decision 2023/019/R Page 55 of 148

text: Annex II to ED Decision 2023/019/R Page 56 of 148

text: A3 B1.3

text: Annex II to ED Decision 2023/019/R Page 57 of 148

text: A3 B1.3

text: Annex II to ED Decision 2023/019/R Page 58 of 148

text: A3 B1.3

text: Annex II to ED Decision 2023/019/R Page 59 of 148

text: A3 B1.3

text: B1.4 A4 B3

text: Annex II to ED Decision 2023/019/R Page 60 of 148

text: B1.4 A4 B3

text: Annex II to ED Decision 2023/019/R Page 61 of 148

text: B1.4 A4 B3

text: Annex II to ED Decision 2023/019/R Page 62 of 148

text: Annex II to ED Decision 2023/019/R Page 63 of 148

text: Annex II to ED Decision 2023/019/R Page 64 of 148

text: Annex II to ED Decision 2023/019/R Page 65 of 148

text: Annex II to ED Decision 2023/019/R Page 66 of 148

text: Annex II to ED Decision 2023/019/R Page 67 of 148

text: Annex II to ED Decision 2023/019/R Page 68 of 148

text: Annex II to ED Decision 2023/019/R Page 69 of 148

text: AND SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 70 of 148

text: AND SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 71 of 148

text: AND SYSTEMS A1 A2 B1.1 B1.2 B3

text: Annex II to ED Decision 2023/019/R Page 72 of 148

text: Annex II to ED Decision 2023/019/R Page 73 of 148

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

text: Annex II to ED Decision 2023/019/R Page 74 of 148

text: Annex II to ED Decision 2023/019/R Page 75 of 148

text: Annex II to ED Decision 2023/019/R Page 76 of 148

text: Annex II to ED Decision 2023/019/R Page 77 of 148

text: Annex II to ED Decision 2023/019/R Page 78 of 148

text: Annex II to ED Decision 2023/019/R Page 79 of 148

text: Annex II to ED Decision 2023/019/R Page 80 of 148

text: Annex II to ED Decision 2023/019/R Page 81 of 148

text: Annex II to ED Decision 2023/019/R Page 82 of 148

text: Annex II to ED Decision 2023/019/R Page 83 of 148

text: Annex II to ED Decision 2023/019/R Page 84 of 148

text: Annex II to ED Decision 2023/019/R Page 85 of 148

text: Annex II to ED Decision 2023/019/R Page 86 of 148

text: Annex II to ED Decision 2023/019/R Page 87 of 148

text: Annex II to ED Decision 2023/019/R Page 88 of 148

text: Annex II to ED Decision 2023/019/R Page 89 of 148

text: Annex II to ED Decision 2023/019/R Page 90 of 148

text: Annex II to ED Decision 2023/019/R Page 91 of 148

text: Annex II to ED Decision 2023/019/R Page 92 of 148

text: Annex II to ED Decision 2023/019/R Page 93 of 148

text: Annex II to ED Decision 2023/019/R Page 94 of 148

text: Annex II to ED Decision 2023/019/R Page 95 of 148

text: Annex II to ED Decision 2023/019/R Page 96 of 148

text: Annex II to ED Decision 2023/019/R Page 97 of 148

text: Annex II to ED Decision 2023/019/R Page 98 of 148

text: Annex II to ED Decision 2023/019/R Page 99 of 148

text: Annex II to ED Decision 2023/019/R Page 100 of 148

text: Annex II to ED Decision 2023/019/R Page 101 of 148

text: Annex II to ED Decision 2023/019/R Page 102 of 148

text: Annex II to ED Decision 2023/019/R Page 103 of 148

text: Annex II to ED Decision 2023/019/R Page 104 of 148

text: Annex II to ED Decision 2023/019/R Page 105 of 148

text: Annex II to ED Decision 2023/019/R Page 106 of 148

text: Annex II to ED Decision 2023/019/R Page 107 of 148

text: Annex II to ED Decision 2023/019/R Page 108 of 148

text: Annex II to ED Decision 2023/019/R Page 109 of 148

text: Annex II to ED Decision 2023/019/R Page 110 of 148

text: Annex II to ED Decision 2023/019/R Page 111 of 148

text: Annex II to ED Decision 2023/019/R Page 112 of 148

text: Annex II to ED Decision 2023/019/R Page 113 of 148

text: Annex II to ED Decision 2023/019/R Page 114 of 148

text: Annex II to ED Decision 2023/019/R Page 115 of 148

text: Annex II to ED Decision 2023/019/R Page 116 of 148

text: Annex II to ED Decision 2023/019/R Page 117 of 148

text: Annex II to ED Decision 2023/019/R Page 118 of 148

text: Annex II to ED Decision 2023/019/R Page 119 of 148

text: Annex II to ED Decision 2023/019/R Page 120 of 148

text: Annex II to ED Decision 2023/019/R Page 121 of 148

text: Annex II to ED Decision 2023/019/R Page 122 of 148

text: Annex II to ED Decision 2023/019/R Page 123 of 148

text: Annex II to ED Decision 2023/019/R Page 124 of 148

text: Annex II to ED Decision 2023/019/R Page 125 of 148

text: Annex II to ED Decision 2023/019/R Page 126 of 148

text: Annex II to ED Decision 2023/019/R Page 127 of 148

text: Annex II to ED Decision 2023/019/R Page 128 of 148

text: Annex II to ED Decision 2023/019/R Page 129 of 148

text: Annex II to ED Decision 2023/019/R Page 130 of 148

text: Annex II to ED Decision 2023/019/R Page 131 of 148

text: Annex II to ED Decision 2023/019/R Page 132 of 148

text: Annex II to ED Decision 2023/019/R Page 133 of 148

text: Annex II to ED Decision 2023/019/R Page 134 of 148

text: Annex II to ED Decision 2023/019/R Page 135 of 148

text: Annex II to ED Decision 2023/019/R Page 136 of 148

text: Annex II to ED Decision 2023/019/R Page 137 of 148

text: Annex II to ED Decision 2023/019/R Page 138 of 148

text: Annex II to ED Decision 2023/019/R Page 139 of 148

text: Annex II to ED Decision 2023/019/R Page 140 of 148

text: Annex II to ED Decision 2023/019/R Page 141 of 148

text: Annex II to ED Decision 2023/019/R Page 142 of 148

text: Annex II to ED Decision 2023/019/R Page 143 of 148

text: Annex II to ED Decision 2023/019/R Page 144 of 148

text: Annex II to ED Decision 2023/019/R Page 145 of 148

text: Annex II to ED Decision 2023/019/R Page 146 of 148

text: Annex II to ED Decision 2023/019/R Page 147 of 148

text: Annex II to ED Decision 2023/019/R Page 148 of 148

identifier: AMC & GM to Part-66 — Issue 2, Amendment 8

beslut: ED Decision 2023/019/R

title: AMC & GM to Part-66 — Issue 2, Amendment 8

text: Acceptable Means of Compliance and Guidance Material to Annex III (Part-66) to

text: Commission Regulation (EU) No 1321/2014

text: — Issue 2, Amendment 8 Annex II to ED Decision 2023/019/R ‘AMC and GM to Part-66 — Issue 2, Amendment 8’ The text of the amendment is arranged to show deleted, new or amended text as follows: — deleted text is struck through; — new or amended text is highlighted; — an ellipsis ‘[…]’ indicates that the rest of the text is unchanged. Note to the reader In amended, and in particular in existing (that is, unchanged) text, ‘Agency’ is used interchangeably with ‘EASA’. The interchangeable use of these two terms is more apparent in the consolidated versions. Therefore, please note that both terms refer to the ‘European Union Aviation Safety Agency (EASA)’. Annex III to Decision 2015/029/R of 17 December 2015 of the Executive Director of the Agency is amended as follows:

text: ANNEX III (PART-66)

text: GENERAL

text: AMC1 66.1(a) Competent Authority

text: […] The purpose of 66.1(a)2 is to allow the possibility for a person who already holds a Part-66 licence issued by one Member State (i.e. Member State X) to replace it by a Part-66 licence issued by another Member State (i.e. Member State Y). This may be useful, for example, in cases where a person holding a licence from ‘Member State X’ is developing his/her career in a maintenance organisation located in ‘Member State Y’. In this case, this person may need to endorse new type ratings based on courses directly approved by the competent authority of ‘Member State Y’ or may need to endorse new licence (sub)categories based on basic examinations performed by the competent authority of ‘Member State Y’. […]

text: SECTION A — TECHNICAL REQUIREMENTS

text: SUBPART A — AIRCRAFT MAINTENANCE LICENCE GM1 66.A.5 Aircraft groups

text: The following table summarises the applicability of categories/subcategories of Part-66 licences versus the groups/subgroups of aircraft:

text: Category/subcategory L

text: A, B1 L1C L2C L3H L4H

text: B2 B2L B3

text: and C and and and and L5 Groups L1 L2 L3G L4G

text: 1 — Complex motor-powered aircraft — Multi-engine helicopters — other than piston-engine

text: X X

text: Aaeroplanes above FL290 — Aircraft with fly-by-wire systems — Any other aircraft when defined by the Agency

text: Category/subcategory L

text: A, B1 L1C L2C L3H L4H

text: B2 B2L B3

text: X X

text: — Gas airships other than ELA2

text: 2 2a: Single-turboprop aeroplanes

text: 2b: Single-turbine helicopters X X X

text: 2c: Single-piston-engine helicopters

text: X X X

text: — Piston-engine aeroplanes

text: 3 Piston engine aeroplanes (nonpressurised of 2 000 kg MTOM

text: and below) X X X X

text: — Non-pressurised ELA2 pistonengine aeroplanes

text: X X X X X

text: — ELA1 piston-engine aeroplanes 4

text: — Sailplanes X X X X — Powered sailplanes X X X — Balloons X X X — Airships not in Group 1 X X X X

text: GM1 66.A.20(a) Privileges

text: […] 5. The category C licence 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 category B1, B2, B2L, B3 and L support staff, as appropriate, have signed for the maintenance tasks 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, B2, B2L, B3 and L support staff, as appropriate, before issue of the certificate of release to service. Only category C personnel who also hold category B1, B2, B2L, B3 or L qualifications may perform both roles in base maintenance. […]

text: AMC1 66.A.30(a) Basic experience requirements

text: 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 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 support staff. 41. Maintenance experience on operating aircraft: — means the experience of being involved in maintenance tasks on aircraft which are being operated by airlines, air taxi organisations, aero clubs, owners, etc., as relevant to the licence category/subcategory; — should cover a wide range of tasks in terms of length, complexity and variety; — aims at gaining sufficient experience in the real environment of maintenance as opposed to only the training school environment; — may be gained within different types of maintenance organisations (Part-145, M.A. Subpart F, Part-CAO, FAR-145, etc.) or under the supervision of independent certifying staff; — Mmay be combined with Part-147 approved training (or other training approved by the competent authority) so that periods of training can be intermixed with periods of experience, similar to an apprenticeship; — may be full-time or part-time, either as a professional or on a voluntary basis; — in the case of the L licence, it is acceptable that the 1 or 2 years of experience required by 66.A.30(a)(2b) covers maintenance performed only during the weekends (or equivalent periods) as long as the applicant has achieved a sufficient level of competency related to the applicable licence subcategory as attested by the corresponding statement(s) issued by the maintenance organisation(s) or independent certifying staff that supervised the applicant. 32. A skilled worker is a person who has successfully completed a 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. 53. In the case of an applicant for a licence, including several categories/subcategories, it is acceptable to combine the periods of experience as long as there is a sufficient experience for each category/subcategory during the required period. Examples: include the following. — Application for a B1.1 (turbine aeroplanes) + B1.3 (turbine helicopters): Tthe Regulation requires 5 years of experience for B1.1 and 5 years of experience for B1.3 for an applicant with no relevant previous technical training:. — It is not acceptable to combine the experience in a single 5-year period where the applicant has been working for 3 years on turbine aeroplanes and 2 years on turbine helicopters. — However, it is acceptable to combine the experience in a single 5-year period if the applicant has been working for 5 years on turbine aeroplanes and turbine helicopters (for example, aeroplanes in the morning, helicopters in the afternoon, or a few days every week on aeroplanes and a few days every week on helicopters). — Application for a B1.1 (turbine aeroplanes) + B2 (avionics): Tthe Regulation requires 5 years of experience for B1.1 and 5 years of experience for B2 for an applicant with no relevant previous technical training. — It is not acceptable to combine the experience in a single 5-year period where the applicant has been working for 3 years on turbine aeroplanes (with no avionics work) and 2 years on avionics systems. — However, it is acceptable to combine the experience in a single 5-year period if the applicant has been working for 5 years on structures, powerplant, mechanical and electrical systems and avionics (for B1.1 tasks in the morning, B2 tasks in the afternoon, or a few days every week for B1.1 tasks and a few days every week for B2 tasks). — Application for a B1.1, B1.2, B1.3, B1.4 and B2: Tthe Regulation requires 5 years of experience for B1.1, B1.3 and B2, and 3 years of experience for B1.2 and B1.4 for an applicant with no relevant previous technical training. — In this case, it is very unlikely that the experience for each category/subcategory would be sufficient. 4. For a category C applicant that holds an academic degree, the participation in the performance of maintenance tasks on operating aircraft may include maintenance, maintenance planning, quality assurance, record-keeping, spare parts management and engineering development. ‘Experience in working in a civil aircraft maintenance environment on a representative selection of tasks directly associated with aircraft maintenance’ means experience gained at an organisation that is approved in accordance with Part-145, Part-CAO, Part-CAMO or similar, or experience in performing comparable work that is directly related to the continuing airworthiness of aircraft within a competent authority. Similar work performed on ‘Annex I aircraft’ or state aircraft may be acceptable as well. ‘Including 6 months of participation in the performance of base maintenance tasks’ on operating aircraft means experience gained through the active participation in base maintenance checks at maintenance organisations. If the applicant has acquired experience on operating CMPA, the corresponding category C licence should be issued. If the experience acquired has been limited to other than CMPA, then only the corresponding category C licence with respect to other than CMPA should be issued. While it is strongly recommended that the participation in the performance of maintenance on aircraft should be at the level required for the issue of a B1 or B2 licence, the objective of the required experience is to gain insight into the performance of base maintenance. The applicant for an academic category C licence should be aware of the type of maintenance carried out before the signature of support staff and understand their roles in the release-to-service process of base maintenance. It is encouraged that the future category C licence holder participates in both simple and complex tasks during their experience in base maintenance and gains insight in some aircraft critical systems. In the case presented in point 66.A.30(e), for the required experience gained outside the European civil regulatory framework, at least 1 year should be in a Part-145 or Part-CAO environment, including participation in the performance of base maintenance tasks for 6 months.

text: GM1 66.A.30(a) Basic experience requirements

text: The table below summarises the basic experience requirements for the category C licence.

text: To: Category C Category C From: for CMPA for other than CMPA

text: 3 years of experience as support staff, Holder of a licence with or both support staff and certifying B1.1, B1.3, B2, B3*B2L*, staff, in operating CMPA, including or L* 12 months as support staff in base 3 years of experience as certifying staff maintenance. or support staff, in operating other than 5 years of experience as support staff, CMPA, including 6 months as support or both support staff and certifying staff in base maintenance. Holder of a licence with staff, in operating CMPA, including B1.2, B1.4 or L5** 12months as support staff in base maintenance. 3 years of experience in working in an Holder of an academic 3 years of experience in working in an aircraft maintenance environment, on degree, in a relevant aircraft maintenance environment, on a representative selection of tasks that technical discipline, a representative selection of tasks that are directly associated with aircraft issued by a university or are directly associated with aircraft maintenance of operating other than any other higher maintenance of operating CMPA, CMPA, including 6 months of educational institution including 6 months of participation in participation in the performance of recognised by the the performance of base maintenance base maintenance tasks on operating competent authority tasks on operating CMPA. other than CMPA. 2 years of experience as B1, B2 or L5 support staff, or both support staff and certifying staff, including 6 months as support staff in base maintenance. Holding an academic degree: 2 years Holder of a licence with of experience in working in an aircraft category C for other than maintenance environment, on a CMPA representative selection of tasks that are directly associated with aircraft maintenance of operating CMPA, including 3 months of participation in the performance of base maintenance tasks on operating CMPA. Holder of a licence with Category C for CMPA includes category category C for CMPA C for other than CMPA. * Only applicable to category C for other than CMPA. ** Only applicable to category C for CMPA.

text: AMC1 66.A.30(e) Basic experience requirements

text: 1.(a) For categories A and L, the additional experience should be a minimum of 6 months in a civil maintenance environment. For categories B1, B2, B2L or B3, the additional experience should be a minimum of 12 months in a civil aircraft maintenance environment. If the licensing authority has established that the experience gained outside an aircraft maintenance organisation approved in accordance with Part-145 or Part-CAO is equivalent to that required by Part-66, the minimum additional experience in aircraft maintenance organisation(s) that is (are) approved in accordance with Part-145 or Part-CAO should be: (1) for categories A and L: 6 months; (2) for categories B1, B2, B2L, B3 and C: 12 months. 2.(b) Aircraft maintenance experience gained outside a civil aircraft maintenance environment may include aircraft maintenance experience gained in armed forces, coast guards, police etc. or in aircraft manufacturing. Experience in aircraft maintenance gained outside an aircraft maintenance organisation(s) that is (are) approved in accordance with Part-145 or Part-CAO may include experience in aircraft maintenance gained in the armed forces, coast guard, police, nationally approved organisations, organisations approved by non-EASA Member States, etc., or in aircraft manufacturing.

text: GM1 66.A.45 Endorsement with aircraft ratings

text: Aircraft rating requirements

text: Aircraft B1/B3/L licence B2/B2L licence C licence Group 1 aircraft, except (For B1) (For B2) airships

text: Individual TYPE RATING Individual TYPE RATING Individual TYPE RATING

text: — Complex motorpowered aircraft. Type training: Type training: Type training: — Multiple-engine — Theory + examination — Theory + examination — Theory + examination helicopters. — Practical + assessment — Practical + assessment — Other than piston- PLUS PLUS engine Aaeroplanes OJT (for first aircraft in OJT (for first aircraft in certified above FL290. licence subcategory) licence subcategory) — Aircraft equipped with fly-by-wire. — Other aircraft when defined by the Agency. […] […] […] […]

text: Aircraft rating requirements

text: Group 2 aircraft (For B1.1, B1.3, B1.4) (For B2)

text: Subgroups: Individual TYPE RATING Individual TYPE RATING Individual TYPE RATING (type training + OJT) or (type training + OJT) or type training or type 2a: single turboprop (type evaluation (type evaluation evaluation examination aeroplanes (*) examination + practical examination + practical experience) experience) 2b: single turbine Full SUBGROUP RATING engine helicopters (*) Full SUBGROUP RATING (For B2 and B2L) type training or type (type training + OJT) or evaluation examination 2c: single piston (type evaluation Full SUBGROUP RATING on at least engine helicopters (*) examination + practical based on demonstration 3 aircraft representative experience) on at least 3 of practical experience of that subgroup (*) Except those aircraft representative of classified in Group 1. that subgroup

text: Manufacturer Manufacturer Manufacturer SUBGROUP RATING SUBGROUP RATING SUBGROUP RATING

text: (type training + OJT) based on demonstration type training or type or (type evaluation of practical experience evaluation examination examination + on at least practical experience) on 2 aircraft representative at least 2 aircraft of that manufacturer representative subgroup of that manufacturer subgroup Group 3 aircraft (For B1.2) (For B2)

text: Piston engine Individual TYPE RATING Individual TYPE RATING Individual TYPE RATING aeroplanes (type training + OJT) or (type training + OJT) or type training or type (except those classified (type evaluation (type evaluation evaluation examination in Group 1) examination + practical examination + practical experience) experience)

text: Full GROUP 3 RATING

text: Full GROUP 3 RATING (For B2 and B2L) based on demonstration based on demonstration of practical experience of practical experience Full GROUP 3 RATING Limitations: based on demonstration — Pressuriszed aeroplanes of appropriate — Metal aeroplanes experience — Composite aeroplanes — Wooden aeroplanes — Metal tubing & and fabric Aaeroplanes

text: GM1 66.A.45(h)(ii)2 Endorsement with aircraft ratings

text: […] However, no the limitations referred to in 66.A.45(h)(ii) are possible for do not apply for the subcategories L1C, L2C, L3H, L4H and L4G. The ratings on these licences can only be obtained after demonstration of the appropriate experience representative of the full scope of the licence subcategory. […]

text: SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES

text: SUBPART B — ISSUE OF AN AIRCRAFT MAINTENANCE LICENCE

text: GM1 66.B.2 Means of compliance

text: ALTERNATIVE MEANS OF COMPLIANCE — GENERAL

text: (a) A competent authority may establish means to comply with the Regulation different from the AMC established by EASA. In that case, the competent authority is responsible for demonstrating how this (these) alternative means of compliance (AltMoC) establish compliance with the Regulation. (b) AltMoC used by a competent authority may also be used by other competent authorities only if processed again in accordance with point 66.B.2. (c) AltMoC issued by the competent authority may cover the following cases: — AltMoC to be used by persons under the oversight of the competent authority and made available to these persons; — AltMoC to be used by the authority itself to discharge its responsibilities.

text: AMC1 66.B.2(b);(c) Means of compliance

text: PROCESSING THE ALTERNATIVE MEANS OF COMPLIANCE

text: To meet the objective of points (b) and (c) of point 66.B.2: (a) the competent authority should establish the means to consistently evaluate over time that all the AltMoC used by itself or by the persons under its oversight allow for the establishment of compliance with the Regulation; (b) if the competent authority issues AltMoC for itself or for the persons under its oversight, it should: (1) make them available to all relevant persons; (2) notify the Agency as soon as the AltMoC is issued, including the information described in point (c) below; (c) the competent authority should provide the Agency with the following information: (1) a summary of the AltMoC; (2) the content of the AltMoC; (3) a statement that compliance with the Regulation is achieved; and (4) in support of that statement, an assessment demonstrating that the AltMoC reaches an acceptable level of safety, taking into account the level of safety provided by the corresponding EASA AMC. All these elements describing the AltMoC form an integral part of the records to be kept in accordance with point 66.B.20.

text: GM1 66.B.2(b);(c) Means of compliance

text: CASE WHERE THE REGULATION HAS NO CORRESPONDING EASA AMC

text: When there is no EASA AMC for a certain requirement in the Regulation, the competent authority may choose to develop national guides or other types of documents to help the persons under its oversight in complying with the Regulation. The competent authority may inform the Agency, so that such guides or other documents may later be considered for transposition into an AMC published by the Agency through the Agency rulemaking process.

text: AMC1 66.B.115 Procedure for the change of an aircraft maintenance licence to include an aircraft rating or to remove limitations

text: […] (c) For the acceptance of the OJT programme described in Section 6 of Appendix III to Part-66, the licensing competent authority should develop adequate procedures which may be similar to the procedure described in AMC 66.B.130 for the ‘direct approval of aircraft type training’. For the acceptance of the OJT tasks and programme, the licensing competent authority should develop procedures compliant with Section 6 of Appendix III to Part-66. […]

text: GM1 66.B.400(d) General

text: In the case of a person applying for the issue or change of an AML, by use of examination credits, to a competent authority of a Member State (hereafter referred to as licensing authority) other than the competent authority that has granted the examination credits (hereafter referred to as competent authority), the licensing authority is expected to contact the competent authority and request the examination credit assessment or the credit report or any other information and documentation it considers necessary in order to ascertain the equivalence of the syllabus of the technical qualification obtained by the applicant to the syllabus of the basic knowledge modules. The competent authority is expected to provide the licensing authority with all the requested information regarding its examination crediting system and the applicant concerned. Should the licensing authority observe any inconsistency in the provided documentation or have doubts regarding the equivalence of the technical qualification of the applicant to the syllabus of the basic knowledge modules, it is expected to address the competent authority and arrive at a mutual understanding. The licensing authority is also expected to assess the application against its own credit report and equivalence criteria in order to ensure a standardised approach to the process of examination crediting, and fair treatment to all its applicants. Unless proven that the examination credits granted by the competent authority were not in compliance with the provisions of the Regulation, or that a positive assessment of the applicant’s documentation would hinder its own examination crediting system, the licensing authority is expected to consider the applicant’s documentation as compliant. The final decision regarding the consideration of the provided documents as valid supporting documentation in respect of point 66.B.100 or 66.B.110 rests with the licensing authority. […]

text: Appendix I — Basic Knowledge Requirements (except for category L licence)

text: AMC1 Appendix I — Basic Knowledge Requirements (except for category L licence) Section 2

text: MODULARISATION MODULE 1 — MATHEMATICS

text: LEVEL

text: A1 B1 MODULE 1 — MATHEMATICS A2 B2 A3 B2L A4 B3

text: 1.1 Arithmetic 1 2 Arithmetical terms and signs, methods of multiplication and division, fractions and decimals, factors and multiples, weights, measures and conversion factors, ratio and proportion, averages and percentages, areas and volumes, squares, cubes, square and cube roots. 1.2 Algebra (a) Evaluating simple algebraic expressions, addition, subtraction, multiplication and 1 2 division, use of brackets, simple algebraic fractions; (b) Linear equations and their solutions; — 1 Indices and powers, negative and fractional indices;

text: LEVEL A1 B1 MODULE 1 — MATHEMATICS A2 B2 A3 B2L A4 B3

text: Binary and other applicable numbering systems; Simultaneous equations and second-degree equations with one unknown; Logarithms. 1.3 Geometry (a) Simple geometrical constructions; — 1 (b) Graphical representation: nature and uses of graphs, graphs of 2 2 equations/functions; (c) Simple trigonometry: trigonometrical relationships, use of tables and rectangular — 2 and polar coordinates.

text: MODULE 2 — PHYSICS

text: LEVEL

text: A1 B1 A2 B2 MODULE 2 — PHYSICS A3 B2L A4 B3

text: 2.1 Matter 1 2 Nature of matter: the chemical elements, structure of atoms, molecules; Chemical compounds; States: solid, liquid, and gaseous; Changes between states. 2.2 Mechanics 2.2.1 Statics 1 2 Forces, moments and couples, representation as vectors; Centre of gravity; Elements of theory of stress, strain, and elasticity: tension, compression, shear, and torsion; Nature and properties of solid, fluid, and gas matter; Pressure and buoyancy in liquids (barometers). 2.2.2 Kinetics 1 2 Linear movement: uniform motion in a straight line, motion under constant acceleration (motion under gravity); Rotational movement: uniform circular motion (centrifugal/centripetal forces); Periodic motion: pendular movement; Simple theory of vibration, harmonics, and resonance; Velocity ratio, mechanical advantage, and efficiency. 2.2.3 Dynamics (a) Mass; 1 2 Force, inertia, work, power, energy (potential, kinetic and total energy), heat, efficiency;

text: LEVEL A1 B1 A2 B2 MODULE 2 — PHYSICS A3 B2L A4 B3

text: (b) Momentum, conservation of momentum; 1 2 Impulse; Gyroscopic principles; Friction: nature and effects, coefficient of friction (rolling resistance). 2.2.4 Fluid dynamics (a) Specific gravity and density; 2 2 (b) Viscosity, fluid resistance, effects of streamlining; 1 2 Effects of compressibility on fluids; Static, dynamic, and total pressure: Bernoulli’s Theorem, venturi. 2.3 Thermodynamics (a) Temperature: thermometers and temperature scales (Celsius, Fahrenheit and 2 2 Kelvin); definition of heat; (b) Heat capacity, specific heat; 1 2 Heat transfer: convection, radiation and conduction; Volumetric expansion; First and second law of thermodynamics; Gases: ideal gases laws; specific heat at constant volume and constant pressure, work done by expanding gas; Isothermal, adiabatic expansion and compression, engine cycles, constant volume and constant pressure, refrigerators and heat pumps; Latent heats of fusion and evaporation, thermal energy, heat of combustion. 2.4 Optics (Light) – 2 Nature of light; speed of light; Laws of reflection and refraction: reflection at plane surfaces, reflection by spherical mirrors, refraction, lenses; Fibre optics. 2.5 Wave motion and sound – 2 Wave motion: mechanical waves, sinusoidal wave motion, interference phenomena, standing waves; Sound: speed of sound, production of sound, intensity, pitch and quality, Doppler effect.

text: MODULE 3 — ELECTRICS FUNDAMENTALS

text: LEVEL

text: MODULE 3 — ELECTRICS FUNDAMENTALS A2

text: 3.1 Electron theory 1 1 1 Structure and distribution of electrical charges within atoms, molecules, ions, and compounds; Molecular structure of conductors, semiconductors, and insulators. 3.2 Static electricity and conduction 1 2 1 Static electricity and distribution of electrostatic charges; Electrostatic laws of attraction and repulsion; Units of charge, Coulomb’s law; Conduction of electricity in solids, liquids, gases and in vacuum. 3.3 Electrical terminology 1 2 1 The following terms, their units and factors affecting them: potential difference, electromotive force, voltage, current, resistance, conductance, charge, conventional current flow, electron flow. 3.4 Generation of electricity 1 1 1 Production of electricity by the following methods: light, heat, friction, pressure, chemical reaction, magnetism, and motion. 3.5 Sources of DC electricity 1 2 2 Construction and basic chemical reaction of primary cells, secondary cells, lead acid cells, nickel cadmium cells, lithium cells, nickel cells and other alkaline cells; Cells connected in series and in parallel; Internal resistance and its effect on a battery; Construction, materials, and operation of thermocouples; Operation of photocells. 3.6 DC circuits 1 2 1 Ohm’s law, Kirchhoff’s voltage, and current laws; Calculations using the above laws to find resistance, voltage, and current; Significance of the internal resistance of a supply. 3.7 Resistance/Resistor (a) Resistance — 2 1 Specific resistance; Calculation of total resistance using series, parallel and series–parallel combinations; Operation and use of potentiometers and rheostats; Operation of Wheatstone Bridge.

text: LEVEL

text: MODULE 3 — ELECTRICS FUNDAMENTALS A2

text: (b) Resistor — 1 — Positive and negative temperature coefficient conductance; Resistor colour code, values and tolerances, preferred values, wattage ratings; Resistors in series and in parallel; Fixed resistors, stability, tolerance and limitations, methods of construction; Variable resistors, thermistors, voltage-dependent resistors; Construction of potentiometers and rheostats; Construction of Wheatstone Bridge. 3.8 Power — 2 1 Power, work, and energy (kinetic and potential); Dissipation of power by a resistor; Power formula; Calculations involving power, work, and energy. 3.9 Capacitance/Capacitor — 2 1 Operation and function of a capacitor; Factors that affect the capacitance area of plates, distance between plates, number of plates, dielectric and dielectric constant, working voltage, voltage rating; Capacitor types, construction, and function; Capacitor colour-coding; Calculations of capacitance and voltage in series and in parallel circuits; Exponential charge and discharge of a capacitor, time constants; Testing of capacitors. 3.10 Magnetism (a) Theory of magnetism; — 2 1 Properties of a magnet; Action of a magnet suspended in the Earth’s magnetic field; Magnetisation and demagnetisation; Magnetic shielding; Various types of magnetic material; Electromagnet construction and principles of operation; Handclasp rules to determine magnetic field around current-carrying conductor. (b) Magnetomotive force, field strength, magnetic flux density, permeability, — 2 1 hysteresis loop, retentivity, coercive force reluctance, saturation point, eddy currents; Precautions for care and storage of magnets. 3.11 Inductance/Inductor — 2 1

text: LEVEL

text: MODULE 3 — ELECTRICS FUNDAMENTALS A2

text: Faraday’s law; Action of inducing a voltage in a conductor that moves in a magnetic field; Induction principles; Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of change of flux, number of conductor turns; Mutual induction; The effect that the rates of change of primary current and mutual inductance have on induced voltage; Factors that affect mutual inductance: number of turns in the coil, physical size of the coil, permeability of the coil, position of coils with respect to each other; Lenz’s law and polarity determining rules; Back EMF, self-induction; Saturation point; Principal uses of inductors. 3.12 DC motor/generator theory – 2 1 Basic motor and generator theory; Construction and purpose of components in a DC generator; Operation of and factors that affect the output and direction of the current in DC generators; Operation of and factors that affect the output power, torque, speed, and direction of rotation of DC motors; Series-wound, shunt-wound and compound motors; Starter generator construction. 3.13 AC theory 1 2 1 Sinusoidal waveform: phase, period, frequency, cycle; Instantaneous, average, root mean square, peak, peak-to-peak current values and calculations of these values in relation to voltage, current and power; Triangular/Square waves; Single-phase/Three-phase principles. 3.14 Resistive (R), capacitive (C) and inductive (L) circuits — 2 1 Phase the relationship of voltage and current in L, C and R circuits, parallel, series and series–parallel; Power dissipation in L, C and R circuits; Impedance, phase angle, power factor and current calculations; True power, apparent power, and reactive power calculations. 3.15 Transformers — 2 1

text: LEVEL

text: MODULE 3 — ELECTRICS FUNDAMENTALS A2

text: Transformer construction principles and operation; Transformer losses and methods for overcoming them; Transformer action under load and no-load conditions; Power transfer, efficiency, polarity markings; Line and phase voltages and currents; Power in a three-phase system; Primary and secondary current, voltage, turn ratio, power, efficiency; Auto-transformers. 3.16 Filters — 1 — Operation, application, and uses of the following filters: low pass, high pass, band pass, band stop. 3.17 AC generators — 2 1 Rotation of loop in a magnetic field and waveform produced; Operation and construction of revolving armature and revolving field type AC generators; Single-phase, two-phase, and three-phase alternators; Three-phase star and delta connection advantages, and uses; Permanent magnet generators. 3.18 AC motors — 2 1 Construction, principles of operation and characteristics of: AC synchronous and induction motors both single-phase and polyphase; Methods of speed control and direction of rotation; Methods of producing a rotating field: capacitor, shaded or split pole.

text: MODULE 4 — ELECTRONICS FUNDAMENTALS

text: LEVEL

text: MODULE 4 — ELECTRONICS FUNDAMENTALS A2 B1 B2

text: 4.1 Semiconductors 4.1.1 Diodes (a) Description and characteristics — 2 2 Diode symbols; Diode characteristics and properties; Diodes in series and in parallel; Materials, electron configuration, electrical properties;

text: LEVEL

text: P and N type materials: effects of impurities on conduction, majority and minority characters; P–N junction in a semiconductor, development of a potential across a P–N junction in unbiased, forward-biased and reverse-biased conditions; Diode parameters: peak inverse voltage, maximum forward current, temperature, frequency, leakage current, power dissipation; Main characteristics and use of silicon-controlled rectifiers (thyristors), lightemitting diodes (LEDs), photo-conductive diodes, rectifier diodes.

text: (b) Operation and function — — 2 Operation and function of diodes in the following circuits: clippers, clampers, full- and half-wave rectifiers, bridge rectifiers, voltage doublers and triplers; Detailed operation and characteristics of the following devices: siliconcontrolled rectifier (thyristor), light-emitting diode (LED), Schottky diode, photo-conductive diode, varactor diode, varistor, rectifier diodes, Zener diode. Functional testing of diodes. 4.1.2 Transistors (a) Description and characteristics — 1 2 Transistor symbols; Component description and orientation; Transistor characteristics and properties. (b) Construction and operation — — 2 Construction and operation of PNP and NPN transistors; Base, collector and emitter configurations; Testing of transistors; Basic appreciation of other transistor types, including types of FET and their uses; Application of transistors: amplifier classes (A, B, C); Simple circuits including bias, decoupling, feedback and stabilisation; Multistage circuit principles: cascades, push–pull, oscillators, multivibrators, flip-flop circuits; Operation and amplifier stages connecting methods: resistive, capacitive, direct, inverting, non-inverting and adding. 4.1.3 Integrated circuits (a) Description and operation of logic circuits and linear circuits/operational — 1 2 amplifiers; (b) Introduction to the operation and function of an operational amplifier used — — 2 as: an integrator, a differentiator, a voltage follower, a comparator; Advantages and disadvantages of positive and negative feedback.

text: LEVEL

text: 4.2 Printed circuit boards — 1 2 Description and use of printed circuit boards. 4.3 Servomechanisms (a) Principles — 1 2 Understanding of the following principles: open- and closed-loop systems, servomechanism, feedback, follow-up, null, overshoot, damping, deadband, hunting, proximity switches, analogue transducers, synchro systems and components, digital tachometers and encoders, inductance, and capacitance transmitters; (b) Construction operation and use of the following synchro-system components: — — 2 resolvers, differential, control and torque, E and I transformers, inductance transmitters, capacitance transmitters, synchronous transmitters; Construction, operation and use of servomechanism and PID controller; Fault-finding of servo defects, reversal of synchro leads, hunting.

text: MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS

text: LEVEL

text: A1 MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS A2 B2 B3 B1 A3 B2L A4

text: 5.1 Electronic instrument systems 1 1 1 1 Typical arrangements of systems and cockpit layout of electronic instrument systems. 5.2 Numbering systems — — 1 2 Numbering systems: binary, octal, and hexadecimal; Demonstration of conversions between the decimal and binary systems, octal and hexadecimal systems and vice versa. 5.3 Data conversion — — 1 2 Analogue data, Digital data; Operation and application of analogue-to-digital and digital-to-analogue converters, inputs and outputs, limitations of various types. 5.4 Data buses — — 2 2 Operation of data buses in aircraft systems, including knowledge of ARINC and other specifications. Aircraft network/Ethernet.

text: LEVEL

text: 5.5 Logic circuits (a) Identification of common logic gate symbols, tables and equivalent — — 2 2 circuits; Applications used for aircraft systems, schematic diagrams. (b) Interpretation of logic diagrams. — — — 2 5.6 Basic computer structure (a) Computer terminology (including bit, byte, software, hardware, CPU, 1 1 2 2 IC, and various memory devices such as RAM, ROM, PROM); Computer technology (as applied in aircraft systems). (b) Computer operation, layout, and interface of the major components in — — — 2 a microcomputer, including their associated bus systems; Information contained in single- and multi-address instruction words; Memory-associated terms; Operation of typical memory devices; Operation, advantages, and disadvantages of the various data storage systems. 5.7 Microprocessors — — — 2 Functions performed and overall operation of a microprocessor; Basic operation of each of the following microprocessor elements: control and processing unit, clock, register, arithmetic logic unit. 5.8 Integrated circuits — — — 2 Operation and use of encoders and decoders; Function of encoder types. 5.9 Multiplexing — — — 2 Operation, application and identification in logic diagrams of multiplexers and demultiplexers. 5.10 Fibre optics — — 1 2 Advantages and disadvantages of fibre optic data transmission over electrical wire propagation; Fibre optic data bus; Fibre-optic-related terms; Terminations; Couplers, control terminals, remote terminals; Application of fibre optics in aircraft systems. 5.11 Electronic displays 1 1 2 2 Principles of operation of common types of displays used in modern aircraft, including cathode-ray tubes (CRTs), light-emitting diodes (LEDs) and liquid crystal displays (LCDs).

text: LEVEL

text: 5.12 Electrostatic-sensitive devices 1 1 2 2 Special handling of components sensitive to electrostatic discharges; Awareness of risks and possible damage, component, and personnel antistatic protection devices. 5.13 Software management control — 1 2 2 Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programs. 5.14 Electromagnetic environment — 1 2 2 Influence of the following phenomena on maintenance practices for electronic systems: EMC — Electromagnetic Compatibility, EMI — Electromagnetic Interference, HIRF — High-Intensity Radiated Field, Lightning / lightning protection. 5.15 Typical electronic/digital aircraft systems 1 1 1 1 General arrangement of typical electronic/digital aircraft systems and associated BITE (Built-In Test Equipment), such as: (a) ACARS — ARINC Communication and Addressing and Reporting System, FBW — Fly-by-Wire, FMS — flight management system, IRS — inertial reference system; (b) ECAM — electronic centralised aircraft monitoring, EICAS — engine indication and crew alerting system, EFIS — electronic flight instrument system, GNSS — global navigation satellite system, TCAS — traffic alert collision avoidance system, Integrated Modular Avionics, Cabin Systems, Information Systems.

text: MODULE 6 — MATERIALS AND HARDWARE

text: LEVEL

text: A1 MODULE 6 — MATERIALS AND HARDWARE A2 B1 B2 A3 B3 B2L A4

text: 6.1 Aircraft materials — ferrous (a) Characteristics, properties and identification of common alloy steels used in 1 2 1 aircraft; Heat treatment and application of alloy steels. (b) Testing of ferrous materials for hardness, tensile strength, fatigue strength and — 1 1 impact resistance. (c) Repair and inspection procedures for ferrous materials, structures, and — 2 1 airframes. 6.2 Aircraft materials — non-ferrous (a) Characteristics, properties and identification of common non-ferrous 1 2 1 materials used in aircraft; Heat treatment and application of non-ferrous materials. (b) Testing of non-ferrous material for hardness, tensile strength, fatigue strength — 1 1 and impact resistance. (c) Repair and inspection procedures for non-ferrous materials, structures, and — 2 1 airframes. 6.3 Aircraft materials — composite and non-metallic 6.3.1 Composite and non-metallic materials other than wood and fabric (a) Characteristics, properties and identification of common composite and 1 2 2 non-metallic materials, other than wood, used in aircraft; Sealant and bonding agents. (b) Detection of defects/deterioration in composite and non-metallic 1 2 — materials. (c) Repair of and inspection procedures for composite and non-metallic — 2 1 materials, structures, and airframes. 6.3.2 Wooden structures 1 1 — Construction methods of wooden airframe structures; Characteristics, properties and types of wood and glue used in aeroplanes; Preservation and maintenance of wooden structures; Types of defects in wood material and wooden structures; Detection of defects in wooden structures; Repair of wooden structures. 6.3.3 Fabric covering — 1 — Characteristics, properties and types of fabrics used in aeroplanes; Inspection methods for fabrics; Types of defects in fabrics; Repair of fabric covering.

text: LEVEL

text: 6.4 Corrosion (a) Chemical fundamentals; 1 1 1 Formation by galvanic action process, microbiological contamination, mechanical stress. (b) Types of corrosion and their identification; 2 3 2 Causes of corrosion; Material types, and their susceptibility to corrosion. 6.5 Fasteners 6.5.1 Screw threads 2 2 2 Screw nomenclature; Thread forms, dimensions and tolerances for standard threads used in aircraft; Measuring screw threads. 6.5.2 Bolts, studs, and screws 2 2 2 Bolt types: specification, identification and marking of aircraft bolts, international standards; Nuts: self-locking, anchor, standard types; Machine screws: aircraft specifications; Studs: types and uses, insertion, and removal; Self-tapping screws, dowels. 6.5.3 Locking devices 2 2 2 Tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quickrelease fasteners, keys, circlips, cotter pins. 6.5.4 Aircraft rivets 1 2 1 Types of solid and blind rivets: specifications and identification, heat treatment. 6.6 Pipes and unions (a) Identification and types of rigid and flexible pipes and their connectors used in 2 2 2 aircraft; (b) Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system 2 2 1 pipes. 6.7 Springs — 2 1 Types of springs, materials, characteristics, and applications. 6.8 Bearings 1 2 2 Purpose of bearings, loads, material, construction; Types of bearings and their application. 6.9 Transmissions 1 2 2

text: LEVEL

text: Gear types and their application; Gear ratios, reduction and multiplication gear systems, driven and driving gears, idler gears, mesh patterns; Belts and pulleys, chains and sprockets. 6.10 Control cables 1 2 1 Types of cables; End fittings, turnbuckles and compensation devices; Pulleys and cable system components; Bowden cables; Aircraft flexible control systems. 6.11 Electrical cables and connectors 1 2 2 Cable types, construction and characteristics; High-tension and coaxial cables; Crimping; Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes.

text: MODULE 7 — MAINTENANCE PRACTICES

text: LEVEL

text: A1 MODULE 7 — MAINTENANCE PRACTICES A2 B1 B2 A3 B3 B2L A4

text: 7.1 Safety precautions — aircraft and workshop 3 3 3 Aspects of safe working practices including precautions to be taken when working with electricity, gases (especially oxygen), oils, and chemicals. Fuel tank safety and fuel tank entry procedures and precautions. Awareness and precautions regarding aircraft equipped with ballistic recovery systems. Also, instructions for the remedial action to be taken in the event of a fire or another accident with one or more of these hazards, including information on fireextinguishing agents. 7.2 Workshop practices 3 3 3 Care of tools, control of tools, use of workshop materials; Dimensions, allowances and tolerances, workmanship standards; Calibration of tools and equipment, calibration standards. 7.3 Tools 3 3 3 Common hand-tool types; Common power-tool types; Operation and use of precision-measuring tools; Lubrication equipment and methods; Operation, function, and use of electrical general test equipment. 7.4 (Reserved)

text: 7.5 Engineering drawings, diagrams, and standards 1 2 2 Drawing types and diagrams, their symbols, dimensions, tolerances and projections; Identification of title block information; Microfilm, microfiche, and computerised presentations; Specification 100 of the Air Transport Association (ATA) of America; Aeronautical and other applicable standards including ISO, AN, MS, NAS and MIL; Wiring diagrams and schematic diagrams. 7.6 Fits and clearances 1 2 1 Drill sizes for bolt holes, classes of fits; Common system for fits and clearances; Schedule of fits and clearances for aircraft and engines; Limits for bow, twist and wear; Standard methods for checking shafts, bearings, and other parts. 7.7 Electrical wiring interconnection system (EWIS) 1 3 3 Continuity, insulation and bonding techniques and testing; Use of crimp tools: hand and hydraulic operated;

text: LEVEL

text: Testing of crimp joints; Connector pin removal and insertion; Coaxial cables: testing and installation precautions; Identification of wire types, their inspection criteria and damage tolerance; Wiring protection techniques: cable looming and loom support, cable clamps, protective sleeving techniques including heat shrink wrapping, shielding; High-Intensity Radiated Fields (HIRF) and protection principles; Soldering of electrical wires, EWIS installations, inspection, repair, maintenance, and cleanliness standards. 7.8 Riveting 1 2 – Riveted joints, rivet spacing and pitch; Tools used for riveting and dimpling; Inspection of riveted joints. 7.9 Pipes and hoses 1 2 – Bending and belling/flaring aircraft pipes; Inspection and testing of aircraft pipes and hoses; Installation and clamping of pipes. 7.10 Springs 1 2 – Inspection and testing of springs. 7.11 Bearings 1 2 – Testing, cleaning and inspection of bearings; Lubrication requirements for bearings; Defects in bearings and their causes. 7.12 Transmissions 1 2 – Inspection of gears, backlash; Inspection of belts and pulleys, chains and sprockets; Inspection of screw jacks, lever devices, push–pull rod systems. 7.13 Control cables 1 2 – Swaging of end fittings; Inspection and testing of control cables; Bowden cables; aircraft flexible control systems. 7.14 Material handling 7.14.1 Sheet metal – 2 – Marking out and calculation of bend allowance; Sheet metal working, including bending and forming; Inspection of sheet metal work. 7.14.2 Composite and non-metallic – 2 –

text: LEVEL

text: Bonding practices; Environmental conditions; Inspection methods. 7.14.3 Additive manufacturing 1 1 1 Common additive manufacturing techniques and their influence on the mechanical properties of the finished part; Inspection of additive manufactured parts and common production failures. 7.15 (Reserved) 7.16 Aircraft weight and balance (a) Calculation of centre-of-gravity / balance limits: use of relevant documents. – 2 2 (b) Preparation of aircraft for weighing; – 2 – Aircraft weighing. 7.17 Aircraft handling and storage 2 2 2 Aircraft taxiing/towing and associated safety precautions; Aircraft jacking, chocking, securing and associated safety precautions; Aircraft storage methods; Refuelling/defuelling procedures; De-icing/anti-icing procedures; Electrical, hydraulic, and pneumatic ground supplies; Effects of environmental conditions on aircraft handling and operation. 7.18 Disassembly, inspection, repair, and assembly techniques (a) Types of defects and visual inspection techniques; 2 3 3 Corrosion removal, assessment and reprotection; (b) General repair methods, structural repair manual; – 2 – Ageing, fatigue, and corrosion control programmes; (c) Non-destructive inspection techniques including penetrant, radiographic, – 2 1 eddy current, magnetic particle, ultrasonic and borescope inspections; including practical training in colour contrast penetrant inspection; (d) Disassembly and reassembly techniques; 2 2 2 (e) Troubleshooting techniques. – 2 2 7.19 Abnormal events (a) Inspections following lightning strikes and HIRF penetration; 2 2 2 (b) Inspections following abnormal events such as heavy landings and flight 2 2 – through turbulence. 7.20 Maintenance procedures 1 2 2

text: LEVEL

text: Maintenance planning; Modification procedures; Stores procedures; Certification/release procedures; Interface with aircraft operation; Maintenance Inspection / Quality Control / Quality Assurance; Additional maintenance procedures; Control of life-limited components. 7.21 Documentation and communication 1 2 2 Documentation: elements and criteria for writing work reports, troubleshooting reports, and shift handover instructions. Communication: clear, comprehensive, and concise.

text: MODULE 8 — BASIC AERODYNAMICS

text: LEVEL

text: A1 A2 B1 MODULE 8 — BASIC AERODYNAMICS A3 B2 A4 B2L B3

text: 8.1 Physics of the atmosphere 1 2 International Standard Atmosphere (ISA), and its application to aerodynamics. 8.2 Aerodynamics 1 2 Airflow around a body; Boundary layer, laminar and turbulent flow, free stream flow, relative airflow, upwash and downwash, vortices, stagnation; The terms: camber, chord, mean aerodynamic chord, profile (parasite) drag, induced drag, centre of pressure, angle of attack, wash-in and wash-out, fineness ratio, wing shape and aspect ratio; Thrust, weight, aerodynamic resultant; Generation of lift and drag angle of attack, lift coefficient, drag coefficient, polar curve, stall; Aerofoil contamination including ice, snow, and frost. 8.3 Theory of flight 1 2

text: LEVEL

text: Relationship between lift, weight, thrust and drag; Glide ratio; Steady-state flights, performance; Theory of the turn; Influence of load factor: stall, flight envelope, and structural limitations; Lift augmentation. 8.4 High-speed airflow 1 2 Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number, compressibility buffet, shock wave, aerodynamic heating, area rule; Factors that affect airflow in engine intakes of high-speed aircraft; Effects of sweepback on critical Mach number. 8.5 Flight stability and dynamics 1 2 Longitudinal, lateral, and directional stability (active and passive).

text: MODULE 9 — HUMAN FACTORS

text: LEVEL

text: MODULE 9 — HUMAN FACTORS ALL

text: 9.1 General 2 The need to take human factors into account when performing maintenance; Incidents attributable to human factors/human error; Murphy’s law. 9.2 Human performance and limitations 2 Vision; Hearing; Information processing; Attention and perception; Memory; Claustrophobia and physical access. 9.3 Social psychology 1 Accountability and responsibility: individual and group; Motivation and demotivation; Peer pressure; Cultural issues; Teamwork; Management, supervision, and leadership. 9.4 Factors that affect performance 2

text: LEVEL

text: MODULE 9 — HUMAN FACTORS ALL

text: Fitness/health; Stress: domestic and work related; Time pressure and deadlines; Workload: overload, underload, and workload management; Sleep and fatigue, shift work; Alcohol, medication, drug abuse; Lack of manpower. 9.5 Physical environment 1 Noise and fumes; Illumination; Climate and temperature; Motion and vibration; Working environment; Situational awareness. 9.6 Tasks 1 Physical work; Repetitive tasks, complacency; Visual inspection; Complex systems; Critical maintenance tasks and error-capturing methods; Technical documentation: access, use, and quality. 9.7 Communication 2 Within and between teams; Work logging and recording; Shift handover; Keeping up to date, currency; Dissemination of information. 9.8 Human error 2 Error models and theories; Types of error in maintenance tasks; Implications of errors (e.g. accidents); Organisational errors; Avoiding and managing errors. 9.9 Safety management 2 Risk management; Occurrence reporting; Safety culture Just culture; Identifying, avoiding, and reporting hazards; Organisational human-factors programme: professionalism and integrity, error-provoking behaviour, reporting errors, disciplinary policy, error investigation, action to address problems, feedback, assertiveness; Dealing with emergencies. 9.10 The ‘Dirty Dozen’ and risk-mitigation 2 The ‘Dirty Dozen’: the twelve most common human-factors errors in maintenance:

text: LEVEL

text: MODULE 9 — HUMAN FACTORS ALL

text: Lack of communication, Lack of teamwork, Lack of assertiveness, Complacency, Fatigue, Stress, Lack of knowledge, Lack of resources, Lack of awareness, Distraction, Pressure, Norms. Risk-mitigation methods.

text: MODULE 10 — AVIATION LEGISLATION

text: LEVEL

text: A1 B1 MODULE 10 — AVIATION LEGISLATION A2 B2 A3 B2L A4 B3

text: 10.1 Regulatory framework 1 1 Role of: — the International Civil Aviation Organization (ICAO); — the European Commission (EC); — the European Union Aviation Safety Agency (EASA); — the European Union Member States and national aviation authorities; — the bilateral agreements concluded by the European Commission; —

text: Regulation (EU) 2018/1139

text: (the Basic Regulation) and its implementing acts: Regulations

text: (EU) No 748/2012

text: (Initial Airworthiness) and

text: (EU) No 1321/2014

text: (Continuing Airworthiness); — the relationship between regulations (hard law) and AMC, GM and CSs (soft law); — occurrence reporting according to

text: Regulation (EU) No 376/2014

text: ; — the relationship between the various annexes (parts) relating to Initial and Continuing Airworthiness (such as Part 21, Part-M, Part-145, Part-66, Part-147, Part-T, Part-ML, Part-CAMO, and Part-CAO) and Regulations

text: (EU) No 965/2012

text: (the Air Operations Regulation) and

text: (EU) No 1178/2011

text: (the Air Crew Regulation). 10.2 Certifying staff — maintenance 2 2 Deep understanding of Part-66 maintenance licences with the associated privileges and authorisations, and how to exercise them properly for the different aircraft categories. 10.3 Approved maintenance organisations 2 2 General understanding of Part-145 and Part-CAO. 10.4 Independent certifying staff — 3

text: LEVEL

text: Privileges, responsibilities, record-keeping, limitations, and oversight according to Part-M, Part-66 and Part-ML. 10.5 Air operations 1 1 General understanding of

text: Regulation (EU) No 965/2012

text: (the Air Operations Regulation); Differences between commercial and non-commercial air operations, and their influence on aircraft maintenance; Air Operator Certificates (AOCs) and self-declaration authorisations; Air operator responsibilities, in particular regarding continuing airworthiness and maintenance; Specialised operations / specific approvals: ETOPS, CAT I/II/III, and BRNAV. Minimum Equipment List (MEL) and Configuration Deviation List (CDL); Aircraft placarding and markings; Documents to be carried on board: — Certificate of Airworthiness / Restricted Certificate of Airworthiness; — Airworthiness Review Certificate; — Permit to Fly; — Certificate of Registration; — Noise Certificate; — Weight and Balance report; — Radio Station Licence. 10.6 Certification of aircraft, parts, and appliances 2 2 Basic understanding of Part 21 and of the following EASA certification specifications: CS-22, CS-23, CS-25, CS-27, CS-29, and CS-STAN. 10.7 Continuing airworthiness 2 2 General understanding of the Part 21 requirements on continuing airworthiness; General understanding of Part-M, Part-ML and Part-CAMO; Aircraft Maintenance Programme. 10.8 Oversight principles in continuing airworthiness 1 1 10.9 Maintenance and certification beyond current EU regulations (if not superseded by EU – 1

text: requirements)

text: Maintenance of European Union aircraft that are not within the scope of

text: Regulation (EU) 2018/1139

text: (Annex I aircraft); European military airworthiness requirement (EMAR) 66 licence; Applicable national and international requirements for component maintenance, welding, painting, NDT, etc. (if not superseded by EU requirements). 10.10 Cybersecurity in aviation maintenance 1 1 Regulation on the introduction of organisation requirements for the management of information security risks related to aeronautical information systems used in civil aviation.

text: MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

text: MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES AND LEVEL

text: 11.1 Theory of flight (a) Aeroplane aerodynamics and flight controls 1 1 2 2 1 Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; — yaw control, rudder limiters; — elevons, ruddervators; — high-lift devices, slots, slats, flaps, flaperons; — drag-inducing devices, spoilers, lift dumpers, speed brakes; — trim tabs, servo tabs, control surface bias. (b) Aeroplane: other aerodynamic devices 1 1 2 2 1 Operation and effect of: — balance and antibalance (leading) tabs; — spring tabs, mass balance, aerodynamic balance panels; — mass balance, aerodynamic balance panels; — effects of wing fences, saw tooth leading edges; — boundary layer control using vortex generators, stall wedges or leading-edge devices. 11.2 Airframe structures (ATA 51) (a) General concepts: 2 2 2 2 2 — Zonal and station identification systems; — Electrical bonding; — Lightning strike protection provisions. (b) Airworthiness requirements for structural strength: 2 2 2 2 2 — Structural classification: primary, secondary, and tertiary; — Fail-safe, safe-life, damage-tolerance concepts; — Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue; — Drains and ventilation provisions; — System installation provisions. (c) Construction methods 1 1 2 2 2 — Stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, skinning, anticorrosive protection, wing, empennage and engine attachments; — Structure assembly techniques: riveting, bolting, bonding;

text: — Methods of surface protection, such as chromating, anodising, painting; — Surface cleaning; — Airframe symmetry: methods of alignment and symmetry checks. 11.3 Airframe structures — aeroplanes 11.3.1 Fuselage, doors, windows (ATA 52/53/56) 1 1 2 2 1 (a) Construction principles — Construction and pressurisation sealing; — Wing, stabiliser, pylon, and undercarriage attachments; — Seat installation and cargo loading system; — Doors and emergency exits: construction, mechanisms, operation and safety devices; — Windows and windscreen construction and mechanisms. (b) Airborne towing devices (glider, banner, target). 1 1 1 1 1 (c) Doors 1 1 2 1 — — Doors and emergency exits: safety devices; — Cargo loading system. 11.3.2 Wings (ATA 57) 1 1 2 2 1 Construction; Fuel storage; Landing gear, pylon, control surface and high lift/drag attachments. 11.3.3 Stabilisers (ATA 55) 1 1 2 2 1 Construction; Control surface attachment. 11.3.4 Flight control surfaces (ATA 55/57) 1 1 2 2 1 Construction and attachments; Balancing — mass and aerodynamics. 11.3.5 Nacelles/pylons (ATA 54) 1 1 2 2 1 Nacelles/Pylons: — Construction, — Firewalls, — Engine mounts. 11.4 Air conditioning and cabin pressurisation (ATA 21) (a) Pressurisation 1 1 3 3 — Pressurisation systems; Cabin pressure controllers, control, and safety valves; Control and indication. (b) Air supply 1 - 3 - —

text: Sources of air supply including engine bleed, APU and ground cart; Distribution systems. (c) Air conditioning 1 — 3 - — Air-conditioning systems; Air cycle and vapour cycle machines; Flow, temperature and humidity control system; Control and indication control valves. (d) Safety and warning devices 1 1 3 3 — Protection and warning devices. (e) Heating and ventilation systems. — 1 - 3 1 11.5 Instruments / avionics systems 11.5.1 Instrument systems (ATA 31) 1 1 2 2 2 Pitot-static: Airspeed indicators, Vertical speed indicators, Altimeters; Gyroscopic: Gyroscopic principles, Artificial horizons, Attitude directors, Direction indicators, Horizontal situation indicators (HSI), Slip indicators, Turn indicators, Turn coordinators; Compass systems: systems, direct reading, remote reading, Stall-warning systems and angle-of-attack indicating systems, Glass cockpit, Indications of other aircraft systems. 11.5.2 Avionics systems 1 1 1 1 1 Fundamentals of system layouts and operation of: Autoflight (ATA 22); Communication systems (ATA 23): — Very High Frequency (VHF) communications, — High Frequency (HF) communications, — Satellite Communications (SATCOM), — Controller–pilot data link communications (CPDLC), — Audio systems, — Emergency Locator Transmitters (ELTs), — Cockpit Voice Recorder (CVR); Navigation systems (ATA 34): — Very high frequency omnidirectional range (VOR), — Automatic direction finder (ADF),

text: — Instrument landing system (ILS), — Microwave landing system (MLS), — Flight director systems (FDSs), distance-measuring equipment (DME), — Area navigation (RNAV) systems, — Flight management systems (FMSs), — Satellite navigation systems, — Air traffic control transponder, secondary surveillance radar, — Traffic alert and collision avoidance system (TCAS), — Weather avoidance radar, — Radio altimeter, — Inertial navigation system (INS), — ARINC (Aeronautical Radio Incorporated) communication and reporting. Types and uses of avionics general test equipment. 11.6 Electrical power (ATA 24) 1 1 3 3 3 — Installation and operation of batteries; — DC power generation; — AC power generation; — Emergency power generation; — Voltage regulation; — Power distribution; — Inverters, transformers, rectifiers; — Circuit protection; — External/ground power. 11.7 Equipment and furnishings (ATA 25) (a) Emergency equipment: 2 2 2 2 2 Emergency equipment requirements. (b) Cabin and cargo layout: 1 1 1 1 — — Seats, harnesses, and belts; — Cabin layout; — Equipment layout; — Cabin furnishing installation; — Galley installation; — Cargo handling and retention equipment; — Airstairs. 11.8 Fire protection (ATA 26) (a) Fire and smoke detection system, and fire-extinguishing systems: 1 1 1 1 — — Fire and smoke detection and warning systems; — Fire-extinguishing systems;

text: — System tests. (b) Portable fire extinguisher. 1 1 1 1 1 11.9 Flight controls (ATA 27) (a) Primary and secondary flight controls: 1 1 3 3 2 — Primary controls: aileron, elevator, rudder, spoiler; — Trim control, trim tabs; — High-lift devices; — System operation: manual; — Gust locks and gust lock systems; — Artificial feel, yaw damper, Mach trim, rudder limiter; — Stall-warning systems. (b) Actuation and protection: 1 — 3 — — — Active load control; — Lift dump, speed brakes; — Hydraulic, pneumatic systems; — Stall-protection systems. (c) System operation: 1 — 3 — — Electrical systems, fly-by-wire systems. (d) Balancing and rigging. 1 1 3 3 2 11.10 Fuel systems (ATA 28, ATA 47) (a) Systems: 1 1 3 3 1 — System layout; — Fuel tanks; — Supply systems. (b) Fuel handling: 1 1 3 3 1 — Cross-feed and transfer; — Refuelling and defuelling. (c) Indication and warnings. 1 1 3 3 1 (d) Special systems: 1 — 3 — — — Dumping, venting, and draining; — Inert gas systems. (e) Balancing: 1 — 3 — — Longitudinal balance fuel systems. 11.11 Hydraulic power (ATA 29) (a) System description: 1 1 3 3 2 System layout; Hydraulic fluids; Hydraulic reservoirs and accumulators; Filters;

text: Power distribution. (b) System operation (1): 1 1 3 3 2 Pressure generation: electric and mechanical; Pressure control; Indication and warning systems; Servicing. (c) System operation (2): 1 — 3 — — Pressure generation: pneumatic; Emergency pressure generation; Interface with other systems. 11.12 Ice and rain protection (ATA 30) (a) Principles: 1 1 3 3 1 Ice formation, classification, and detection. (b) De-icing: 1 1 3 3 1 De-icing systems: electrical, hot-air, pneumatic, chemical; Probe and drain heating. (c) Anti-icing: 1 — 3 — — Anti-icing systems: electrical, hot-air, chemical. (d) Wipers: 1 1 3 3 1 Wiper systems. (e) Rain-repellent systems. 1 — 3 — —

text: 11.13 Landing gear (ATA 32) (a) Description: 2 2 3 3 2 Construction, shock absorbing; Tyres. (b) Systems: 2 2 3 3 2 Extension and retraction systems: normal and emergency; Indications and warnings; Wheels, brakes, antiskid, and autobraking; Steering. (c) Air–ground sensing. 2 — 3 — — (d) Tail protection: 2 2 3 3 2 Skids. 11.14 Lights (ATA 33) 2 2 3 3 2 External: navigation, anticollision, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 11.15 Oxygen (ATA 35) 1 1 3 3 2

text: System layout: cockpit, cabin; Sources, storage, charging and distribution; Supply regulation; Indications and warnings. 11.16 Pneumatic / vacuum (ATA 36) (a) Systems: 1 1 3 3 2 System layout; Sources: engine / APU (Auxiliary Power Unit), compressors, reservoirs, ground supply; Pressure control; Distribution; Indications and warnings; Interface with other systems. (b) Pumps: 1 1 3 3 2 Pressure and vacuum pumps. 11.17 Water / waste (ATA 38) (a) Systems: 2 2 3 3 2 Water system layout, supply, distribution, servicing and draining; Toilet system layout, flushing and servicing. (b) Corrosion: 2 2 3 3 2 Corrosion aspects. 11.18 Onboard maintenance systems (ATA 45) 1 — 2 — — Central maintenance computers; Data-loading system; Electronic library system; Printing systems; Structure monitoring (damage-tolerance monitoring). 11.19 Integrated modular avionics (IMA) (ATA 42) 1 — 2 — — (a) Overall system description and theory: Core system; network components; Functions that may be typically integrated in the integrated modular avionics (IMA) modules are, among others: Bleed management, air pressure control, air ventilation and control, avionics and cockpit ventilation control, temperature control, air traffic communication, avionics communication router, electrical load management, circuit breaker monitoring, electrical system BITE, fuel management, braking control, steering control, landing gear extension and retraction, tyre pressure indication, oleo pressure indication, brake temperature monitoring, etc. (b) Typical system layout. 1 — 2 — —

text: 11.20 Cabin systems (ATA 44) 1 — 2 — — System architecture, operation, and control of systems for: — passenger in-flight entertainment; — communication within the aircraft (Cabin intercommunication data system (CIDS); — communication between the aircraft cabin and ground stations; — including voice, data, music, and video transmission. CIDS interface between cockpit/cabin crew and cabin systems. Data exchange between the different related line replaceable units (LRUs). Flight attendant panels (FAPs). Cabin network server (CNS) and interfaces with the following systems: — Data/radio communication; — Cabin core system (CCS); — In-flight entertainment system (IFES); — External communication system (ECS); — Cabin mass memory system (CMMS); — Cabin monitoring system (CMS); — Miscellaneous cabin systems (MCSs); and — Other systems. Cabin network server (CNS) hosting functions: — Access to predeparture/departure reports; — Email/intranet/internet access; passenger database; — In-flight entertainment system; — External communication system; — Cabin mass memory system; — Cabin monitoring system; — Miscellaneous cabin system. 11.21 Information systems (ATA 46) 1 — 2 — — System architecture, operation, and control of: — Storage and electronic library; — Updating; — Retrieving of digital information; — Air traffic and information management systems (ATIMS) and network server systems; — Aircraft general information system; — Flight deck information system; — Maintenance information system;

text: — Passenger cabin information system;

text: — Miscellaneous information systems;

text: — Other linked systems.

text: MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

text: LEVEL

text: MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 B1.3 A4 B1.4

text: 12.1 Theory of flight — rotary wing aerodynamics 1 2 Terminology; Effects of gyroscopic precession; Torque reaction and directional control; Dissymmetry of lift, blade tip stall; Translating tendency and its correction; Coriolis effect and compensation; Vortex ring state, power setting, overpitching; Auto-rotation; Ground effect. 12.2 Flight control systems (ATA 67) 2 3 Cyclic control; Collective control; Swashplate; Yaw control: antitorque control, tail rotor, bleed air; Main-rotor head: design and operation features; Blade dampers: function and construction; Rotor blades: main- and tail-rotor blade construction and attachment; Trim control, fixed and adjustable stabilisers; System operation: manual, hydraulic, electrical, fly-by-wire; Artificial feel; Balancing and rigging. 12.3 Blade tracking and vibration analysis (ATA 18) 1 3 Rotor alignment; Main-rotor and tail-rotor tracking; Static and dynamic balancing; Vibration types, and vibration reduction methods; Ground resonance. 12.4 Transmission 1 3 Gear boxes, main and tail rotors; Clutches, free wheel units and rotor brake; Tail-rotor drive shafts, flexible couplings, bearings, vibration dampers and bearing hangers. 12.5 Airframe structures (a) General concept 2 2 Airworthiness requirements for structural strength;

text: LEVEL

text: Structural classification: primary, secondary, tertiary; Fail-safe, safe-life, damage-tolerance concepts; Zonal and station identification systems; Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue; Drains and ventilation provisions; System installation provisions; Lightning strike protection provisions. (b) Construction methods for the principal elements 1 2 Stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, skinning and anticorrosive protection; Pylon, stabiliser and undercarriage attachments; Seat installation; Doors: construction, mechanisms, operation, and safety devices; Windows and windscreen construction; Fuel storage; Firewalls; Engine mounts; Structure assembly techniques: riveting, bolting, bonding; Methods for surface protection, such as chromating, anodising, painting; Surface cleaning; Airframe symmetry: methods for alignment and symmetry checks. 12.6 Air conditioning (ATA 21) 12.6.1 Air supply 1 2 Sources of air supply, including engine bleed and ground cart. 12.6.2 Air conditioning 1 3 Air-conditioning systems; Distribution systems; Flow and temperature control systems; Protection and warning devices. 12.7 Instruments / avionics systems 12.7.1 Instrument systems (ATA 31) 1 2 Pitot-static: altimeter, airspeed indicator, vertical speed indicator; Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator; Compasses: direct reading, remote reading; Vibration indicating systems / health and usage monitoring systems (HUMSs); Glass cockpit; Indications of other aircraft systems.

text: LEVEL

text: 12.7.2 Avionics systems 1 1 Fundamentals of system layouts and operation of: Autoflight (ATA 22); Communications (ATA 23): — Very high frequency (VHF) communications, — High-frequency (HF) communications, — Satellite communications (SATCOM), — Controller–pilot data link communications (CPDLC), — Audio systems, — Emergency locator transmitters (ELTs), — Cockpit voice recorder (CVR); Navigation systems (ATA 34): — Very high frequency omnidirectional range (VOR), — Automatic direction finding (ADF), — Instrument landing system (ILS), — Microwave landing system (MLS), — Flight director systems (FDSs), distance-measuring equipment (DME), — Area navigation (RNAV) systems, — Flight management systems (FMSs), — Satellite navigation systems, — Inertial navigation system (INS), — Air traffic control transponder, secondary surveillance radar, — Traffic alert and collision avoidance system (TCAS), — Weather avoidance radar, — Radio altimeter, — ARINC communication and reporting. Types and uses of general test equipment for avionics. 12.8 Electric power (ATA 24) 1 3 Installation and operation of batteries; DC power generation, AC power generation; Emergency power generation; Voltage regulation, circuit protection; Power distribution; Inverters, transformers, rectifiers; External/Ground power. 12.9 Equipment and furnishings (ATA 25) (a) Emergency equipment requirements; 2 2 Seats, harnesses, and belts;

text: LEVEL

text: Lifting systems. (b) Emergency flotation systems; 1 1 Cabin layout, cargo retention; Equipment layout; Cabin furnishing installation. 12.10 Fire protection (ATA 26) 1 3 (a) Fire and smoke detection and warning systems; Fire-extinguishing systems; System tests. (b) Portable fire extinguishers. 1 1 12.11 Fuel systems (ATA 28) 1 3 System layout; Fuel tanks; Supply systems; Dumping, venting, and draining; Cross-feed and transfer; Indications and warnings; Refuelling and defuelling. 12.12 Hydraulic power (ATA 29) 1 3 System layout; Hydraulic fluids; Hydraulic reservoirs and accumulators; Pressure generation: electric, mechanical, pneumatic; Emergency pressure generation; Filters; Pressure control; Power distribution; Indication and warning systems; Interface with other systems; Servicing. 12.13 Ice and rain protection (ATA 30) 1 3 Ice formation, classification, and detection; Anti-icing and de-icing systems: electrical, hot-air, and chemical; Rain repellent and removal; Probe and drain heating; Wiper system. 12.14 Landing gear (ATA 32)

text: LEVEL

text: (a) System description and operation: 2 3 Construction, shock absorbing; Extension and retraction systems: normal and emergency; Wheels, tyres, brakes; Steering; Skids, floats. (b) Sensors: 2 3 Indications and warning; Air–ground sensing. 12.15 Lights (ATA 33) 2 3 External: navigation, landing, taxiing; Internal: cabin, cockpit, cargo; Emergency. 12.16 (Reserved)

text: 12.17 Integrated modular avionics (IMA) (ATA 42) 1 2 (a) Overall system description and theory Functions that may be typically integrated in the integrated modular avionics (IMA) modules: Bleed management, air pressure control, air ventilation and control, avionics and cockpit ventilation control, temperature control, air traffic communication, avionics communication router, electrical load management, circuit breaker monitoring, electrical system BITE, fuel management, steering control, landing gear extension and retraction, tyre pressure indication, oleo pressure indication, brake temperature monitoring, etc.; Core System; Network Components. (b) Typical system layouts. 1 2 12.18 Onboard maintenance systems (ATA 45) 1 2 Central maintenance computers; Data-loading system; Electronic library system. 12.19 Information systems (ATA 46) 1 2

text: LEVEL

text: The units and components which furnish a means of storing, updating, and retrieving digital information traditionally provided on paper, microfilm or microfiche. They include units that are dedicated to the information storage and retrieval function, such as the electronic library mass storage and controller. They do not include units or components installed for other uses and shared with other systems, such as flight deck printer or general-use display. Typical examples include air traffic and information management systems and network server systems. Aircraft general information system. Flight deck information system. Maintenance information system. Miscellaneous information system.

text: MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: 13.1 Theory of flight (a) Aeroplane aerodynamics and flight controls 1 1 — — — — — Operation and effect of: — roll control: ailerons and spoilers; — pitch control: elevators, stabilators, variable incidence stabilisers and canards; and — yaw control: rudder limiters; — control using elevons, ruddervators; — high-lift devices: slots, slats, flaps; — drag-inducing devices: spoilers, lift dumpers, speed brakes; — trim tabs, servo tabs, and control surface bias. (b) Rotary wing aerodynamics 1 1 — — — — — Terminology; Operation and effect of cyclic, collective, and antitorque controls. 13.2 Structures — general concepts (a) General concepts; 2 2 — — — — — Zonal and station identification systems; Electrical bonding; Lightning strike protection provisions. (b) Fundamentals of structural systems. 1 1 — — — — —

text: LEVEL MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: 13.3 Autoflight (ATA 22) (a) Fundamentals of automatic flight control: 3 — — — 3 — — — Working principles and current terminology; — Command signal processing; — Modes of operation: roll, pitch, and yaw channels; — Yaw dampers; — Stability augmentation system in helicopters; — Automatic trim control; — Autopilot navigation aids interface. — (b) Autothrottle systems and automatic landing 3 — — — 3 — — systems: — Principles and categories; — Modes of operation; — Approach; — Glideslope; — Land, go-around; — System monitors and failure conditions. 13.4 Communication/navigation (ATA 23/34) (a) Fundamentals of communication and navigation 3 — 3 — — — — systems: — Radio wave propagation, antennas, transmission lines, communication, receiver, and transmitter; Working principles of the following systems: — Very high frequency (VHF) communications; — High-frequency (HF) communications; — Satellite communications (SATCOM); — Controller–pilot data link communications (CPDLC); — Audio systems; — Emergency locator transmitters (ELTs); — Cockpit voice recorder (CVR); — Very high frequency omnidirectional range (VOR); — Automatic direction finding (ADF); — Instrument landing system (ILS); — Flight director systems (FDSs), distancemeasuring equipment (DME); — Area navigation (RNAV) systems; — Flight management systems (FMSs);

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: — Global navigation satellite systems (GNSSs), Global Positioning System (GPS), ground-based augmentation system (GBAS), satellite-based augmentation system (SBAS) such as the European geostationary navigation overlay service (EGNOS) and the wide area augmentation system (WAAS); — Data link and two-way data link. (b) Fundamentals of aircraft surveillance systems: 3 — — — — 3 — — Air traffic control transponder, secondary surveillance radar; — Traffic alert and collision avoidance system (TCAS); — Weather avoidance radar; — Radio altimeter; — Automatic dependent surveillance — broadcast (ADS-B) and its other associated services such as FIS-B, TIS-B and multilink; — Inertial navigation system (INS); — ARINC (Aeronautical Radio Incorporated) communication and reporting. 13.5 Electric power (ATA 24) — Installation and operation of batteries; 3 3 — — — — — — DC power generation; — AC power generation; — Emergency power generation; — Voltage regulation; — Power distribution; — Inverters, transformers, rectifiers; — Circuit protection; — External/ground power. 13.6 Equipment and furnishings (ATA 25) Electronic emergency equipment requirements. 3 — — — — — — 13.7 Flight controls (a) Primary and secondary flight controls (ATA 27): 2 — — — 2 — — — Primary controls: aileron, elevator, rudder, spoiler; — Trim control: trim tabs; — High-lift devices; — System operation: manual; — Gust locks and gust lock systems;

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: — Artificial feel, yaw damper, Mach trim, rudder limiter; — Stall-warning systems. (b) Actuation and protection: 2 — — — 2 — — — Active load control; — Lift dump, speed brakes; — Hydraulic, pneumatic systems; — Stall-protection systems. (c) System operation: 3 — — — 3 — — — System operation: electrical, fly-by-wire. (d) Rotorcraft flight controls (ATA 67): 2 — — — 2 — — Rotorcraft controls: cyclic control, collective control, swashplate, yaw control. 13.8 Instruments (ATA 31) 3 — — 3 — — — — Classification; — Atmosphere; — Terminology; — Pressure-measuring devices and systems; — Pitot-static systems; — Altimeters; — Vertical speed indicators; — Airspeed indicators; — Machmeters; — Altitude-reporting/-alerting systems; — Air-data computers; — Instrument pneumatic systems; — Direct-reading pressure and temperature gauges; — Temperature-indicating systems; — Gyroscopic principles; — Artificial horizons; — Slip indicators; — Directional gyros; — Ground proximity warning systems (GPWSs); — Compass systems; — Flight data recording systems (FDRSs); — Electronic flight instrument systems (EFISs) — typical system arrangements and cockpit layout; — Instrument warning systems, including master warning systems and centralised warning panels;

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: — Stall-warning systems and angle-of-attack indicating systems; — Vibration measurement and indication; — Glass cockpit; — Types and uses of general test equipment for avionics. 13.9 Lights (ATA 33) External: navigation, anticollision, landing, taxiing, ice; 3 3 — — — — — Internal: cabin, cockpit, cargo; Emergency. 13.10 Onboard maintenance systems (ATA 45) Central maintenance computers; 3 — — — — — — Data-loading system; Electronic library system; Printing system; Structure monitoring system (damage-tolerance monitoring). 13.11 Air conditioning and cabin pressurisation (ATA 21) (a) Pressurisation: 3 — — — — — 3 — Pressurisation systems; — Cabin pressure controllers, control and safety valves; — Control and indication. (b) Air supply: 1 — — — — — 1 Sources of air supply including engine bleed, APU and ground cart; Distribution systems. (c) Air conditioning. 3 — — — — — 3 (d) Safety and warning devices. 3 — — — — — 3 13.12 Fire protection (ATA 26) (a) Fire and smoke detection system and fire- 3 — — — — — 3 extinguishing systems; — Fire and smoke detection and warning systems; — Fire-extinguishing systems; — System tests. (b) Portable fire extinguisher. 1 — — — — — 1 13.13 Fuel systems (ATA 28, ATA 47) (a) System layout: 1 — — — — — 1 System layout;

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: Fuel tanks; Supply systems. (b) Fuel handling; 2 — — — — — 2 Cross-feed and transfer; Refuelling and defuelling. (c) Indications and warnings. 3 — — — — — 3 (d) Special systems: 1 — — — — — 1 Dumping, venting and draining; Inert gas systems. (e) Balancing: 3 — — — — — 3 Longitudinal balance fuel systems. 13.14 Hydraulic power (ATA 29) (a) System layout: 1 — — — — — 1 System layout; Hydraulic fluids; Hydraulic reservoirs and accumulators; Filters; Power distribution. (b) System operation (1): 3 — — — — — 3 Pressure generation: electric and mechanical; Pressure control; Indication and warning systems; Servicing. (c) System operation (2): 3 — — — — — 3 Pressure generation: pneumatic; Emergency pressure generation; Interface with other systems.

text: 13.15 Ice and rain protection (ATA 30)

text: (a) Principles: 2 — — — — — 2 Ice formation, classification, and detection. (b) De-icing: 3 — — — — — 3 De-icing systems: electrical, hot-air, pneumatic, and chemical; Probe and drain heating. (c) Anti-icing: 2 — — — — — 2 Anti-icing systems: electrical, hot-air, and chemical. (d) Wiper systems. 1 — — — — — 1 (e) Rain repellent. 1 — — — — — 1

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: 13.16 Landing gear (ATA 32) (a) Description: 1 — — — — — 1 Construction, shock absorbing; Tyres. (b) Systems: 3 — — — — — 3 Extension and retraction systems: normal and emergency; Indications and warnings; Wheels, brakes, antiskid, and autobraking; Steering. (c) Air–ground sensing. 3 — — — — — 3 13.17 Oxygen (ATA 35) System layout: cockpit, cabin; 3 — — — — — 3 Sources, storage, charging, and distribution; Supply regulation; Indications and warnings. 13.18 Pneumatic/vacuum (ATA 36) — System layout; 2 — — — — — 2 — Sources: engine/APU, compressors, reservoirs, ground supply; — Pressure control; — Distribution; — Indications and warnings; — Interfaces with other systems. 13.19 Water/waste (ATA 38) — Water system layout, supply, distribution, servicing, 2 — — — — — 2 and draining; — Toilet system layout, flushing and servicing. 13.20 Integrated modular avionics (IMA) (ATA 42) 3 — — — — — —

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: (a) Overall system description and theory: Core system; Network components. Note: Functions that may be typically integrated into the integrated modular avionics (IMA) modules are, among others: — Bleed management; — Air pressure control; — Air ventilation and control; — Avionics and cockpit ventilation control, temperature control; — Air traffic communication; — Avionics communication router; — Electrical load management; — Circuit breaker monitoring; — Electrical system built-in test equipment (BITE); — Fuel management; — Braking control; — Steering control; — Landing gear extension and retraction; — Tyre pressure indication; — Oleo pressure indication; — Brake temperature monitoring. (b) Typical system layouts. 3 — — — — — — 13.21 Cabin systems (ATA 44) System architecture, operation and control of systems 3 — — — — — — for: — passenger in-flight entertainment; — communication within the aircraft (cabin intercommunication data system (CIDS); — communication between the aircraft cabin and ground stations, including voice, data, music and video transmission. CIDS interface between cockpit/cabin crew and cabin systems; Data exchange between the different related line replaceable units (LRUs); Flight attendant panels (FAPs). CNS server and interfaces with the following systems: — Data/radio communication system;

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: — Cabin core system (CCS); — In-flight entertainment system (IFES); — External communication system (ECS); — Cabin mass memory system (CMMS); — Cabin monitoring system (CMS); — Miscellaneous cabin systems (MCSs). The CNS may host functions such as: — access to predeparture/departure reports; — email/intranet/internet access; — passenger database. 13.22 Information systems (ATA 46) 3 — — — — — — The units and components which furnish a means of storing, updating, and retrieving digital information traditionally provided on paper, microfilm or microfiche. They include units that are dedicated to the information storage and retrieval function, such as the electronic library mass storage and controller, but they do not include units or components installed for other uses and shared with other systems, such as flight deck printer or general-use display. Typical examples include: — air traffic and information management systems and network server systems; — aircraft general information system; — flight deck information system; — maintenance information system; — passenger cabin information system; — miscellaneous information systems; — other linked systems.

text: MODULE 14 — PROPULSION

text: LEVEL

text: B2 MODULE 14 — PROPULSION B2L Instruments B2L Airframe & Systems

text: 14.1 Engines (a) Constructional arrangement and operation of turbojet, turbofan, 1 turboshaft, and turboprop engines. (b) Constructional arrangement and operation of auxiliary power units (APUs). 1 (c) Constructional arrangement and operation of piston engines. 1

text: LEVEL

text: (d) Constructional arrangement and operation of electric and hybrid engines, 2 their electric energy storage and control systems. (e) Electronic engine control and fuel-metering systems (full authority digital 2 engine control (FADEC)). 14.2 Electric/electronic engine indication systems 2 — Exhaust gas temperature / interstage turbine temperature systems; — Cylinder head temperature, engine coolant temperature, engine speed; — Engine thrust indication: engine pressure ratio, engine turbine discharge pressure or jet pipe pressure systems; — Vibration measurement systems; — Oil pressure and temperature; — Fuel pressure, temperature, and flow; — Manifold pressure; — Engine torque. 14.3 Propeller systems 2 — Propeller speed indication; — Speed control and pitch change methods — electrical/electronic; — Synchronising and synchrophasing equipment; — Electrical anti-icing/de-icing equipment. 14.4 Starting and ignition systems 2 — Operation of engine start systems and components; — Ignition systems and components; — Maintenance safety requirements.

text: MODULE 15 — GAS-TURBINE ENGINE

text: LEVEL

text: MODULE 15 — GAS-TURBINE ENGINE A1 B1.1

text: 15.1 Fundamentals 1 2 — Potential energy, kinetic energy, Newton’s laws of motion, Brayton cycle; — The relationship between force, work, power, energy, velocity, and acceleration; — Constructional arrangement and operation of turbojet, turbofan, turboshaft, turboprop, and geared turbofan engines. 15.2 Engine performance – 2 — Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption; — Engine efficiencies;

text: LEVEL

text: MODULE 15 — GAS-TURBINE ENGINE A1 B1.1

text: — By-pass ratio and engine pressure ratio; — Pressure, temperature, and velocity of the gas flow; — Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations. 15.3 Inlet 2 2 — Compressor inlet ducts; — Effects of various inlet configurations; — Ice protection. 15.4 Compressors 1 2 — Axial and centrifugal types; — Constructional features, operating principles, and applications; — Fan balancing; — Operation: o Causes and effects of compressor stall and surge; o Methods of air-flow control: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades; o Compressor ratio. 15.5 Combustion section 1 2 Constructional features and principles of operation. 15.6 Turbine section 2 2 — Operation and characteristics of different turbine blade types; — Blade-to-disk attachment; — Nozzle guide vanes; — Causes and effects of turbine blade stress and creep. 15.7 Exhaust 1 2 — Constructional features and principles of operation; — Convergent, divergent, and variable area nozzles; — Engine noise reduction; — Thrust reversers. 15.8 Bearings and seals — 2 Constructional features and principles of operation. 15.9 Lubricants and fuels 1 2 — Properties and specifications of standard, alternate, and drop-in fuel; — Properties and specifications of lubricants; — Fuel additives; — Safety precautions. 15.10 Lubrication systems 1 2

text: LEVEL

text: MODULE 15 — GAS-TURBINE ENGINE A1 B1.1

text: System operation/layout and components. 15.11 Fuel systems 1 2 — Operation of engine control and fuel-metering systems, including electronic engine control (full authority digital engine control (FADEC)) and electronic power augmentation; — System layout and components. 15.12 Air systems 1 2 Operation of engine air distribution and anti-icing control systems, including internal cooling and sealing, and external air services. 15.13 Starting and ignition systems 1 2 — Operation of engine start systems and components; — Ignition systems and components; — Maintenance safety requirements. 15.14 Engine indication systems 1 2 — Exhaust gas temperature / interstage turbine temperature; — Engine thrust indication: engine pressure ratio, engine turbine discharge pressure or jet pipe pressure systems; — Oil pressure and temperature; — Fuel pressure and flow; — Engine speed; — Vibration measurement and indication; — Torque; — Power. 15.15 Alternate turbine constructions — 1 — Geared turbofan (GTF); — Variable fan blades; — Open rotor/propfan; — Hybrid turbine-electric concepts and electric power augmentation; — Future trends and developments. 15.16 Turboprop engines 1 2 — Gas-coupled/free-turbine and gear-coupled turbines; — Reduction gears; — Integrated engine and propeller controls; — Overspeed safety devices. 15.17 Turboshaft engines 1 2 Arrangements, drive systems, reduction gearing, couplings, control systems. 15.18 Auxiliary power units (APUs) 1 2

text: LEVEL

text: MODULE 15 — GAS-TURBINE ENGINE A1 B1.1

text: Purpose, operation, protective systems. 15.19 Power plant installation 1 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains. 15.20 Fire protection systems 1 2 Operation of fire-detection and fire-extinguishing systems. 15.21 Engine monitoring and ground operation 1 3 — Procedures for starting and ground run-up; — Interpretation of engine power output and parameters; — Trend (including oil analysis, vibration and borescope) monitoring; — Inspection of engine and components to criteria, tolerances and data specified by the engine manufacturer; — Compressor washing/cleaning; — Foreign object damage (FOD). 15.22 Engine storage and preservation — 2 Preservation and depreservation for the engine and its accessories/systems.

text: MODULE 16 — PISTON ENGINE

text: LEVEL

text: MODULE 16 — PISTON ENGINE A2

text: 16.1 Fundamentals 1 2 — Mechanical, thermal, and volumetric efficiencies; — Operating principles: 2-stroke, 4-stroke, Otto, diesel, and rotary (Wankel); — Piston displacement and compression ratio; — Engine configuration and firing order. 16.2 Engine performance 1 2 — Power calculation and measurement; — Factors that affect engine power; — Mixtures/leaning, pre-ignition. 16.3 Engine construction 1 2 — Crank case, crank shaft, cam shafts, sumps; — Accessory gearbox; — Cylinder and piston assemblies; — Connecting rods, inlet and exhaust manifolds; — Valve mechanisms;

text: LEVEL

text: MODULE 16 — PISTON ENGINE A2

text: — Propeller reduction gearboxes. 16.4 Engine fuel systems 16.4.1 Carburettors 1 2 — Types, construction, and principles of operation; — Icing and heating. 16.4.2 Fuel injection systems 1 2 Types, construction, and principles of operation. 16.4.3 Electronic engine control 1 2 — Operation of engine control and fuel-metering systems including electronic engine control (full authority digital engine control (FADEC)); — System layout and components. 16.5 Starting and ignition systems 1 2 — Starting systems, preheat systems; — Magneto types, construction, and principles of operation; — Ignition harnesses, spark plugs; — Low- and high-tension systems. 16.6 Induction, exhaust, and cooling systems 1 2 — Construction and operation of induction systems, including alternate air systems; — Exhaust systems, engine cooling systems — air and liquid. 16.7 Supercharging/turbocharging 1 2 — Principles and purpose of supercharging and its effects on engine parameters; — Construction and operation of supercharging/turbocharging systems; — System terminology; — Control systems; — System protection. 16.8 Lubricants and fuels 1 2 — Properties and specifications of standard, alternate, and drop-in fuel; — Properties and specifications of lubricants; — Fuel additives; — Safety precautions. 16.9 Lubrication systems 1 2 System operation/layout and components. 16.10 Engine indication systems 1 2

text: LEVEL

text: MODULE 16 — PISTON ENGINE A2

text: — Engine speed; — Cylinder head temperature; — Coolant temperature; — Oil pressure and temperature; — Exhaust gas temperature; — Fuel pressure and flow; — Manifold pressure. 16.11 Power plant installation 1 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains. 16.12 Engine monitoring and ground operation 1 3 — Procedures for starting and ground run-up; — Interpretation of engine power output and parameters; — Inspection of engine and components: criteria, tolerances, and data specified by the engine manufacturer. 16.13 Engine storage and preservation — 2 Preservation and depreservation for the engine and its accessories/systems. 16.14 Alternate piston-engine constructions 1 1 Hybrid piston–electric concepts and electric power augmentation.

text: MODULE 17 — PROPELLER

text: LEVEL

text: B1.1 MODULE 17 — PROPELLER A1 B1.2 A2 B3

text: 17.1 Fundamentals 1 2 — Blade element theory; — High/low blade angle, reverse angle, angle of attack, rotational speed; — Propeller slip; — Aerodynamic, centrifugal, and thrust forces; — Torque; — Relative airflow on blade angle of attack; — Vibration and resonance. 17.2 Propeller construction 1 2

text: LEVEL

text: — Construction methods and materials used in wooden, composite and metal propellers; — Blade station, blade face, blade shank, blade back / thrust face and hub assembly; — Fixed pitch, controllable pitch, constant speeding propeller; — Propeller/spinner installation. 17.3 Propeller pitch control 1 2 — Speed control and pitch change methods — mechanical and electrical/electronic; — Feathering and reverse pitch; — Overspeed protection. 17.4 Propeller synchronising — 2 Synchronising and synchrophasing equipment. 17.5 Propeller ice protection 1 2 Fluid and electrical de-icing equipment. 17.6 Propeller maintenance 1 3 — Static and dynamic balancing; — Blade tracking; — Assessment of blade damage, erosion, corrosion, impact damage, delamination; — Propeller treatment/repair schemes; — Propeller engine running. 17.7 Propeller storage and preservation 1 2 Propeller preservation and depreservation.

text: AMC1 Appendix I — Basic Knowledge Requirements (except for category L licence) Section 3

text: Basic training methods

text: Training methods are categorised as follows: ‘instructor-centred training’, ‘student-centred training’, and ‘blended training’. The actual training method and training tools should be adapted to suit the training subject and be chosen considering their intrinsic characteristics, such as but not limited to their efficiency and the pedagogical benefits of the training method/tool. Basic training modules 7, 9, 11, 12, 13, 14, 15, 16 and 17 should not normally be taught solely through a student-centred method unless provisions are in place to verify the actual and progressive acquisition of knowledge, skills and attitude by the student. […]

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

text: The tables below show the acceptable number of questions for the submodules. Justified deviations from these values are also acceptable, provided the sum of the questions complies with the total number of questions for a given module. MODULE 1 — MATHEMATICS

text: Nr of questions

text: B1 MODULE 1 — MATHEMATICS B2 A B2L B3

text: Total number for the module: 16 32 1.1 Arithmetic 6 6 1.2 Algebra: (a) Simple algebraic expressions; 5 4 (b) Equations. — 12 1.3 Geometry: (a) Simple geometrical constructions; — 3 (b) Graphical representation; 5 4 (c) Trigonometry. — 3

text: MODULE 2 — PHYSICS

text: Nr of questions B1 MODULE 2 — PHYSICS A B2 B3 B2L

text: Total number for the module: 32 52 2.1 Matter 4 5

text: 2.2 Mechanics

text: 2.2.1 Statics 6 7 2.2.2 Kinetics 6 7 2.2.3 Dynamics: (a) Mass, force, and energy; 4 5 (b) Momentum and conservation of momentum. 4 4 2.2.4 Fluid dynamics: (a) Gravity and density; 2 2 (b) Viscosity; compressibility on fluids; static, dynamic, and total pressure. 2 3 2.3 Thermodynamics: (a) Temperature; 2 2

text: (b) Heat. 2 8 2.4 Optics (light) — 5 2.5 Wave motion and sound — 4

text: MODULE 3 — ELECTRICS FUNDAMENTALS

text: Nr of questions B1 MODULE 3 — ELECTRICAL FUNDAMENTALS A B2 B3 B2L

text: Total number for the module: 20 24 52 3.1 Electron theory 2 2 2 3.2 Static electricity and conduction 3 2 3 3.3 Electrical terminology 3 2 2 3.4 Generation of electricity 3 2 2 3.5 Sources of DC electricity 3 3 3 3.6 DC circuits 1 1 2 3.7 Resistance/resistor: (a) Resistance; — 1 3 (b) Resistors. — — 2 3.8 Power — 1 3 3.9 Capacitance/capacitor — 1 4 3.10 Magnetism: (a) Theory of magnetism; — 1 3 (b) Magnetomotive force. — 1 1 3.11 Inductance/inductor — 1 4 3.12 DC motor/generator theory — 1 3 3.13 AC theory 5 1 3 3.14 Resistive (R), capacitive (C) and inductive (L) circuits — 1 3 3.15 Transformers — 1 3 3.16 Filters — — 1 3.17 AC generators — 1 3 3.18 AC motors — 1 2

text: MODULE 4 — ELECTRONICS FUNDAMENTALS

text: Nr of questions MODULE 4 — ELECTRONICS FUNDAMENTALS B1 B2 A B3 B2L

text: Total number for the module: — 20 40

text: 4.1 Semiconductors

text: 4.1.1 Diodes: (a) Description and characteristics; — 8 8 (b) Operation and function. — — 7 4.1.2 Transistors: (a) Description and characteristics; — 4 4 (b) Construction and operation. — — 7 4.1.3 Integrated circuits: (a) Basic description and operation; — 3 2 (b) Description and operation. — — 4 4.2 Printed circuit boards — 2 3 4.3 Servomechanisms: (a) Principles; — 3 2 (b) Construction, operation, and use. — — 3

text: Nr of questions MODULE 5 — DIGITAL TECHNIQUES / ELECTRONIC INSTRUMENT SYSTEMS B2 A B3 B1 B2L

text: Total number for the module: 20 20 40 72 5.1 Electronic instrument systems 4 4 4 4 5.2 Numbering systems — — 3 5 5.3 Data conversion — — 3 4 5.4 Data buses — — 3 5 5.5 Logic circuits: (a) Identification and applications; — — 3 4 (b) Interpretation of logic diagrams. — — — 4 5.6 Basic computer structure: (a) Computer terminology and technology; 6 2 4 2 (b) Computer operation. — — — 6 5.7 Microprocessors — — — 4 5.8 Integrated circuits — — — 5 5.9 Multiplexing — — — 4 5.10 Fibre optics — — 3 3 5.11 Electronic displays 2 2 2 4 5.12 Electrostatic sensitive devices 6 6 4 5

text: 5.13 Software management control — 1 3 3 5.14 Electromagnetic environment — 1 3 4 5.15 Typical electronic/digital aircraft systems 2 4 5 6

text: MODULE 6 — MATERIALS AND HARDWARE

text: Nr of questions MODULE 6 — MATERIALS AND HARDWARE B1 B2 A B3 B2L

text: Total number for the module: 52 80 60 6.1 Aircraft materials — ferrous: (a) Alloy steels used in aircraft; 3 3 3 (b) Testing of ferrous materials; — 2 1 (c) Repair and inspection procedures. — 2 1 6.2 Aircraft materials — non-ferrous: (a) Characteristics; 3 4 3 (b) Testing of non-ferrous materials; — 3 2 (c) Repair and inspection procedures. — 2 1

text: 6.3 Aircraft materials — composite and non-metallic

text: 6.3.1 Composite and non-metallic other than wood and fabric: (a) Characteristics; 2 4 3 (b) Detection of defects; 2 4 — (c) Repairs and inspection procedures. — 2 2 6.3.2 Wooden structures 3 4 — 6.3.3 Fabric covering — 4 — 6.4 Corrosion: (a) Chemical fundamentals; 3 3 3 (b) Types of corrosion. 4 5 3

text: 6.5 Fasteners

text: 6.5.1 Screw threads 4 4 3 6.5.2 Bolts, studs, and screws 6 6 5 6.5.3 Locking devices 2 2 2 6.5.4 Aircraft rivets 2 3 2 6.6 Pipes and unions: (a) Identification; 1 1 1 (b) Standard unions. 2 2 2 6.7 Springs — 1 1 6.8 Bearings 2 4 3 6.9 Transmissions 3 4 4 6.10 Control cables 5 5 4 6.11 Electrical cables and connectors 5 6 11

text: MODULE 7 — MAINTENANCE PRACTICES

text: Nr of questions MODULE 7 — MAINTENANCE PRACTICES B1 B2 A B3 B2L

text: Total number for the module: 76 80 60 7.1 Safety precautions — aircraft and workshop 4 4 4 7.2 Workshop practices 4 4 4 7.3 Tools 6 6 6 7.4 (Reserved) — — — 7.5 Engineering drawings, diagrams, and standards 6 6 6 7.6 Fits and clearances 5 5 5 7.7 Electrical wiring interconnection system (EWIS) 4 4 8 7.8 Riveting 4 3 — 7.9 Pipes and hoses 4 3 — 7.10 Springs 1 1 — 7.11 Bearings 4 3 — 7.12 Transmissions 3 3 — 7.13 Control cables 4 3 —

text: 7.14 Material handling

text: 7.14.1 Sheet metal — 2 — 7.14.2 Composite and non-metallic — 2 — 7.14.3 Additive manufacturing 2 4 2 7.15 (Reserved) — — — 7.16 Aircraft weight and balance: (a) Centre-of-gravity calculation; — 2 2 (b) Aircraft weighing. — 1 — 7.17 Aircraft handling and storage 7 5 6 7.18 Disassembly, inspection, repair, and assembly techniques: (a) Types of defects and visual inspection techniques; 2 2 2 (b) General repair methods — structural repair manual; — 2 — (c) Non-destructive inspection techniques; — 1 1 (d) Disassembly and reassembly techniques; 2 1 1 (e) Troubleshooting techniques. — 1 1 7.19 Abnormal events: (a) Inspections following lightning strikes and HIRF penetration; 2 1 2 (b) Inspections following abnormal events such as heavy landing and flight 2 1 — through turbulence. 7.20 Maintenance procedures 6 6 6 7.21 Documentation and communication 4 4 4

text: MODULE 8 — BASIC AERODYNAMICS

text: Nr of questions B1 MODULE 8 — BASIC AERODYNAMICS A B2 B3 B2L

text: Total number for the module: 24 24

text: 8.1 Physics of the atmosphere

text: 2 2 International Standard Atmosphere (ISA), application to aerodynamics. 8.2 Aerodynamics 9 9 8.3 Theory of flight 7 7 8.4 High-speed airflow 4 4 8.5 Flight stability and dynamics 2 2

text: MODULE 9 — HUMAN FACTORS

text: Nr of questions MODULE 9 — HUMAN FACTORS ALL

text: Total number for the module: 28 9.1 General 3 9.2 Human performance and limitations 3 9.3 Social psychology 2 9.4 Factors that affect human performance 3 9.5 Physical environment 2 9.6 Tasks 2 9.7 Communication 3 9.8 Human error 4 9.9 Safety management 2 9.10 The ‘Dirty Dozen’ and risk-mitigation 4

text: MODULE 10 — AVIATION LEGISLATION

text: Nr of questions B1 MODULE 10 — AVIATION LEGISLATION B2 A B2L B3

text: Total number for the module: 32 44 10.1 Regulatory framework 5 5 10.2 Certifying staff — maintenance 7 7 10.3 Approved maintenance organisations 6 6 10.4 Independent certifying staff - 4 10.5 Air operations 4 4 10.6 Certification of aircraft, parts, and appliances 1 4 10.7 Continuing airworthiness 6 7 10.8 Oversight principles in continuing airworthiness 2 3 10.9 Maintenance and certification beyond the current EU regulations — 3

text: (if not superseded by EU requirements)

text: 10.10 Cybersecurity in aviation maintenance 1 1

text: MODULE 11 — AEROPLANE AERODYNAMICS, STRUCTURES Nr of questions

text: Total number for the module: 108 72 140 100 60 11.1 Theory of flight: (a) Aeroplane aerodynamics and flight controls; 2 2 2 2 1 (b) Aeroplane, other aerodynamic devices. 2 2 2 2 1 11.2 Airframe structures (ATA 51): (a) General concepts; 3 3 4 3 2 (b) Airworthiness requirements for structural strength; 3 3 3 3 1 (c) Construction methods. 1 1 3 2 1

text: 11.3 Airframe structures — aeroplanes

text: 11.3.1 Fuselage, doors, windows (ATA 52/53/56): 1 1 2 2 2 (a) Construction principles; (b) Airborne towing devices; 1 1 1 1 1 (c) Doors. 1 1 1 1 - 11.3.2 Wings (ATA 57) 2 2 3 3 2 11.3.3 Stabilisers (ATA 55) 1 1 2 1 1 11.3.4 Flight control surfaces (ATA 55/57) 1 1 2 2 1 11.3.5 Nacelles/pylons (ATA 54) 1 1 2 1 1 11.4 Air conditioning and cabin pressurisation (ATA 21): (a) Pressurisation; 2 2 3 1 —

text: (b) Air supply; 3 — 3 — — (c) Air conditioning; 3 — 3 — — (d) Safety and warning devices; 2 1 2 2 — (e) Heating and ventilation system. — 1 — 2 1

text: 11.5 Instruments / avionics systems

text: 11.5.1 Instrument systems (ATA 31) 2 2 4 3 3

text: 11.5.2 Avionics systems

text: Fundamentals of system layouts and operation of: — Autoflight (ATA 22); 3 2 5 4 4 — Communications (ATA 23); — Navigation systems (ATA 34). 11.6 Electrical power (ATA 24) 4 3 5 5 4

text: 11.7 Equipment and furnishings (ATA 25)

text: (a) Emergency equipment; 4 2 4 3 2 (b) Cabin and cargo layout. 3 3 3 3 -

text: 11.8 Fire protection (ATA 26)

text: (a) Fire and smoke detection system and fire- 3 2 4 3 — extinguishing systems; (b) Portable fire extinguisher. 1 1 1 1 1

text: 11.9 Flight controls (ATA 27)

text: 3 2 4 4 2 (a) Primary and secondary flight controls; (b) Actuation and protection; 3 — 3 3 2 (c) System operation; 3 — 3 2 1 (d) Balancing and rigging. 1 1 3 2 2

text: 11.10 Fuel systems (ATA 28/47)

text: 2 2 3 3 2 (a) Systems layout; (b) Fuel handling; 2 2 2 2 1 (c) Indications and warnings; 1 1 2 2 1 (d) Special systems; 1 — 1 — — (e) Balancing. 2 — 2 — —

text: 11.11 Hydraulic power (ATA 29)

text: 1 1 3 3 2 (a) System description; (b) System operation (1); 1 1 3 1 1 (c) System operation (2). 2 — 2 — —

text: 11.12 Ice and rain protection (ATA 30)

text: 1 1 2 2 1 (a) Principles; (b) De-icing; 1 1 2 2 1

text: (c) Anti-icing; 1 — 2 — — (d) Wipers; 1 1 2 2 1 (e) Rain-repellent systems. 2 — 2 — —

text: 11.13 Landing gear (ATA 32)

text: 3 3 4 3 1 (a) Description; (b) System operation; 3 3 4 2 1 (c) Air–ground sensing; 1 — 1 — — (d) Tail protection. 1 1 1 1 1 11.14 Lights (ATA 33) 2 2 3 3 2 11.15 Oxygen (ATA 35) 3 3 4 4 3

text: 11.16 Pneumatic/vacuum (ATA 36)

text: (a)Systems; 3 3 3 3 2 (b)Pumps. 3 3 3 3 2

text: 11.17 Water/waste (ATA 38)

text: (a)Systems; 2 2 2 2 1 (b)Corrosion. 1 1 1 1 1 11.18 Onboard maintenance systems (ATA 45) 3 — 3 — —

text: 11.19 Integrated modular avionics (IMA) (ATA 42)

text: (a)Overall system description and theory; 1 — 1 — — (b)Typical system layouts. 1 — 1 — — 11.20 Cabin systems (ATA 44) 2 — 2 — — 11.21 Information systems (ATA 46) 2 — 2 — —

text: Nr of questions MODULE 12 — HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS A3 B1.3 A4 B1.4

text: Total number for the module: 100 128 12.1 Theory of flight — rotary wing aerodynamics 6 9 12.2 Flight control systems (ATA 67) 9 9 12.3 Blade tracking and vibration analysis (ATA 18) 6 9 12.4 Transmission 3 6

text: 12.5 Airframe structures (ATA 51)

text: (a) General concept; 5 6 (b) Construction methods of the principal elements. 5 7 12.6 Air conditioning (ATA 21) — —

text: 12.6.1 Air supply 1 2 12.6.2 Air conditioning 3 5

text: 12.7 Instruments / avionics systems

text: 12.7.1 Instrument systems (ATA 31) 6 9 12.7.2 Avionics systems 5 7 Fundamentals of system layouts and operation of: — Autoflight (ATA 22); — Communications (ATA 23); — Navigation systems (ATA 34). 12.8 Electrical power (ATA 24) 8 10

text: 12.9 Equipment and furnishings (ATA 25)

text: (a) Emergency equipment: 2 3 Seats, harnesses, and belts; Lifting systems. (b) Emergency flotation systems: 3 3 Cabin layout, cargo retention; Equipment layout; Cabin furnishing installation. 12.10 Fire protection (ATA 26) 3 4 (a) Fire and smoke detection systems and fire-extinguishing systems; (b) Portable fire extinguishers. 1 1 12.11 Fuel systems (ATA 28) 7 8 12.12 Hydraulic power (ATA 29) 8 8 12.13 Ice and rain protection (ATA 30) 4 4

text: 12.14 Landing gear (ATA 32)

text: (a) System description and operation; 3 4 (b) Sensors. 3 3 12.15 Lights (ATA 33) 3 4

text: 12.16 (Reserved)

text: 12.17 Integrated modular avionics (IMA) (ATA 42)

text: (a) Overall system description and theory; 1 1 (b) Typical system layouts. 1 1 12.18 Onboard maintenance systems (ATA 45) 2 3 Central maintenance computers; Data-loading system; Electronic library system. 12.19 Information systems (ATA 46) 2 2

text: Nr of questions

text: MODULE 13 — AIRCRAFT AERODYNAMICS, STRUCTURES

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: Total number for the module: 188 32 24 20 28 20 50

text: 13.1 Theory of flight

text: (a) Aeroplane aerodynamics and flight controls; 3 3 — — — — — (b) Rotary wing aerodynamics. 1 1 — — — — —

text: 13.2 Structures — general concepts (ATA 51)

text: (a) General concepts; 4 4 — — — — — (b) Fundamentals of structural systems. 4 4 — — — — —

text: 13.3 Autoflight (ATA 22)

text: (a) Fundamentals of automatic flight control; 12 — — — 8 — —

text: (b) Autothrottle systems and automatic landing 8 — — — 8 — — systems.

text: 13.4 Communication/navigation (ATA 23/34)

text: (a) Fundamentals of communication and 24 — 24 — — — — navigation systems; (b) Fundamentals of aircraft surveillance systems. 3 — — — — 20 —

text: 13.5 Electrical power (ATA 24) 13 13 — — — — — 13.6 Equipment and furnishings (ATA 25) 5 — — — — — —

text: 13.7 Flight controls

text: (a) Primary and secondary flight controls (ATA 27); 4 — — — 3 — — (b) Actuation and protection; 4 — — — 3 — — (c) System operation; 2 — — — 3 — — (d) Rotorcraft flight controls (ATA 67). 2 — — — 3 — — 13.8 Instruments (ATA 31) 20 — — 20 — — — 13.9 Lights (ATA 33) 7 7 — — — — — 13.10 Onboard maintenance systems (ATA 45) 5 – – – – – –

text: 13.11 Air conditioning and cabin pressurisation (ATA 21)

text: (a) Pressurisation; 2 — — — — — 2 (b) Air supply; 2 — — — — — 2 (c) Air conditioning; 2 — — — — — 2 (d) Safety and warning devices. 2 — — — — — 2

text: 13.12 Fire protection (ATA 26)

text: (a) Fire and smoke detection system and fire- 2 — — — — — 2 extinguishing systems; (b) Portable fire extinguisher. 1 — — — — — 1

text: 13.13 Fuel systems (ATA 28, ATA 47)

text: (a) System layout; 2 — — — — — 2 (b) Fuel handling; 2 — — — — — 2

text: Nr of questions

text: B2L B2L B2L B2L B2L B2L

text: AND SYSTEMS B2

text: Basic C/N Ins. A/F Sur. A/S

text: (c) Indications and warnings; 2 — — — — — 2 (d) Special systems; 2 — — — — — 2 (e) Balancing. 1 — — — — — 1

text: 13.14 Hydraulic power (ATA 29)

text: (a) System layout; 1 — — — — — 1 (b) System operation (1); 5 — — — — — 4 (c) System operation (2). 5 — — — — — 4

text: 13.15 Ice and rain protection (ATA 30)

text: (a) Principles; 1 — — — — — 1 (b) De-icing; 2 — — — — — 2 (c) Anti-icing; 1 — — — — — 1 (d) Wiper systems; 1 — — — — — 1 (e) Rain repellent. 1 — — — — — 1

text: 13.16 Landing gear (ATA 32)

text: (a) Description; 1 — — — — — 1 (b) System; 3 — — — — — 3 (c) Air–ground sensing. 3 — — — — — 3 13.17 Oxygen (ATA 35) 2 – — — — — — 13.18 Pneumatic/vacuum (ATA 36) 6 – — — — — 6 13.19 Water/waste (ATA 38) 2 – — — — — 2

text: 13.20 Integrated modular avionics (IMA) (ATA 42)

text: (a) Overall system description and theory; 2 — — — — — — (b) Typical system layouts. 1 — — — — — — 13.21 Cabin systems (ATA 44) 3 — — — — — — 13.22 Information systems (ATA 46) 3 — — — — — —

text: MODULE 14 — PROPULSION

text: Nr of questions B2 MODULE 14 — PROPULSION B2L Instruments B2L Airframe and Systems

text: Total number for the module: 32

text: 14.1 Engines

text: (a) Turbine engines; 3 (b) Auxiliary power units (APUs); 4 (c) Piston engines; 2 (d) Electric and hybrid engines; 4 (e) Engine control. 3 14.2 Electric/electronic engine indication systems 10 14.3 Propeller systems 2

text: 14.4 Starting and ignition systems 4

text: MODULE 15 — GAS-TURBINE ENGINE

text: Nr of questions MODULE 15 — GAS-TURBINE ENGINE A1 B1.1 A3 B1.3

text: Total number for the module: 60 92 15.1 Fundamentals 4 4 15.2 Engine performance — 6 15.3 Inlet 3 4 15.4 Compressors 5 7 15.5 Combustion section 3 3 15.6 Turbine section 5 5 15.7 Exhaust 4 4 15.8 Bearings and seals — 3 15.9 Lubricants and fuels 3 4 15.10 Lubrication systems 3 4 15.11 Fuel systems 4 5 15.12 Air systems 3 3 15.13 Starting and ignition systems 3 4 15.14 Engine indication systems 5 7 15.15 Alternate turbine constructions — 2 15.16 Turboprop engines 3 5 15.17 Turboshaft engines 2 3 15.18 Auxiliary power units (APUs) 2 3 15.19 Power plant installation 2 3 15.20 Fire protection systems 2 3 15.21 Engine monitoring and ground operation 4 7 15.22 Engine storage and preservation — 3

text: MODULE 16 — PISTON ENGINE

text: Nr of questions MODULE 16 — PISTON ENGINE B1.2 A2 B1.4 A4 B3

text: Total number for the module: 52 76 16.1 Fundamentals of piston engines 5 5 16.2 Engine performance 3 5 16.3 Engine construction 7 8 16.4 Engine fuel systems — — 16.4.1 Carburettors 3 4 16.4.2 Fuel injection systems 2 4 16.4.3 Electronic engine control 2 4 16.5 Starting and ignition systems 5 5 16.6 Induction, exhaust, and cooling systems 3 4 16.7 Supercharging/turbocharging 4 6 16.8 Lubricants and fuels 2 5 16.9 Lubrication systems 3 4 16.10 Engine indication systems 6 7 16.11 Power plant installation 3 3 16.12 Engine monitoring and ground operation 3 5 16.13 Engine storage and preservation — 3 16.14 Alternative piston-engine constructions 1 4

text: MODULE 17 — PROPELLER

text: Nr of questions MODULE 17 — PROPELLER B1.1 A1 B1.2 A2 B3

text: Total number for the module: 20 32 17.1 Fundamentals of propellers 5 8 17.2 Propeller construction 4 5 17.3 Propeller pitch control 4 6 17.4 Propeller synchronising — 2 17.5 Propeller ice protection 2 3 17.6 Propeller maintenance 3 6 17.7 Propeller storage and preservation 2 2

text: AMC1 to Section 1 of Appendix III to Part-66 ‘Aircraft Ttype Ttraining and Examination type evaluation Sstandard. — Oon-the- Jjob Ttraining’ (OJT) Section 1

text: Aircraft Type Training […] 6. The theoretical and practical training should be complementary and may be: – Iintegrated or split; – Ssupported by the use of training aids, such as trainers, virtual aircraft, aircraft components, maintenance simulation training devices (MSTDs) and maintenance training devices (MTDs).synthetic training devices (STD), computer based training devices (CBT), etc. 7. The integration and usage of MSTDs and MTDs, as defined in AMC 147.A.30(a), in maintenance type training (theoretical and/or practical) should consider the following: — The use of actual aircraft components should be allowed for any MSTD or MTD, even if the components are in a non-airworthy condition. — The complexity and degree of simulation for an MSTD may vary and should support type training elements that address a component, a system or the entire aircraft. Based on its characteristics and capabilities, the MSTD may be: — a training device capable of providing, for the respective component or system, the representation of aircraft location, access and layout, and for servicing with an acceptable level of accuracy and limited simulation; or — a training device capable of providing, for the respective component or system, the representation of aircraft location, access and layout with sufficient accuracy and with interactive simulation for servicing, and the applicable maintenance data for operational (O) and functional (F) test elements including built-in test (BIT) initiation and monitoring from outside the cockpit; such representation should have the capability to accommodate some troubleshooting scenarios; or — a training device capable of providing, for the respective component or system, the representation of onboard (flight deck/cockpit or cabin) indication and controls with an acceptable level of accuracy and limited interactive simulation; or — a training device capable of providing, for the respective component or system, the representation of onboard (flight deck/cockpit or cabin) indication and controls with sufficient accuracy and with interactive simulation for servicing, and the applicable maintenance data for operational (O) and functional (F) test elements including built-in test (BIT) initiation and monitoring; such representation should have the capability to accommodate some troubleshooting scenarios; or — any combination of the above. — Flight simulation training devices (FSTDs) may be used as MSTDs whenever their characteristics and capabilities are considered appropriate for, and supportive of, the delivery of the respective maintenance training element(s). — An MTD is any training device other than an MSTD used for maintenance training and/or examination and/or assessment.

text: GM1 Appendix III Aircraft type training and type evaluation standard — on-the-job training (OJT) Section 1(c)

text: DIFFERENCES TRAINING If the holder of a B1 and B2 licence, without any type rating, successfully completes a combined type training course (B1 + B2) followed by an OJT tailored only to B1 tasks, they can obtain only the typerating endorsement that is applicable to the B1 subcategory. Within the next 3 years from the completion of the combined training course, endorsement of the aircraft type for the B2 category is possible after carrying out an OJT programme limited to the tasks relevant to the B2 category only. When instead, the aircraft type endorsement would be requested after more than 3 years, the applicant would be required to also pass a differences type training course (from B1 to B2) plus the OJT programme limited to the tasks relevant to the B2 category only. All common theoretical and practical elements, and OJT tasks, already demonstrated as B1, shall be considered fulfilled.

text: AMC1 Appendix III Aircraft type training and type evaluation standard — on-the-job training (OJT) Section 3

text: AIRCRAFT TYPE TRAINING STANDARD Training methods are categorised as ‘instructor-centred’, ‘student-centred’ and ‘blended training’. The actual training method and the training tools should be adapted to suit the training subject and be chosen considering their intrinsic characteristics, such as but not limited to their efficiency and the pedagogical benefits of the method/tool. A complex or critical subject should not normally be taught solely through a student-centred method unless provisions are in place to verify the actual and progressive acquisition of knowledge of the student. Complex and critical areas should be identified by the training needs analysis (TNA). The complexity and criticality of the areas could differ on a case-by-case basis (that is, areas proven to be critical by organisations’ ‘in-service events’, occurrence reporting, human factors, safety, etc.), but should in any case cover the maintenance areas with special emphasis (MASE) identified by the type-certificate holder (TCH) in its operational suitability data (OSD).

text: AMC1 to point 3.1(d) of Appendix III to Part-66 ‘Aircraft Ttype Ttraining and Examination type evaluation Sstandard. – Oon-the- Jjob Ttraining’ (OJT) Section 3.1(d)

text: Training Nneeds Aanalysis (TNA) for the Ttheoretical Eelement of the Aaircraft Ttype Ttraining […] 4. In order to approve a reduction of such minimum duration, the evaluation done by the competent authority should be performed on a case-by-case basis appropriate to the aircraft type. For example, while it would be exceptional for a theoretical course for a transport category complex motor-powered aircraft such as an A330 or B757 to be below the minimum duration shown, it would not necessarily be exceptional in the case of a General Aviation (GA) business aircraft such as a Learjet 45 or similar. Typically the TNA for a GA aircraft course would demonstrate that a course of a shorter duration satisfies the requirement. In order to approve the reduction of such minimum duration, the competent authority should perform an assessment on a case-by-case basis, and the assessment should be appropriate to the aircraft type and to the training methods and tools proposed. For example: (a) While it would be exceptional for a theoretical course for a large transport category aircraft, such as an A330 or a B777, to be below the minimum duration shown, it would not necessarily be exceptional in the case of a business aircraft, such as a Learjet 45 or similar. The TNA for a business aircraft course could demonstrate that a course of a shorter duration satisfies the applicable requirements. (b) The use of an MSTD (i.e. flat panel trainer) comprising aircraft-type-specific software may result in the duration of the training being reduced due to a more effective transfer of knowledge. (c) The use of multimedia-based training (MBT), or blending the training methods, may improve the efficiency of the training and, consequently, contribute to the reduction of the overall time needed to achieve the learning objectives. 5. When developing the TNA, the following should be considered: […] (g) The TNA should: […] • Describe the following: - The instructional methods and equipment training tools and their blended application, teaching methods and blending of the teaching methods in order to ensure the effectiveness of the training.; - The maintenance training documentation/material to be delivered to the student.; - Facilitated discussions, questioning session, additional practiced-oriented training, etc.; - The homework, if developed, i.e. to support the achievement of the learning objectives while using asynchronous distance-learning or self-learning methods. - The training provider’s resources available to the learner. (h) It is acceptable to differentiate between subjects issues which have to be led by an instructor and subjects issues which may be delivered through interactive simulation training devices and/or covered by web based self-paced elements. The Ooverall time of the course will be allocated accordingly. (i) […] (j) The minimum participation time for the trainee in order for the trainee to meet the objectives of the course should not be less than 90 % of the tuition hours, or 95 % completion of the content in case of student-centred methods in aof the theoretical training course. Additional training may be provided by the training organisation in order to meet the minimum participation time. If the minimum participation defined for the course is not met, a certificate of recognition should not be issued. (k) […] […]

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

text: Type training examination and assessment standard 4.1 Theoretical element examination standard Examinations may be computer or paper based, or a combination of both. Refer to point 147.A.135.

text: AMC1 to Section 6 of Appendix III to Part-66 ‘Aircraft Ttype Ttraining and Examination type evaluation Sstandard. — Oon-the- Jjob Ttraining (OJT) Section 6

text: On-the-Job Training (OJT) 1. ‘A maintenance organisation appropriately approved for the maintenance of the particular aircraft type’ means a Part-145, M.A. Subpart F or Part-CAO approved maintenance organisation holding an A rating for such aircraft. 2. The OJT should include one to one supervision and should involve actual work task performance on aircraft/components, covering line and/or base maintenance tasks. 3. The use of simulators for OJT should not be allowed. 4. The OJT should cover at least 50 % of the tasks contained in Appendix II to AMC to Part-66. Some tasks should be selected from each paragraph of the Appendix II list. Tasks should be selected among those applicable to the type of aircraft and licence (sub)category applied for. Other tasks than those in the Appendix II may be considered as a replacement when they are relevant. Typically, in addition to the variety and the complexity, the OJT tasks should be selected because of their frequency, safety, novelty, etc. 5. Up to 50 % of the required OJT may be undertaken before the aircraft theoretical type training starts. 6. The organisation providing the on-the-job training should provide trainees a schedule or plan indicating the list of tasks to be performed under supervision. A record of the tasks completed should be entered into a logbook which should be designed such that each task or group of tasks is countersigned by the corresponding supervisor. The logbook format and its use should be clearly defined. 7. Regarding the day-to-day supervision of the OJT programme in the approved maintenance organisation and the role of the supervisor(s), the following should be considered: — It is sufficient that the completion of individual OJT tasks is confirmed by the direct supervisor(s), without being necessary the direct evaluation of the assessor. — During the day-to-day OJT performance, the supervision aims at overseeing the complete process, including task completion, use of manuals and procedures, observance of safety measures, warnings and recommendations and adequate behaviour in the maintenance environment. — The supervisor(s) should personally observe the work being performed to ensure the safe completeness and should be readily available for consultation, if needed during the OJT performance. — The supervisor(s) should countersign the tasks and release the maintenance tasks as the trainee is still not qualified to do so. — The supervisor(s) should therefore: − have certifying staff or support staff privileges relevant to the OJT tasks; − be competent for the selected tasks; − be safety-orientated; − be capable to coach (setting objectives, giving training, performing supervision, evaluating, handling trainee’s reactions and cultural issues, managing objectively and positively debriefing sessions, determining the need for extra training or reorientate the training, reporting, etc.); − be designated by the approved maintenance organisation to carry out the supervision. 8. Regarding the assessor, the following should be considered: — The function of the assessor, as described in Section 6 of Appendix III to Part-66, is to conduct the final assessment of the completed OJT. This assessment should include confirmation of the completion of the required diversity and quantity of OJT and should be based on the supervisor(s) reports and feedback. — In Section 6 of Appendix III to Part-66, the term ‘designated assessor appropriately qualified’ means that the assessor should demonstrate training and experience on the assessment process being undertaken and should be authorised to do so by the organisation. Further guidance about the assessment and the designated assessors is provided in Appendix III to AMC to Part-66. 9. The procedures for OJT of a part-145 Organisation should be included into the approved maintenance organisation exposition (Chapter 3.20 as indicated in AMC 145.A.70(a)). However, since these procedures are approved by the competent authority of the maintenance organisation, and providing training is not one of the privileges of a maintenance organisation, they can only be used when the licensing authority is the same as the competent authority of the maintenance organisation. In other cases, it is up to the licensing authority to decide whether it accepts such procedures for the purpose of approving the OJT (refer to AMC 66.B.115). On-the-job training (OJT) General ‘Maintenance organisations appropriately approved according to this Regulation for the maintenance of that aircraft type’ means Part-145 or Part-CAO approved maintenance organisations (AMO) that hold an ‘A’ rating for such aircraft. The OJT may be split in several parts and carried out at different AMOs, also combining line and base facilities from the same or different organisations. The organisation at which the final assessment is carried out, should control and coordinate the OJT activities and have the responsibility for the entire OJT programme. The procedures for the OJT should be included in the Exposition Manual of the approved maintenance organisation. ‘Skills and responsibilities of a typical certifying staff’ include but are not limited to: — understanding the importance of professional integrity, behaviour and having an appropriate attitude towards safety; — understanding the conditions for ensuring the continuing airworthiness of aircraft and components; — the ability to identify and rectify existing and potential unsafe conditions; — the ability to prioritise tasks, coordinate with a team, and report discrepancies; — the ability to determine the required qualifications for the performance of maintenance tasks; — the ability to confirm the proper accomplishment of maintenance tasks; — the ability to compile and control completed work cards; — knowledge of safety risks linked to a particular working environment; — understanding of human performance and limitations; — understanding of the AMO’s (where the OJT is performed) privileges and limitations; — understanding of the AMO’s personnel authorisations and limitations; — being familiar with the AMO’s documents/forms (work packages, work orders, work cards, etc.); — being familiar with AMO’s release-to-service procedures: use of the aircraft technical logbook (ATLB), deferral of items and dispatch under MEL/CDL; — access, use and control of the required tools and equipment; — access, use and control of the required ICAs (AMM, TSM, SRM, etc.). OJT content and OJT logbook If the aircraft manufacturer has defined the OJT tasks during the type certification of a particular aircraft type (e.g. the operational suitability data (OSD) has been approved for a particular aircraft type), those tasks should be selected. In particular, the analysis performed for the maintenance areas of specific emphasis (MASE), as defined in point 430 of CS-MCSD, helps the organisation identify the more appropriate tasks. Where no such data exists, the task list in Appendix II to the AMC to Annex III (Part-66) serves as the basis to develop an OJT programme including the applicable tasks for a particular aircraft type, based typically on the AMM. The tasks may be selected from the table in Appendix II in order to cover a broader representative sample of both simple and complex tasks on the particular aircraft type in order to reach a balanced distribution of the tasks between line and base maintenance. The tasks should be selected among those that are applicable to the aircraft type and the licence (sub)category applied for; for example, the selection could exclude location tasks (LOC) and tasks that can be considered under the category A licence privileges (seat covers, boilers, wheels, etc.). A minimum number of tasks, as described in point 2 ‘List of tasks for OJT’ of Appendix II, of each of the following categories should be performed: INS/inspections, FOT/functional or operational, SGH/servicing, R/I removal and installation, MEL, and T/S troubleshooting. The licensing authority may accept that a limited number of tasks is not performed as long as the relevant cross section of the tasks as regards quality, quantity and complexity is still assured. A task may be performed on the analogous system installed on a different aircraft type when the systems are similar in terms of design architecture, technology, and functionality. This can be the case, for example, for tasks performed on engines or landing gear of aircraft of the same manufacturer. Such task should be clearly identified and recorded. Certain maintenance tasks could be performed on non-airworthy aircraft that still maintain functionality of systems to the extent that the maintenance tasks can be completely performed without any deviation from the maintenance instructions. Tasks circumscribed to system components may be performed at the workshop. This can be the case, for example, for avionics functional tests. Such scenarios should be limited to specific tasks that may not occur often in the maintenance of operational aircraft. The use of MSTDs and MTDs for OJT should be restricted to a minimum. When an existing licence is changed to include an additional category with a type rating, a different OJT from the category held to the new one may be permissible. In those cases, only tasks corresponding to the differences between the two categories should be performed. The OJT may be partly performed on aircraft whose maintenance is not subject to

text: Regulation (EU) 2018/1139

text: (for example, aircraft subject to the FAA regulatory framework or training helicopters used by the military) provided that the maintenance is subject to the same procedures and manuals. A minimum of maintenance activity on aircraft that are subject to

text: Regulation (EU) 2018/1139

text: is, however, required in order to gain sufficient insight into the European civil aviation regulatory framework and into release-to-service procedures. The acceptance of the OJT is up to the licensing authority. The organisation that has control over the OJT should provide candidates with a schedule or plan which indicates the list of tasks to be performed under supervision. A record of the completed tasks is to be entered into a logbook whose design and format should be such that each task or group of tasks is countersigned by the corresponding mentor(s). Regarding day-to-day supervision of the OJT programme in the approved maintenance organisation and the role of the mentor(s), the following should be considered: — It is sufficient for the completion of the individual OJT tasks to be confirmed by the direct mentor(s), without the direct evaluation of the assessor being necessary. — During the day-to-day OJT performance, the aim of the supervision is for mentors to oversee the whole process, including task completion, use of manuals, adherence to procedures, observance of safety measures, warnings, cautions and recommendations, and demonstration of appropriate behaviour in the maintenance environment. — The mentor(s) should personally observe the work being performed to ensure its safe completion, and should be readily available for consultation if needed during the OJT. — The mentor(s) should sign the tasks and release the maintenance tasks as the candidate is still not qualified to do so. — The mentor(s) should be designated by the approved maintenance organisation to supervise. For training in release-to-service procedures, following the completion of the performance of a specific task chosen by the mentor, the candidate should prepare a document with simulated release to service which has to be marked as ‘for training purposes only’ (e.g. ATL page, maintenance task card, CRS). If both the task and the simulated release to service have been performed to the satisfaction of the mentor, the task may be countersigned in the OJT task list by the mentor. A physical or electronic copy of the document with simulated release should be added to the syllabus. Tasks which are usually performed with more than one person may be performed by more than one candidate under the supervision of one mentor. During the performance of the tasks, the mentor is limited to overseeing three candidates at the same time, given that the candidates can be properly seen ‘at a glance’ from the mentor’s position. Those tasks should be marked as ‘group tasks’ when applying for the approval. All other tasks should be a one-to-one mentorship. In such cases, all the candidates involved should be noted on the work order. At the end of the performance of the OJT, a compliance report shall be made which verifies and documents the correct and complete performance and the recommendation of the mentor(s) for the following assessment. The mentor(s) may deny a recommendation if the candidate has not demonstrated the knowledge, skills, behaviour and/or ethics required from certifying staff. Final assessment of the applicant The OJT assessment should consist of a theoretical part and a practical part. The theoretical part comprises the regulatory framework, safety procedures, knowledge of aircraft and its systems, maintenance procedures, and other typical certifying staff activities such as: — the review and acceptance of work orders; — shift-handover procedures and team coordination; — communication and interaction with the flight crew; — dispatch with unserviceable items; — clear aircraft logbook entries and reporting notes; — checks before release to service. The practical part should include maintenance tasks on the aircraft (e.g. rem./inst., TS, R/I, FOT, MEL dispatch). The assessor may decide to simulate some aspects of the maintenance tasks. The aircraft type on which the OJT is performed needs to be available for the assessment together with access to the required maintenance data, equipment, and tools. A training aircraft may be acceptable. It is good practice to assess the practical skills on the aircraft in question while the assessment of knowledge may be performed either on the aircraft or in theory. Further guidance about the designated assessors is provided in the AMC to Appendix III to Part-66. If an independent observer is required for the OJT, they shall be selected by the maintenance organisation among the maintenance personnel that have not taken part in the OJT performance but do have an adequate understanding of the OJT procedures. […]

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

text: MODULE 1L — BASIC KNOWLEDGE

text: MODULE 1L — BASIC KNOWLEDGE Level

text: 1L.1 Mathematics 1 Arithmetic: — Arithmetical terms and signs; — Methods of multiplication and division; — Fractions and decimals; — Factors and multiples; — Weights, measures, and conversion factors; — Ratio and proportion; — Averages and percentages; — Areas and volumes, squares, cubes. Algebra: — Evaluating simple algebraic expressions: addition, subtraction, multiplication, and division; — Use of brackets; — Simple algebraic fractions.

text: MODULE 1L — BASIC KNOWLEDGE Level

text: Geometry: — Simple geometrical constructions; — Graphical representation: nature and uses of graphs. 1L.2 Physics 1 Matter: — Nature of matter: the chemical elements; — Chemical compounds; — States: solid, liquid, gaseous; — Changes between states. Mechanics: — Forces, moments and couples, and representation as vectors; — Centre of gravity; — Tension, compression, shear, and torsion; — Nature and properties of solids, fluids, and gases. Temperature: — Thermometers and temperature scales: Celsius, Fahrenheit, and Kelvin; — Definition. 1L.3 Electrics 1 AC and DC circuits: — Ohm’s law, Kirchhoff’s voltage, and current laws; — Significance of the internal resistance of a supply; — Resistance/resistor; — Resistor colour code, values and tolerances, preferred values, wattage ratings; — Resistors in series and in parallel. 1L.4 Aerodynamics/aerostatics 1 International Standard Atmosphere (ISA), application to aerodynamics and aerostatics. 1L.5 Workplace safety and environmental protection 2 — Safe working practices and precautions when working with electricity, gases (especially oxygen), oils, and chemicals; — Labelling, storage and disposal of hazardous (to workplace safety and environment) materials; — Remedial action in the event of a fire or another accident with one or more hazards, including knowledge of fire-extinguishing agents.

text: MODULE 2L — HUMAN FACTORS

text: MODULE 2L — HUMAN FACTORS Level

text: 2L.1 General 1 — The need to take human factors into account in the maintenance domain; — Incidents attributable to human factors/human error; — Murphy’s law. 2L.2 Human performance and limitations 1 Vision, hearing, information processing, attention and perception, memory. 2L.3 Social psychology 1 Responsibility, motivation, peer pressure, teamwork. 2L.4 Factors that affect performance 1 Fitness, physical and mental health, stress, sleep, fatigue, alcohol, medication, drug abuse. 2L.5 Physical environment 1

text: MODULE 2L — HUMAN FACTORS Level

text: Working environment (climate, noise, illumination). 2L.6 The ‘Dirty Dozen’ and risk-mitigation 2 The ‘Dirty Dozen’: — lack of communication — lack of teamwork — lack of assertiveness — complacency — fatigue — stress — lack of knowledge — lack of resources — lack of awareness — distraction — pressure — norms. Risk-mitigation methods.

text: MODULE 3L — AVIATION LEGISLATION

text: MODULE 3L — AVIATION LEGISLATION Level

text: 3L.1 Regulatory framework 1 — Role of the European Commission (EC), the European Union Aviation Safety Agency (EASA) and national aviation authorities (NAAs); — Scope and limitations of the regulatory framework. 3L.2 Continuing airworthiness regulations 1 — General understanding of the applicable parts of Part-66; — General understanding of the applicable parts of Part-ML; — General understanding of the applicable parts of Part-CAO; — General understanding of Part-M, Part-CAMO and Part-145. 3L.3 Repairs and modifications (Part-ML) 2 — Approval of changes (repairs and modifications); — Standard changes and standard repairs. 3L.4 Maintenance data (Part-ML) 2 — Airworthiness directives (ADs), safety information bulletins (SIBs); — Service bulletins (SBs), instructions for Continuing Airworthiness (ICAs) (AMM, IPC, etc.), aircraft flight manual (AFM), maintenance records, maintenance programmes. 3L.5 Licence privileges and how to exercise them properly (Part-66, Part-ML) 2 Conditions for release to service: — in a maintenance organisation; — as independent certifying staff; — release-to-service procedures.

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

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

text: 4L.1 Airframe wooden/combination of metal tube and fabric 2 — General construction principles for wooden structures covered with fabric, metal-tube structures covered with fabric, and combination of wooden and metal-tube structures; — Wood as a technical material (heartwood, sapwood, grain, etc.); — Wood defects (types, acceptable/ not acceptable); — Different woodcuts (tangential cuts, radial cuts, etc.) and their properties (tangential cuts, radial cuts, etc.); — Metal tubing (mechanical and stress properties of metal tubes); — Types of welding and welding joints; — General characteristics of aircraft coverings; — General characteristics of paint; — Transmission of loads in and between structures. 4L.2 Materials 2 — Types of wood (solid wood, laminated wood, plywood, wood composites), suitable wood materials and their properties (spruce, firs, etc.), wood defects (acceptable / not acceptable), stability, deterioration (temperature, humidity, ageing, etc.); — Types of covering and technologies (natural and synthetic polymers), deterioration; — Types of glues, adhesives, paints and other associated materials; — Types of metal-tubing material (steel, light alloy tubes, etc.); — Welding seams, fittings, screws and bolts (material and properties);

text: — Proper storage of those materials; — Plastics (overview and understanding of their properties). 4L.3 Identifying damages and defects 3 — Inspection procedures; — Damage identification in wooden structures (heavy landing, rot, glue failure, fungi, shrinkage, stress damage, cracks, fatigue, etc.); — Damage identification in metal-tube structures (hard landing, stress, corrosion, fatigue, dents, cracks, fatigue, etc.); — Damage identification in welded seams; — Damage identification in fabric coverings (tears, strains, UV damage, hard landing, etc.). 4L.4 Standard repair and maintenance procedures 3 — Repair and conservation of wooden aircraft structures: wing rib, wing spar, bolt and brushing holes, patches (fabric, splayed, surface, plug, scarf); — Repair and reapplication of fabric on aircraft (fabric, tape, lacing, threads, seams, fabric protection, stitching, knots, fasteners, finishing tape, rings and grommets, dope); — Repair and corrosion protection/prevention methods for metal-tube aircraft structures (welding, patch plates, reinforcement tubes, sleeves, etc.); — Repair, removal and application of paint and dope on airframes in wooden / combination of metal tube and fabric (surface preparation, application and finish).

text: MODULE 5L — COMPOSITE STRUCTURE

text: MODULE 5L — COMPOSITE STRUCTURE Level

text: 5L.1 Airframe fibre-reinforced plastic (FRP) 2 — General construction principles of airframes in FRP and its properties; — Characteristics of laminated structures (matrix and fibres); — Fibre (fibre orientation, strength characteristics, isotropic, anisotropic, filament, strands, tows, yarns, rovings, impreg and prepreg); — Fabric weave styles (plain weave, twill weave, atlas weave, unidirectional) and non-woven material (stitched and knotted) and their characteristics; — Matrix (thermosetting, thermoplastic, curing stages); — Characteristics of sandwich structures and their supporting cores (honeycombs, foams, wooden cores, pseudo-cores); — General characteristics of accelerators and additives/modifiers; — Transmission of loads in and between structures. 5L.2 Materials 2 — Types of fibres (fibreglass, E-glass, aramid, carbon/graphite, boron, ceramic, lightning protection fibre); — Types of matrices (different types, properties and application); — Types of resin filler materials (fumed silica, glass powder, hollow glass, phenolic and plastic microballoons, cotton, flox, colour pigments, fire retardants); — Types of sandwich structure core materials (honeycombs: aramid paper, kraft paper, thermoplastic, aluminium, fibreglass, carbon; foams: polystyrene, phenolic, polyurethane, polypropylene, PVC, polymethacylimide; balsa wood); — Behaviour, interaction, and technological aspects of composites made of those materials;

text: MODULE 5L — COMPOSITE STRUCTURE Level

text: — Storage and handling of those materials. 5L.3 Identifying damages and defects 3 — Inspection procedures (visual inspection, tapping, NDT testing, etc.); — Types of manufacturing defects and damages and their causes (fibre breakage, matrix imperfections, delamination, debonding, improper drilling, environmental degradation, impact damage, fatigue, erosion, corrosion, UV damage, hard landing, stress, etc.). 5L.4 Standard repair and maintenance procedures 3 — Repairs of aircraft structures: wing, rib, wing spar, aerofoil, bolt and brushing holes, patches, sandwich core and faceplate repairs, bolted and bonded repairs; — Proper construction and repair fittings, and load-bearing points for composites and composite sandwich structures; — Creation and use of repair moulds from the airframe or intact parts (types, procedures, coatings, etc.); — Proper procedure for the mixing of resins, fibre layering and curing of composites; — Bonding metals and other materials; — Composite painting and finish.

text: MODULE 6L — METALLIC STRUCTURE

text: MODULE 6L — METALLIC STRUCTURE Level

text: 6L.1 Metallic airframe 2 — General construction principles for metal-structure airframes; — General knowledge of the properties of metal as a technical material (classification; physical, mechanical and electrical properties; manufacturing properties; chemical properties); — General knowledge of the properties of pure metals and alloys; — Metal grain structure of pure metals and alloys and its impact on behaviour (grain boundaries; corrosion; hardening; annealing; differences between forged, machined and cast metals); — Stresses in structural members (tension, compression, torsion, shearing, bearing, bending); — Types of corrosion and corrosion protection (electrochemical oxidation, galvanic corrosion, stress-corrosion cracking, corrosion in passivated materials, high-temperature corrosion); — Types of rivets and fasteners (solid shank rivet, blind rivets, self-plugging rivets (mechanical and friction lock), pull-thru rivets, pin rivets, head styles, taper-lok, rivet nut, lockbolt, high shear fastener, identification, measuring); — Types of welding and welding joints; — Transmission of loads in and between structures. 6L.2 Materials 2 — Types of iron and steel, and their alloys in aviation (cast, forged, tempering, corrosion, strength properties); — Types of aluminium and aluminium alloys in aviation in airframes, rivets, and fasteners (strength properties, corrosion); — Common alloying elements for steel and aluminium (influence on the mechanical and physical properties of the alloy); — Common paint and surface protection materials;

text: MODULE 6L — METALLIC STRUCTURE Level

text: — Common adhesives for use with metals. 6L.3 Identifying damages and defects 3 — Inspection procedures (sheet metal, structure, bonded joints, soldered joints, welded and brazed joints, riveted joints, corrosion); — Identification and classification of cracks, fatigue, and corrosion in metallic structures. 6L.4 Standard repair and maintenance procedures 3 — Metal and sheet metal (marking out and calculation of bend allowance, cutting, drilling, bending and forming, inspection of metal work); — Welding, brazing, soldering and bonding (soldering methods, welding and brazing methods, bonding methods); — Riveting (riveted joints, rivet spacing and pitch; tools used for riveting and dimpling; inspection of riveted joints); — Repairing by patching, insertion, and replacement of parts; — Corrosion treatment; — Problems in multiple-material systems.

text: MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

text: MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS Level

text: 7L.1 Theory of flight — gliders and aeroplanes 1 Aerodynamics and flight controls: — Airflow around a body; — Boundary layer, laminar and turbulent flow; — Thrust, weight, aerodynamic resultant; — Generation of lift and drag angle of attack, polar curve, stall. Operation and effect of roll control, pitch control, yaw control and rudder limiters: — Control using dual-purpose controls; — High-lift devices, slots, slats, flaps, flaperons; — Drag-inducing devices, lift dumpers, speed brakes, dive brakes; — Effects of wing fences, saw tooth leading edges; — Boundary layer control using vortex generators, stall wedges or leading-edge devices; — Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels. 7L.2 Airframe structure — gliders and aeroplanes 1 — Fuselage: construction (truss type, monocoque, semimonocoque), attach points (wing, tail plane, undercarriage); — Wings: construction (monospar, multispar, box beam), configurations (cantilever, semicantilever, strut/wire braced), fairing; — Stabilisers: construction, control surface attachments; — Flight control surfaces: construction and attachment, balancing (mass and aerodynamics); — Tow hooks (Schweizer and Tost hook); — Aircraft assembly, storage, jacking, chocking, securing and associated safety precautions; — Effects of environmental conditions on aircraft handling and operation. 7L.3 Air conditioning (ATA 21) 1

text: Heating and ventilation for small aircraft. 7L.4 Electrical power, cables, and connectors (ATA 24) 2 — Installation and operation of batteries; — Power generation / power sources (AC/DC) on small aircraft, voltage regulation, power distribution and circuit protection; — Cable types, construction and characteristics, high-tension and coaxial cables, testing and installation precautions; — Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes, pin insertion and removal; — Crimping (crimping, tools, testing of crimp joints); — Continuity, insulation and bonding techniques and testing; — Wiring protection techniques (cable looming and loom support, cable clamps, protective sleeving techniques (including heat shrink wrapping), shielding). 7L.5 Equipment and furnishing (ATA 25) 2 — Emergency equipment requirements; — Seats, harnesses, and belts. 7L.6 Fire protection and other safety systems (ATA 26) 2 — Portable fire extinguisher; — Rescue systems (safety parachute, recovery parachute, launching systems, including safety measures for pyrotechnics). 7L.7 Flight controls (ATA 27) 3 — Primary controls: aileron, elevator/stabilator, rudder, dual-purpose controls (stabilator, ruddervator, flaperons); — Secondary controls: elevator trim systems, wing flaps, slats and spoilers / dive breaks; — System operation: manual; — Gust locks, balancing and rigging of flight controls; — Simple stall-warning systems. 7L.8 Fuel system (ATA 28) 2 — System layout; — Fuel tanks; — Supply systems; — Indications and warnings; — Refuelling and defuelling. 7L.9 Hydraulic power (ATA 29) 2 — System layout; — Hydraulic fluids; — Hydraulic reservoirs and accumulators, pressure generation (electric, mechanical), filters, pressure control, power distribution, indication and warning systems. 7L.10 Ice and rain protection (ATA 30) 1 — Hydrophobic coatings; — Pitot probe heating. 7L.11 Landing gear (ATA 32) 2 — Construction (tricycle, tailwheel, outrigger wheels, skids), shock absorbing;

text: — Extension and retraction systems: normal and emergency operation; — Indications and warnings; — Wheels, brakes, tyres, and steering; — Standard repair and maintenance procedures for the landing gear. 7L.12 Lights (ATA 33) 2 — External lights: navigation, anticollision, landing, taxiing; — Internal lights: cockpit. 7L.13 Oxygen (ATA 35) 2 — System layout: storage system (containers), delivery system (continuous flow, diluter demand and pressure demand) and masks/nasal cannula; — System operation, including charging and discharging; — The ‘PRICE’ check. 7L.14 Pneumatic/vacuum (ATA 36) 2 — System layout; — Sources, pumps, control and distribution; — Indication and warnings. 7L.15 Water ballast (ATA 41) 2 Water tanks (main tank, fin tank), drain valves, vents. 7L.16 Fasteners 2 — Screw threads: nomenclature, forms, dimensions and tolerances, and measuring; — Bolts, studs and screws: types (specifications, identification, markings, international standards), nuts (self-locking, anchor, standard types), machine screws (aircraft specifications), studs (types and uses, insertion and removal), self-tapping screws, dowels; — Locking devices: tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quickrelease fasteners, keys, circlips, cotter pins; — Aircraft rivets: types of solid and blind rivets: specifications and identification, heat treatment. 7L.17 Pipes, hoses, and connectors 2 — Types and connectors of pipes and hoses for hydraulic, fuel, oil, pneumatic and air; — Bending, belling/flaring, inspection, testing and installation of pipes and hoses. 7L.18 Springs 2 Types of springs, materials, characteristics, applications, inspection, and testing. 7L.19 Bearings 2 — Purpose of bearings, loads, material, construction; — Types of bearings, their application, testing, cleaning, inspection, lubrication requirements, and common defects in bearings and their causes. 7L.20 Transmission 2 — Gear types, their application, gear ratios, reduction and multiplication gear systems, driven and driving gears, idler gears, mesh patterns, inspection of gears, backlash/play; — Types, application and inspection of belts and pulleys, chains and sprockets; — Inspection of screw jacks, lever devices, push–pull rod systems. 7L.21 Control cables 2

text: — Types of cables, end fittings, turnbuckles, compensation devices, pulleys, cable system components, Bowden cables and aircraft flexible control systems; — Swaging of end fittings; — Inspection and testing of control cables, Bowden cables, and aircraft flexible control systems. 7L.22 Fits and clearances 2 Common system of fits, clearances and tolerances, drill sizes for bolt holes, classes of fits, schedule of fits and clearances for aircraft and engines, limits for bow, twist and wear, standard methods for checking shafts, bearings and other parts. 7L.23 Aircraft weight and balance 2 Calculation of centre-of-gravity / balance limits: use of relevant documents, preparation of aircraft for weighing, aircraft weighing. 7L.24 Workshop practices and tools 2 — Common hand-tool types, power-tool types, precision tool types and equipment, their operation, care, control, calibration, and standards; — Operation, function and use of electrical general test equipment; — Proper handling of engineering drawings, diagrams and standards, and comprehension of the information presented thereupon (symbols, schematics and diagrams); — Use of workshop materials; — Dimensions, allowances and tolerances, standards of workmanship; — Lubrication equipment and methods. 7L.25 Disassembly, inspection, repair, and assembly techniques 2 — Types of defects and visual inspection techniques; corrosion removal, assessment and reprotection; — General repair methods, structural repair manual; ageing, fatigue and corrosion control programmes; — Non-destructive inspection techniques, including penetrant, radiographic, eddy current, ultrasonic and borescope methods; — Disassembly and reassembly techniques; — Troubleshooting techniques. 7L.26 Abnormal events 2 Inspection following lightning strike, HIRF penetration, heavy landing, and flight through turbulence. 7L.27 Maintenance procedures 2 Maintenance planning, modification procedures, stores procedures, maintenance inspection / quality control / quality assurance, additional maintenance procedures, control of life-limited components.

text: MODULE 8L — POWER PLANT

text: MODULE 8L — POWER PLANT Level

text: 8L.1 Engine fundamentals — general 2 — Potential energy, kinetic energy, Newton’s laws of motion, Brayton cycle; — The relationship between force, work, power, energy, velocity, and acceleration; — Mechanical, thermal, and volumetric efficiencies. 8L.2 Piston-engine fundamentals and performance 2 — Operating principles: 2-stroke, 4-stroke, Otto, Diesel, and Rotary (Wankel); — Piston displacement and compression ratio; — Engine configuration and firing order; — Power calculation and measurement; — Factors that affect engine power; — Mixtures/leaning, pre-ignition. 8L.3 Piston-engine construction 2 — Crank case, crank shaft, cam shafts, sumps; — Accessory gearbox; — Cylinder and piston assemblies; — Connecting rods, inlet and exhaust manifolds; — Valve mechanisms; — Propeller reduction gearboxes. 8L.4 Piston-engine fuel system (non-electronic) 2 — Carburettors (types, construction and principles of operation, icing and heating); — Fuel injection systems (types, construction, and principles of operation). 8L.5 Starting and ignition systems 2 — Starting systems, preheat systems; — Magneto types, construction, and principles of operation; — Ignition harnesses, spark plugs; — Low- and high-tension systems. 8L.6 Air-intake, exhaust, and cooling systems 2 — Construction and operation of induction systems, including alternate air systems; — Exhaust systems, engine cooling systems — air and liquid. 8L.7 Supercharging/turbocharging 2 — Principles and purpose of supercharging and its effects on engine parameters; — Construction and operation of supercharging/turbocharging systems; — System-associated terminology; — Control systems; — System protection. 8L.8 Lubrication systems of piston engines 2 System operation/layout and components.

text: MODULE 8L — POWER PLANT Level

text: 8L.9 Engine indication systems 2 — Indication systems specific to general combustion engines (coolant temperature, oil pressure and temperature, exhaust gas temperature, fuel pressure and flow); — Indication systems specific to piston engines (cylinder head temperature, manifold pressure, engine speed); — Indication systems specific to turbine engines (exhaust gas temperature, engine thrust indication, engine speed); — Indication systems specific to electric engines (voltage). 8L.10 Electric aircraft engines 2 — Types and construction of electric motors (AC and DC motors, rotor, stator, bearings, windings, commutator, self-commutated, externally commutated, outrunner and inrunner, motor cooling, etc.); — Power electronics; — Transformer, transducer, and inverter; — Engine control systems; — Power storage systems (common high-density batteries, chemistry batteries, load cycles, degradation, effects of charging and overcharging, thermal runaway); — Battery management systems (general functions, battery balancing, monitoring); — Wiring of electric power storage, power electronics, and electric motor; — High-energy safety procedures. 8L.11 Turbine-engine fundamentals and performance 2 — Constructional arrangement and operation of turbojet and turboprop engines; — Thrust: thrust horsepower, shaft horsepower, specific fuel consumption; — Engine pressure ratio; — Pressure, temperature, and velocity of gas flow; — Engine ratings, static thrust, limitations. 8L.12 Inlet and compressor 2 — Compressor inlet; — Axial and centrifugal compressor types, constructional features, operating principles and applications; — Compressor (stator, rotor, blisk, disk, blades, compressor stall and surge); — Compressor ratio. 8L.13 Combustion chamber, starting and ignition system 2 — Constructional features and principles of operation; — Operation of engine start systems and components; — Ignition systems and components (exciter, ignition plugs and glow plugs). 8L.14 Turbine section and exhaust 2 — Operation and characteristics of different turbine blade types, nozzle guide vanes; — Gas producer turbine and power turbine, blade-to-disk attachment; — Causes and effects of turbine blade stress and creep; — Engine exhaust nozzle and noise reduction.

text: MODULE 8L — POWER PLANT Level

text: 8L.15 Other turbine-engine components and systems 2 — General knowledge of the type features and principles of bearings and seals in turbine engines; — System operation, layout and components of lubrication systems in small turbine engines (separate lubrication, as part of the fuel system); — System operation, layout and components of air and fuel systems in small turbine engines; — Turboprop reduction gears. 8L.16 Turbine-engine inspection and ground operation 2 — Standard procedures for starting and ground run-up and interpretation of engine power output and parameters; — Inspection of engine and components to criteria, tolerances and data specified by the engine manufacturer; — Foreign object damage (FOD). 8L.17 Propeller 2 — Propeller fundamentals (blade element theory, blade angles, angle of attack, rotational speed, propeller slip, aerodynamic/centrifugal/thrust forces, torque, relative airflow, vibration and resonance); — Propeller construction (methods of construction and materials used in wooden/composite/metal propellers, blade station, blade face, blade shank, blade back/thrust face and hub assembly, fixed pitch, controllable pitch, constant speed propeller, propeller/spinner installation); — Propeller pitch control (speed control and mechanical/electrical pitch change methods, feathering, propeller accumulators, overspeed protection); — Environmental protection (de-icing and metal tipping); — Propeller balancing (static and dynamic) and blade tracking; — Damage assessment, erosion, corrosion, impact damage, delamination and decay; — Standard treatment and repair methods for propellers. 8L.18 Full authority digital engine control (FADEC) 2 — Operation of engine control and fuel-metering systems in piston and turbine engines, including electronic engine control (FADEC); — System layout and components. 8L.19 Lubricants and fuels 2 — Properties and specifications of standard, alternate and drop-in fuels, fuel additives, and lubricants. 8L.20 Engine and propeller installation 2 — Construction of nacelles; — Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains; — Extension and retraction systems, including propeller position control; — Propeller installation.

text: MODULE 8L — POWER PLANT Level

text: 8L.21 Engine monitoring and ground operation 2 — Procedures for starting and ground run-up; — Interpretation of engine power output and parameters; — Inspection of engine and components to criteria, tolerances and data specified by the engine manufacturer; — Foreign object damage (FOD). 8L.22 Engine/propeller storage and preservation 2 — Preservation and depreservation of the engine, the propeller, and accessories/systems.

text: MODULE 9L — BALLOONS: HOT-AIR BALLOONS

text: MODULE 9L — BALLOONS: HOT-AIR BALLOONS Level

text: 9L.1 Theory of flight — hot-air balloons 1 — Aerostatics and controls; — Principles; — Effect on envelopes, wind effect, altitude, and temperature effects. 9L.2 General airframe of hot-air balloons 2 Components and assembly of a hot-air balloon: — Identification plate; — Envelope; — Heater system / burner; — Suspension cables; — Basket; — Lines and ropes (crown line, actuationline). 9L.3 Envelope 3 — Shape and assembly of envelope (poles, equator, panels, gores, special shapes); — Fabrics, seams, and materials; — Crown ring; — Deflation port/parachute and ripping panel; — Load tapes (horizontal and vertical) and rip stoppers; — Turning vent; — Mouth; — Skirt/scoop; — Diaphragms/catenaries (special shapes). 9L.4 Heater system / burner 3 — System layout (burner, fuel tanks, fuel lines); — Types of burners (whisper-/cow-burner, main/take-off burner); — Functionality, materials, use, inspection, and care of: — fuel tanks (propane cylinders, material, valves, fittings, fuel quantity gauge), — fuel lines / gas hoses, — burner (piezo igniter, pilot light and valve, blast valve, heat exchanger / burner coils, nozzle, etc.).

text: 9L.5 Basket and basket suspension (including alternative devices) 3 — Common assembly of and materials for hot-air balloon baskets; — Rigging points, burner frame, burner support rods, metal frame, basket padding and leather trim; — Basket weave, grab handles, cylinder attachment, take-off aid and rope; — Basket wire and basket wire routing; — Basket floor, basket frame / load-bearing frame, sliders, rawhide protective covering. 9L.6 Instruments 2 Basic operation, maintenance, and testing of: — altimeter (mechanical and electronic); — variometer (mechanical and electronic); — pyrometer / temperature sensors; — Mode S transponder; — VHF radio; — Emergency locator transmitter (ELT) and personal locator beacon (PLB). 9L.7 Equipment 2 — Required equipment for free-ballooning operation and its care. 9L.8 Hot-air balloon handling and storage 2 — Ground procedures for hot-air balloons, rigging and launch preparation; — Safe handling of propane; — Effects of environmental conditions on hot-air balloon handling. 9L.9 Disassembly, inspection, repair, and assembly techniques 3 — Types of defects and visual inspection techniques; — Allowable damage to and tolerance of envelope, basket, lines, ropes, etc.; — Common test procedures (grab test); — General repair methods for envelopes, load ring, ropes and lines, basket; — Inspection methods for envelopes, ropes and lines, basket; — Ageing, fatigue; — Disassembly and reassembly techniques; — Troubleshooting techniques.

text: MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS

text: MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS Level

text: 10L.1 Theory of flight — gas balloons 1 Aerostatics and controls: — Principles; — Effect on envelopes, wind effect, altitude, and temperature effects. 10L.2 General airframe of gas balloons 2 Components and assembly of a gas balloon: — Identification plate; — Envelope;

text: — Valve; — Netting; — Load ring (hoop); — Basket; — Lines and ropes (drag rope, mooring line, valve line, emergency opening rope, ripping line, neckline). 10L.3 Envelope 3 — Shape and assembly of envelope (poles, equator, panels); — Fabrics, seams, and materials; — Deflation opening and parachute; — Load belt; — Ripping panel; — Appendix; — Emergency opening; — Holding-down patches; — Ballonets; — Electrostatic properties. 10L.4 Netting 3 — Netting assembly (net ring, net, mesh); — Mesh dimensions (knots, sizes, angles); — Materials for netting and accessories; — Electrostatic properties. 10L.5 Valves, parachutes, and other related systems 3 — Construction, operation, maintenance and testing of manoeuvring/helium valves, pressure relief valves, gas-tight parachutes, and ballonet fans; — Construction, operation, maintenance and testing of parachute-centring belt and pull-down belts. 10L.6 Load ring 3 — Function, material, and common problems (steel pipe, strops, toggles). 10L.7 Basket (including alternative devices) 3 Common assembly of and materials for hot-air/gas balloon baskets: — Metal frame, basket padding and leather trim; — Basket weave, grab handles, basket strops and toggles, ballast system (bags, support and sand dumpers); — Basket wire and basket wire routing; — Basket floor, basket frame / load-bearing frame, sliders, rawhide protective covering. 10L.8 Ropes and lines 3 Functionality, materials, use, inspection, and care of: — Shroud lines / envelope ropes / bridles; — Trail rope /drag rope and trail-rope bag; — Holding ropes; — Valve line/ valve cord and parachute rope; — Emergency opening rope;

text: — Appendix pull-close rope; — Appendix anchor line; — Inflation aid. 10L.9 Instruments 2 Basic operation, maintenance, and testing of: — Altimeter (mechanical and electronic); — Variometer (mechanical and electronic); — Mode-S transponder; — VHF radio; — Emergency locator transmitter (ELT) and personal locator beacon (PLB). 10L.10 Tethered gas balloon (TGB) systems 3 Functionality, operation, materials, use, inspection, and care of: — Launch platform; — Winch system: winch (electric, hydraulic, emergency operation), tether cable (cable, sheaves, swivel, clamps), and control panel; — Gondola (metal-tubing construction); — Night lighting. 10L.11 Equipment 2 — Required equipment for free-ballooning and for tethered operations, and its care. 10L.12 Gas-balloon handling and storage 2 — Ground procedures and mooring for gas balloons and tethered gas balloons, ballasting, rigging and launch preparation; — Safe handling of hydrogen, helium, illuminating gas, and other lifting gases; — Lifting gas (charging, purifying and leak testing, pressure monitoring); — Effects of environmental conditions on gas-balloon handling. 10L.13 Disassembly, inspection, repair, and assembly techniques 3 — Types of defects and visual inspection techniques; — Allowable damage to and tolerance of envelope, basket, lines, ropes, etc.; — Common test procedures (grab test, tensile strength, tear growth, porosity, electric resistivity, etc.); — General repair methods for envelopes, load ring, ropes and lines, basket/gondola; — Inspection methods for envelopes, load ring, ropes and lines, basket/gondola (especially for steel frames and welds on TGB gondolas); — Ageing, fatigue and corrosion control programmes; — Disassembly and reassembly techniques; — Troubleshooting techniques.

text: MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS

text: MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS Level

text: 11L.1 Theory of flight and control of airships 2 — Control using fins, rudders and elevators; — Aerodynamic lift and aerodynamic balance;

text: — Stability and control; — Free ballooning; — Operation of trim tabs, balance and antibalance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels; — Vectored thrust; — Fire and lightning protection. 11L.2 Airship airframe structure — general concepts 2 — Classification of airships (rigid airship, semi-rigid airship, non-rigid airship); — Construction of semi-rigid airships (envelope, ballonet, membranes, nose cone, internal structures, keel, trusses, longerons, suspension lines); — Construction of non-rigid airships (envelope, ballonet, catenary curtains, suspension lines, air scoops); — Attachment of stabilisers and control surfaces to the airframe. 11L.3 Airship envelope 2 — Nose cone battens / bow strips; — Catenary systems (catenary curtain, support/suspension cables); — Ballonets and their positioning (forward, aft); — Air systems (air scoops, ballonet fans, empennage air system, dampers and transfer fans). 11L.4 Gondola 3 — General knowledge of gondola construction (metal-tubing gondolas, metal-structure gondolas, composite gondolas); — Doors, windows, and hatches; — Attachment of the gondola to the airframe/envelope; — Gondola layout, equipment and furnishing (emergency equipment requirements, seats, harnesses and belts); — Simple water/waste systems in airships; — Gondola heating and ventilation (ventilations and heating systems, heat exchanger, blower); — Landing gear (construction, shock absorbing, tyres, weight-on-wheels). 11L.5 Airship flight controls (ATA 27/55) 3 — Primary controls (rudder, elevator, asymmetric thrust, thrust vectoring); — Trim control; — System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire; — Balancing and rigging. 11L.6 Electrical power (ATA 24) 3 — Installation and operation of batteries; — DC power generation; — AC power generation; — Voltage regulation; — Power distribution; — Wiring, electrical connections; — Inverters, transformers, rectifiers; — Circuit protection; — External/ground power.

text: 11L.7 Lights (ATA 33) 2 — External: navigation, anticollision, landing, taxiing, ground approach light, aft landing light; — Internal: flight compartment (cockpit) and passenger compartment (cabin); — Emergency. 11L.8 Ice and rain protection 3 — Windscreen wipers and windscreen de-misting systems; — Surface de-icing systems. 11L.9 Fuel systems (ATA 28) 2 — System layout; — Fuel tanks: venting, draining; — Supply systems; — Cross-feed and transfer; — Indications and warnings; — Refuelling and defuelling. 11L.10 Engine and propellers in airships 2 — General understanding of engine layout, thrust vectoring, swivel systems, ducted propellers and control system. 11L.11 Airship handling and storage 2 — Ground procedures and mooring with and without mooring mast, ballasting, hangaring, rigging and launch preparation; — Lifting gas (charging, purifying and leak testing, pressure monitoring); — Effects of environmental conditions on airship handling. 11L.12 Disassembly, inspection, repair, and assembly techniques 2 — Types of defects and visual inspection techniques; — Corrosion removal, assessment and reprotection; — General repair methods, structural repair manual; — Ageing, fatigue and corrosion control programmes; — Non-destructive inspection techniques; — Disassembly and reassembly techniques; — Troubleshooting techniques.

text: MODULE 12L — RADIO COM / ELTs / TRANSPONDERS / INSTRUMENTS

text: MODULE 12L — RADIO COM / ELTs / TRANSPONDERS / INSTRUMENTS Level

text: 12L.1 Radio COM / ELTs 2 Fundamentals of radio-wave propagation, antennas, transmission lines, communication, receiver, and transmitter. Working principle of: — Emergency locator transmitters (ELTs); — Very-high-frequency (VHF) communications; — installation and testing of ELTs and VHF radio and antennas. 12L.2 Transponder and FLARM 2

text: — Air traffic control transponder, secondary surveillance radar (basic operation, configuration, modes); — FLARM; — Installation and testing. 12L.3 Instruments 2 — Pitot-static: altimeter, airspeed indicator, vertical speed indicator, total energy probes; — Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator; — Compasses: direct reading, remote reading; — Angle-of-attack indication, stall-warning systems; — Glass and analogue cockpit; — Indications of other aircraft systems; — Installation and testing of instruments. 12L.4 Avionics general test equipment 1 — Operation, function, and use of general test equipment for avionics.

text: AMC1 Appendix VIII — Basic examination standard for category L aircraft maintenance licence

text: NUMBER OF QUESTIONS PER SUBMODULE The tables below show the number of questions recommended for each submodule. Justified deviations from these values are also acceptable, provided that the sum of the questions for the submodules equals the total number for a given module. MODULE 1L — BASIC KNOWLEDGE

text: Nr of questions MODULE 1L — BASIC KNOWLEDGE

text: 20 1L.1 Mathematics 4 1L.2 Physics 5 1L.3 Electrics 4 1L.4 Aerodynamics/aerostatics 2 1L.5 Workplace safety and environmental protection 5

text: MODULE 2L — HUMAN FACTORS

text: Nr of questions MODULE 2L — HUMAN FACTORS

text: 20 2L.1 General 3 2L.2 Human performance and limitations 2 2L.3 Social psychology 2 2L.4 Factors that affect performance 4 2L.5 Physical environment 4 2L.6 The ‘Dirty Dozen’ and risk-mitigation 5

text: MODULE 3L — AVIATION LEGISLATION

text: Nr of questions MODULE 3L — AVIATION LEGISLATION

text: 28 3L.1 Regulatory framework 4 3L.2 Continuing airworthiness regulations 6 3L.3 Repairs and modifications (Part-ML) 5 3L.4 Maintenance data (Part-ML) 5 3L.5 Licence privileges and how to exercise them properly (Part-66, Part-ML) 8

text: Nr of questions MODULE 4L — WOODEN AND/OR METAL-TUBE STRUCTURE COVERED WITH FABRIC

text: 40 4L.1 Combined structures made of wood, metal tube and fabric 8 4L.2 Materials 8

text: 40 4L.3 Identifying damages and defects 12 4L.4 Standard repair and maintenance procedures 12

text: MODULE 5L — COMPOSITE STRUCTURE

text: Nr of questions MODULE 5L — COMPOSITE STRUCTURE

text: 32 5L.1 Fibre-reinforced plastic (FRP) airframe 6 5L.2 Materials 6 5L.3 Identifying damages and defects 10 5L.4 Standard repair and maintenance procedures 10

text: MODULE 6L — METALLIC STRUCTURE

text: Nr of questions MODULE 6L — METALLIC STRUCTURE

text: 32 6L.1 Metallic airframe 6 6L.2 Materials 6 6L.3 Identifying damages and defects 10 6L.4 Standard repair and maintenance procedures 10

text: Nr of questions MODULE 7L — AIRFRAME: GENERAL, MECHANICAL AND ELECTRICAL SYSTEMS

text: 60 7L.1 Theory of Flight — gliders and aeroplanes 4 7L.2 Airframe Structure — gliders and aeroplanes 4 7L.3 Air conditioning (ATA 21) 1 7L.4 Electrical power, cables, and connectors (ATA 24) 3 7L.5 Equipment and furnishing (ATA 25) 2 7L.6 Fire protection and other safety systems (ATA 26) 2 7L.7 Flight controls (ATA 27) 3 7L.8 Fuel system (ATA 28) 2 7L.9 Hydraulic power (ATA 29) 2 7L.10 Ice and rain protection (ATA 30) 1 7L.11 Landing gear (ATA 32) 3 7L.12 Lights (ATA 33) 1 7L.13 Oxygen (ATA 35) 1 7L.14 Pneumatic/vacuum (ATA 36) 1 7L.15 Water ballast (ATA 41) 1 7L.16 Fasteners 2 7L.17 Pipes, hoses, and connectors 2 7L.18 Springs 1 7L.19 Bearings 1

text: 60 7L.20 Transmissions 2 7L.21 Control cables 3 7L.22 Fits and clearances 1 7L.23 Aircraft weight and balance 2 7L.24 Workshop practices and tools 4 7L.25 Disassembly, inspection, repair, and assembly techniques 4 7L.26 Abnormal events 3 7L.27 Maintenance procedures 4

text: MODULE 8L — POWER PLANT

text: Nr of questions MODULE 8L — POWER PLANT

text: 64 8L.1 Engine fundamentals — general 2 8L.2 Piston-engine fundamentals and performance 2 8L.3 Piston-engine construction 3 8L.4 Piston-engine fuel system (non-electronic) 2 8L.5 Starting and ignition systems 3 8L.6 Air intake, exhaust, and cooling systems 2 8L.7 Supercharging/turbocharging 2 8L.8 Lubrication systems of piston engines 2 8L.9 Engine indication systems 3 8L.10 Electric and hybrid aircraft engines 9 8L.11 Turbine-engine fundamentals and performance 2 8L.12 Inlet and compressor 2 8L.13 Combustion chamber, starting and ignition system 2 8L.14 Turbine section and exhaust 2 8L.15 Other turbine-engine components and systems 2 8L.16 Turbine-engine inspections and ground operation 3 8L.17 Propeller 7 8L.18 Full authority digital engine control (FADEC) 2 8L.19 Lubricants and fuels 3 8L.20 Engine and propeller installation 4 8L.21 Engine monitoring and ground operation 3 8L.22 Engine/propeller storage and preservation 2

text: Note: In accordance with Appendix VII ‘1. Modularisation’ to Annex III, Module 8L training subjects for L5 category AML and, therefore, the number of questions, should be limited to the relevant propulsion

text: system. As such, in the above table, certain submodules may not be applicable and should not be taken into account, and the total number of questions should also be adapted accordingly.

text: MODULE 9L — BALLOONS: HOT-AIR BALLOONS

text: Nr of questions MODULE 9L — BALLOONS: HOT-AIR BALLOONS

text: 36 9L.1 Theory of flight — hot-air balloons 2 9L.2 Airframe of hot-air balloons 3 9L.3 Envelope 4 9L.4 Heater system / burner 4 9L.5 Basket and basket suspension (including alternative devices) 4 9L.6 Instruments 5 9L.7 Equipment 2 9L.8 Hot-air balloon handling and storage 4 9L.9 Disassembly, inspection, repair, and assembly techniques 8

text: Nr of questions MODULE 10L — BALLOONS: GAS (FREE/TETHERED) BALLOONS 44

text: 10L.1 Theory of flight of gas balloons 2 10L.2 Airframe of gas balloons 3 10L.3 Envelope 3 10L.4 Netting 1 10L.5 Valves, parachutes, and other related systems 1 10L.6 Load ring 1 10L.7 Basket (including alternative devices) 4 10L.8 Ropes and lines 2 10L.9 Instruments 5 10L.10 Tethered gas balloon (TGB) systems 8 10L.11 Equipment 2 10L.12 Gas-balloon handling and storage 4 10L.13 Disassembly, inspection, repair, and assembly techniques 8

text: Nr of questions MODULE 11L — AIRSHIPS: HOT-AIR/GAS AIRSHIPS 40

text: 11L.1 Theory of flight and control of airships 3 11L.2 Airship airframe structure — general concepts 3 11L.3 Airship envelope 3 11L.4 Gondola 6 11L.5 Airship flight controls (ATA 27/55) 2 11L.6 Electrical power (ATA 24) 3 11L.7 Lights (ATA 33) 1 11L.8 Ice and rain protection 2 11L.9 Fuel systems (ATA 28) 3 11L.10 Engines and propellers in airships 2 11L.11 Airship handling and storage 4 11L.12 Disassembly, inspection, repair, and assembly techniques 8

text: Nr of questions MODULE 12L — RADIO COM / ELTs / TRANSPONDER / INSTRUMENTS 20

text: 12L.1 Radio COM / ELTs 6 12L.2 Transponder and FLARM 5 12L.3 Instruments 8 12L.4 Avionics general test equipment 1

text: APPENDICES TO AMC TO ANNEX III (PART-66) Appendix I to AMC to Annex III — Aircraft type ratings for Part-66 aircraft maintenance licences

text: […] GROUP 1 AEROPLANES

text: GROUP 1 AEROPLANES

text: TC Holder Model Com. des. Part-66 type rating endorsement Note […] […] […] […] […] Airbus A319/A320/A321 (CFM LEAP- TC not yet AIRBUS A319-152N A319 NEO 1A) released A319-171N A319 NEO Airbus A319/A320/A321 (IAE TC not yet

text: AIRBUS

text: PW1100G) released

text: GROUP 1 AEROPLANES

text: A330-743L Beluga XL Airbus A330 (RR Trent 700) TC not yet

text: AIRBUS

text: released

text: A330-841 A330 NEO Airbus A330 (RR Trent 7000) TC not yet

text: AIRBUS

text: released

text: BOEING 737-8200 B737 MAX Boeing 737-7/8/9 (CFM LEAP-1B) TC not yet

text: COMPANY (THE) released

text: Canadair CL-215 (PWC PW120

text: BOMBARDIER (CL-215T

text: Variant)

text: DASSAULT Falcon 6X Falcon 6X Falcon 6X (PW812D) OSD

text: AVIATION mandatory.

text: GULFSTREAM OSD GVII-G500 G500 Gulfstream GVII (PWC PW800GA) AEROSPACE mandatory.

text: Corporation

text: Not yet

text: GULFSTREAM

text: GVII-G600 Gulfstream GVII (PWC PW800GA) certified. AEROSPACE G600 OSD

text: Corporation

text: mandatory.

text: GULFSTREAM GVIII-2 Gulfstream GVIII-2 (RR BR700) Not yet

text: AEROSPACE certified.

text: Corporation OSD

text: mandatory.

text: TEXTRON Citation Cessna 700 (Honeywell HTF7000) 700 AVIATION Inc. Longitude

text: TEXTRON Businessliner 402C Cessna 400 Series (Continental) AVIATION Inc. Utiliner

text: TEXTRON

text: 414A Chancellor Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 421B Golden Eagle Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 421C Golden Eagle Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 404 Titan Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 401 Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 402 Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 411 Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 414 Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 421 Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 401A Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 401B Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 402A Cessna 400 Series (Continental)

text: AVIATION Inc.

text: GROUP 1 AEROPLANES TEXTRON

text: 402B Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 411A Cessna 400 Series (Continental)

text: AVIATION Inc. TEXTRON

text: 421A Cessna 400 Series (Continental)

text: AVIATION Inc.

text: GROUP 1 HELICOPTERS

text: GROUP 1 HELICOPTERS TC Holder Model Com. des. Part-66 type rating endorsement Note

text: […] […] […] […] […] AIRBUS H160-B AIRBUS HELICOPTERS H160 (SAFRAN

text: HELICOPTERS ARRANO 1)

text: AIRBUS MBB-BK117 H145 Eurocopter MBB-BK 117 D3 (Safran HELICOPTERS D-3 Arriel 2)

text: DEUTSCHLAND GmbH

text: AIRBUS MBB-BK117 H145 Eurocopter MBB-BK 117 D3 (Safran HELICOPTERS D-3m Arriel 2)

text: DEUTSCHLAND GmbH

text: ERICKSON AIR- S-64E Erickson S-64 (Erickson JFTD 12)

text: CRANE

text: LEONARDO AW189 AW189K AW189 (Safran ANETO-1K)

text: S.p.A.

text: […] GROUP 3: PISTON-ENGINE AEROPLANES (other than those in Group 1)

text: GROUP 3: PISTON-ENGINE AEROPLANES (other than those in Group 1)

text: Type of Part-66 MTOM TC Holder Model Note structure type rating endorsement ≤2T >2T […] […] […] […] […] […] […] AQUILA Aviation AQUILA Composite Aquila AT01 (Rotax) ELA1 X by Excellence AG AT01-200

text: BLACKSHAPE BS 115 Composite Blackshape BS 115/BK 160 ELA1 X

text: S.p.A. (Rotax Lycoming)

text: BLACKSHAPE BK 160 Composite Blackshape BS 115/BK 160 ELA1 X

text: S.p.A. (Lycoming)

text: BLACKSHAPE BK 160-200 Composite Blackshape BS 115/BK 160 ELA1 X

text: S.p.A. (Lycoming)

text: BLACKSHAPE BK 160TR Composite Blackshape BS 115/BK 160 ELA1 X

text: S.p.A. (Lycoming)

text: BRM Aero s.r.o. Bristell B23 Metal Bristell B23 (Rotax) ELA1 X

text: BRM Aero s.r.o. Bristell B23- Metal Bristell B23 (Rotax) ELA1 X 915 Czech Sport PS-28 N Composite + Aircraft a.s. Cruiser Metal Czech Sport PS-28 (Rotax) ELA1 X

text: DIAMOND

text: ELA1 AIRCRAFT DA 40 Composite Diamond DA40 (Lycoming) X ELA2

text: Industries DIAMOND

text: ELA1 AIRCRAFT DA 40 F Composite Diamond DA40 (Lycoming) X ELA2

text: Industries DIAMOND

text: ELA1 AIRCRAFT DA 40 D Composite Diamond DA40 D (Technify) X ELA2

text: Industries DIAMOND

text: AIRCRAFT DA 50 C Composite Diamond DA50 (Continental) ELA2 X

text: Industries EXTRA Flugzeugprodukti ons- und

text: EA 300 Composite Extra EA-300 Series (Lycoming) ELA1 X

text: Vertriebs-GmbH Extra Aerobatic Aircraft GmbH EXTRA Flugzeugprodukti ons- und

text: EA 300/200 Composite Extra EA-300 Series (Lycoming) ELA1 X

text: EA 300/L Composite Extra EA-300 Series (Lycoming) ELA1 X

text: EA 300/LC Composite Extra EA-300 Series (Lycoming) ELA1 X

text: EA 300/LT Composite Extra EA-300 Series (Lycoming) ELA1 X

text: EA 300/S Composite Extra EA-300 Series (Lycoming) ELA1 X

text: Vertriebs-GmbH Extra Aerobatic Aircraft GmbH

text: GROUP 3: PISTON-ENGINE AEROPLANES (other than those in Group 1) EXTRA Flugzeugprodukti ons- und

text: EA 300/SC Composite Extra EA-300 Series (Lycoming) ELA1 X

text: Vertriebs-GmbH Extra Aerobatic Aircraft GmbH Extra Aerobatic

text: EXTRA NG Composite Extra NG (Lycomimg) ELA1 X

text: Aircraft GmbH Flight Design

text: general aviation F2-CS23 Composite F2-CS23 (Rotax) ELA1 X

text: GmbH Flight Design GmbH

text: Flight Design CTLS-ELA Composite CTLS-ELA (Rotax) ELA1 X

text: general aviation GmbH ISSOIRE

text: APM41 Composite Issoire APM 40 (Rotax) ELA1 X

text: AVIATION LAVIA

text: MetalMetal

text: ARGENTINA S.A. PA-25 Piper PA-25 Series (Lycoming) ELA2 X

text: tubing Fabric

text: (LAVIASA) LAVIA

text: MetalMetal

text: ARGENTINA S.A. PA-25-235 Piper PA-25 Series (Lycoming) ELA2 X

text: tubing Fabric

text: (LAVIASA) LAVIA

text: MetalMetal

text: ARGENTINA S.A. PA-25-260 Piper PA-25 Series (Lycoming) ELA2 X

text: tubing Fabric

text: (LAVIASA) Magnaghi

text: Sky Arrow Aeronautica Composite III Sky Arrow 600 (Rotax) ELA1 X 600 Sport

text: S.p.A.

text: Pipistrel Vertical Virus SW Composite Pipistrel Virus (Rotax) ELA1* X Solutions d.o.o. 121 Pipistrel Vertical Virus SW Composite Pipistrel Virus Electro (Pipistrel ELA1** X Solutions d.o.o. 128 E-811)

text: TECNAM

text: Costruzioni P-Mentor Metal Tecnam P2002 (Rotax) ELA1 X

text: Aeronautiche TECNAM

text: Composite +

text: Costruzioni P2010 TDI Tecnam P2010 (Continental) ELA1 X

text: Metal

text: Aeronautiche

text: ELA1. Viper SD-4 TOMARK, s.r.o. Metal Tomark Viper SD-4 (Rotax) Restricted X RTC TC. TEXTRON 402C Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 414A Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 421B Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 421C Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 404 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 401 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 402 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 411 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 414 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 421 Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 401A Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 401B Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 402A Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: TEXTRON 402B Composite Cessna 400 Series (Continental) X

text: AVIATION Inc.

text: *Electrical Virus variants certified (within the L2 licence privilege) GROUP 4 SAILPLANES

text: GROUP 4 SAILPLANES

text: TC Holder Model Type of structure Note […] […] […] […]

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-100 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-100 ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-100 G Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-100 G ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-1000S Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-200 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-200/17 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-200/17 C Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-300 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-300 CLUB ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-300 CLUB ELAN ACRO Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-300 ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-300 ELAN ACRO Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500 ELAN ORION Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500 ELAN TRAINER Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500/20 ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500/22 ELAN Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-600 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-600/18 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-800 S Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-808 S Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-0 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 10-a Composite

text: GROUP 4 SAILPLANES DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-a Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-b Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-c Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-d Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-e Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-f Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 1-f (45) Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 3 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 3-17 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 3-a Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 4 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 4-a Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 4-b Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6-18w Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6-a Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6-b Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6-c Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 6-c18 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 7 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS 7-WL Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS10-s Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-18 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-a Composite

text: GROUP 4 SAILPLANES DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-b Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-s Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-sb Composite The model has also M&D Flugzeugbau GmbH & Co. KG powered variants. JS-MD 3 Composite M&D Flugzeugbau GmbH & Co. KG JS-MD 3 RES Composite SPORTINE AVIACIJA IR KO LAK-17A mini Composite

text: GROUP 4 POWERED SAILPLANES

text: GROUP 4 POWERED SAILPLANES

text: TC Holder Model Type of structure Note […] […] […] […] ALEXANDER SCHLEICHER AS 33 Es Composite ALEXANDER SCHLEICHER AS 33 Me Composite (electrical) ALEXANDER SCHLEICHER AS 34 Me Composite (electrical)

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-1000M Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-1000T Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-1001E Composite (electrical)

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-400 Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500 M Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-500 MB Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-600/18 M Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-600M Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-800 A Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-800 B Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-800 LA Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH DG-808 C Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS10-st Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-e Composite

text: GROUP 4 POWERED SAILPLANES DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS8-t Composite

text: DG FLUGZEUGBAU GMBH

text: DG AVIATION GmbH LS9 Composite GANTENBRINK, BRUNO EtaN4 Composite HPH SPOL SRO Glasflügel 304 S Jet composite LANGE AVIATION GMBH Antares 18T composite SCHEMPP HIRTH FLUGZEUGBAU Ventus-3M Composite SCHEMPP HIRTH FLUGZEUGBAU Ventus-3F Composite SPORTINE AVIACIJA IR KO LAK-17B FES mini Composite […] […] […] […]

text: GROUP 4 GAS BALLOONS

text: GROUP 4 GAS BALLOONS TC Holder Model Note

text: […] […] […] CAMERON BALLOONS LIMITED TGB-1150 Tethered gas balloon LINDSTRAND TECHNOLOGIES LTD 197-T (PTB) Tethered gas balloon […] […] […]

text: GROUP 4 HOT-AIR BALLOONS

text: GROUP 4 HOT-AIR BALLOONS TC Holder Model Note

text: […] […] […] BALLONS CHAIZE SSHAB-Model ELA1 BALLONS CHAIZE SW-Model […] […] […]

text: Appendix II to AMC to Annex III — Aircraft Type Practical Experience and On-the-Job Training — List of Tasks

text: Tasks are divided in categories of aircraft: 1) Aircraft type practical experience The tasks are divided in categories of aircraft: A) aeroplanes and helicopters B) sailplanes and powered sailplanes C) balloons and airships A. SPECIFIC TASKS FOR AEROPLANES AND HELICOPTERS […] B. SPECIFIC TASKS FOR SAILPLANES AND POWERED SAILPLANES […] C. SPECIFIC TASKS FOR BALLOONS AND AIRSHIPS

text: Tasks Balloon Airship

text: Hot-air Gas Hot-air Gas (free/tethered)

text: General activities:

text: Functionality test of aircraft (*) x x x x Placards check or replacement x x x x Documentation annual inspection, repair, x x x x ADs, equipment (*) Classification repair (*) x x x x

text: Weighing:

text: Weighing and weighing report (*) x x x x

text: Servicing:

text: Lubrication of controls when applicable x x x Cleaning of envelope, basket, burner x x x x

text: Inspections:

text: Eight annual inspections (covering at least 3 x three different types) (*) Five annual inspections (covering at least 2 x (free) two different types) (*) Three annual inspections (covering at least 2 x (tethered) x two different types) (*) Two annual inspections (*) x Strength test of envelope fabric (*) x x x x

text: Flight control systems: Removal — Inspection — Reinstallation

text: Control surface cable x Trim system x

text: Tasks Balloon Airship

text: Hot-air Gas Hot-air Gas (free/tethered) Safeguarding of pins, screws, castellated nuts x (tethered) x x (*) Stick and pedals x Hydromechanical control systems x (tethered) x Ballonet control systems (*) x (tethered) x x Electrical control systems x (tethered) x Valves (gas valve, turning vent, parachute or x x x x rip panel) (*) Control and shroud lines and pulleys x x x x Elevator — stabiliser (including balancing if x applicable) Rudder (including balancing if applicable) x Drag rope x (free)

text: Electrical system:

text: Removal — installation of electrical wires x (tethered) x x Removal — installation of electrical x (tethered) x x components Servicing of batteries x x x x

text: Communication system — transponder:

text: Removal — installation of COM x x x x Removal — installation of NAV x Removal — installation of XPDR x x x x Installation of antenna x x x x Replacement of antenna cable x x x x

text: Cabin — equipment:

text: Pitot-static systems — tubes removal — x installation — replacement Flight instruments: removal — installation — x x x x replacement Installation of an approved system x x x x Magnetic compass installation — x compensation Fire extinguisher x x x

text: Ballast — replacement of:

text: Water ballast (when applicable) x Sand/shot ballast (when applicable) x x Valves — inspection and rigging of valves x

text: Envelope:

text: Inspection and repair of envelope x x x x panels/gores/seams Inspection and repair of load tapes and x x x x attachment points Inspection and repair of deflation system x x x Inspection and repair of net x Inspection and repair of mooring system x (tethered)

text: Tasks Balloon Airship

text: Hot-air Gas Hot-air Gas (free/tethered) Electrostatic conductivity test (if type is x x approved for hydrogen) (*) Ballonet inspection and repair x x Inspection and fabrication of a suspension x x x x cable or rope Inspection and fabrication of a catena x x

text: Load ring/frame:

text: Crack detection (welded and machined parts) x x x (*)

text: Heater system:

text: Removal, inspection and reinstallation x x Inspection and cleaning of vaporiser and filter x x (*) Inspection and replacement of hoses (*) x x Inspection and replacement of pilot flame x x ignition unit (*) Sealing of fittings (*) x x Pressure and leak test (*) x x Disassembly and assembly of fuel cell (*) x x 10-year inspection of fuel cell x x

text: Basket/gondola:

text: Removal, inspection and reinstallation (as x x x x applicable) Inspection and fabrication of a suspension x x cable or rope (*) Removal — installation of padding x x Removal — installation of belts — safety x x harness Removal — installation of essential elements x x x x of the cabin Inspection and fabrication of a basket wire x x Inspection of operational equipment and its x x x x fixation points Crack detection and repair (welded parts and x x x x frames)

text: Landing gear:

text: Removal, inspection and reinstallation of x (tethered) x x wheels Removal, inspection and reinstallation of x brakes Removal, inspection and reinstallation of x shock absorbers

text: Fuel — Engine — Propeller — Engine instruments systems:

text: Refer to tasks in blocks for aeroplanes x x

text: Wood structure:

text: Structure repair x x Protective coating

text: Tasks Balloon Airship

text: Hot-air Gas Hot-air Gas (free/tethered)

text: Composite structure:

text: Laminate repair x (tethered) x Sandwich structure repair x (tethered) x

text: Metallic structures:

text: Crack detection (welded and machined parts) x x x x Riveting jobs x x Bonding of structures x x x Anticorrosion treatment x (tethered) x x Repair of fairings x (tethered) x

text: Engine:

text: Tasks for aeroplanes of comparable x x certification level

text: Exhaust system:

text: Propeller:

text: Fuel system:

text: Hydraulic system:

text: Pneumatic system:

text: Winch system:

text: Witness winch inspection x (tethered)

text: 2) List of tasks for OJT The minimum list of tasks should be selected from the table below according to the following procedures and criteria: (i) Filter the ATA chapters (or sub-chapters, when required) applicable to the specific aircraft type (add others if they are missing). (ii) Identify relevant and significant tasks for each required category of INS, FOT, SGH, R/I, MEL and TS. (iii) Retain the required percentage for each task category, and throughout ATA chapters, as much as relevant to the particular aircraft type. The selection of tasks should give precedence to tasks which are critical and complex in terms of: — difficulty to execute; — interpretation of the maintenance procedures / work instructions; — specific tools and equipment; — coordination among maintenance staff (teamwork); — human factors (accessibility, human–machine interface (HMI), etc.); — safety impact on the aircraft and the crew. Removal and installation tasks include the final confirmation test, if required. Credit may be given for similar tasks between ATA systems (e.g. pneumatic valves in ATA 21, 30 and 36), but this should be kept to a minimum. Some tasks may be performed on another aircraft type as long as both the system and the task are similar. The following table provides an acceptable method of selection of OJT tasks for B1 and B2 AML categories, per ATA chapter or sub-chapters, as required by point 6.2(e) of Appendix III to Annex III.

text: OJT TASK SELECTION B1 B2 ATA Chapters INS FOT SGH R/I MEL TS INS FOT SGH R/I MEL TS

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories

text: Introduction subjects:

text: 05 Time limits / maintenance checks X — — — — — X — — — — — (see Note below) 06 Dimensions/ X — — — — — X — — — — — areas 07 Lifting and X — — — — — X — — — — — shoring 08 Levelling and — — — — — — X X X — — — weighing 09 Towing and — — — — — — X — X — — — taxiing 10 Parking/mooring, storing and return to — — X — — — — — X — — — service 11 Placards and X — — — — — X — — — — — markings 12 Servicing — — X — — — — — X — — — 20 Standard practices — only X — X — — — X — X — — — type particular (ATA 50 or 60)

text: Rotorcraft (only):

text: 18 Vibration and noise analysis (blade — — — — — X — — — — — — tracking) 62 Rotors 62-10 Rotor blades X — — X — — — — — — — — 62-20 Rotor head(s) X — — X — — — — — — — — 62-30 Rotor shaft(s) / swashplate X — — X — — — — — — — — assy(s) 62-40 Indicating — X X — X X — — — — — X 63 Rotor drives 63-10 Engine/gearbox X — X X — — — — — — — — couplings 63-20 Gearbox(es) X — X X — — — — — — — — 63-30 Mounts, X — X — — — — — — — — — attachments 63-40 Indicating — X — — X X — — — — — X 63-50 Rotor brake X — — X — — — — — — — — 63-60 Drain lines X — — — — — — — — — — — 64 Tail rotor

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 64-10 Rotor blades X — X X — — — — — — — — 64-20 Rotor head X — — X — — — — — — — — 64-40 Indicating — X — X X X — — — — — X 65 Tail-rotor drive 65-10 Shafts X — X X — — — — — — — — 65-20 Gearboxes X — X X — — — — — — — — 65-40 Indicating — X — — X X — — — — — X 66 Folding blades / pylon 66-10 Rotor blades X — — X — — — — — — — — 66-20 Tail pylon X — — — — — — — — — — — 66-30 Controls and — — — — — — — — — X X X indicating 67 Rotors flight control 67-10 Rotor X — — — — — — — — — — — 67-20 Antitorque — — — — — — — — — — rotor control X X (yaw control) 67-30 Servocontrol — — — — — — — — — — X X system

text: Airframe systems:

text: 21 Air conditioning 21-10 Compression — — X X — X — — — — — — 21-20 Distribution — X — X — — — — — — — — 21-30 Pressurisation — — — — — — — — — X X X control 21-40 Heating — — — X — — — — — — — — 21-50 Cooling — — — X — — — — — — — — 21-60 Temperature — — — X X X — — — — — — control 22 Autoflight 22-10 Autopilot — — — — — — — X X X X X 22-20 Speed — — — — — — — — — — X X attitude correction 22-30 Autothrottle — X — — — — X X — X — X 22-40 System — — — — — — — — — — X X monitor 22-50 Aerodynamic — — — — — — — — — — X X load alleviating 23 Communications 23-10 Speech — — — X — — — — — X X X communications 23-15 SATCOM — X — — — — X X — X — X

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 23-20 Data transmission and — X — — — — — X — X — X automatic calling 23-30 Passenger — address, — X — — — — X — X — X entertainment and comfort 23-40 Interphone — X — — — — X — — X — X 23-50 Audio — — X — — — — — X — X X integrating 23-60 Static — — — — — X X — X X X X discharging 23-70 Audio and — — — — — X X X — X — X video monitoring 23-80 Integrated — — — — — — — X — X — X automatic tuning 24 Electrical power 24-10 Generator — — X X X X X X X X X X drive 24-20 AC Generation — X — — — X X X — — X X 24-30 DC generation — X — X — X X X — X X X 24-40 External — — — X — X X X X — X X power 24-50 AC electrical — — — — — — X — X X X X load distribution 24-60 DC Electrical — — — — X — — — X X X X load distribution 25 Equipment and furnishings 25-10 Flight — — — — X X X X X — X X compartment 25-20 Passenger — — — — — — — — X — — X compartment 25-30 Galley X X — X — — X X — — — — 25-40 Lavatories X X — — — — X — — — — — 25-50 Additional — — — — — — — — — — X X compartments 50-00 Cargo accessory X — — — — — — — — — — — compartment 50-10 Cargo X — — — — — — — — — — — compartments 50-20 Cargo loading — X X — — — X X — — — X systems 50-30 Cargo-related X — — — — — — — — — — — systems 50-50 Accessory X — — — — — — — — — — — 50-60 Insulation X — — — — — — — — — — —

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 25-60 Emergency X X X X — — X X — — — — 26 Fire protection 26-10 Detection — X - X — X — X — — — X 26-20 Extinguishing — X X X — — — — — — — — 26-30 Explosion X — — — — — — — — — — — suppression 27 Flight controls 27-10 Aileron and — — — X — — — — X X X X tab 27-20 Rudder and — — — X — — — — X X X X tab 27-30 Elevator and — — — X — — — — X X X X tab 27-40 Horizontal — — — X — — — — X X X X stabiliser 27-50 Flaps X X — X — X — X — — — — 27-60 Spoiler, drag — — — X — — — — devices and variable X X X X aerodynamic fairings 27-70 Gust lock and — — X — — — — X X X X X dampener 27-80 Lift — — X — — — — — X X X X augmenting 28 Fuel systems 28-10 Storage X — X X X — — — X — — — 28-20 Distribution — — — X — — — X — — — — 28-30 Dump X — — — — — — - — — — 28-40 Indicating — X — — — X X X — — — X 47-00 Nitrogen — — — — X X X X X X — X generation system 29 Hydraulic power 29-10 Main X X X X — — — X — — — — 29-20 Auxiliary — X X X — — — X — — — — 29-30 Indicating — X — X — X — X — — — X 30 Ice and rain protection 30-10 Aerofoil X X — X — — — — — — — — 30-20 Air intakes X X — — — — — — — — — — 30-30 Pitot and — — — X — — X — — X X X static 30-40 Windows, — — — — — — — windshields and — X X X X doors 30-50 Antennas and — — — — — — — X X X X X radomes

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 30-60 — — — — — — — X — — — — Propellers/rotors 30-70 Water lines X — — — — — X — — — — — 30-80 Detection — X — X — X — X — — — X 31 Indicating/recording systems 31-10 Instrument — X — X — — — X — X X X and control panels 31-20 Independent — X — — — — — X — X — X instruments 31-30 Recorders — X — — — — — X X X — — 31-40 Central — — — — — — — X — X — X computers 31-50 Central — X — — — — — X — X X X warning systems 31-60 Central — X — — — — — X — X — X display systems 31-70 Automatic data reporting — — — — — — — X X X — X systems 32 Landing gear 32-10 Main gear and X X X X — — — — — — — — doors 32-20 Nose gear and X X X X — — — — — — — — doors 32-30 Extension and — X X — X X — — — — — — retraction 32-40 Wheels and — X — X X — — — — — — — brakes 32-50 Steering X X X X — X — — — — — — 32-60 Position — indication and — X — X X X X — X — X warning 32-70 X X X X — — — — — — — — Supplementary gear 33 Lights 33-10 Flight — — — — — X X X X X X X compartment 33-20 Passenger — — — — — X X X X X X X compartment 33-30 Cargo and — — — — — — — service X X X X X compartments 33-40 Exterior X X — X — — X X — — — X 33-50 Emergency — — — — — X — X X X X X lighting 34 Navigation

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 34-10 Flight — X — — — — — X — — — X environment data 34-20 Attitude and — X — — — — — X — X X X direction 34-30 Landing and — — — — — — — X — X X X taxiing aids 34-40 Independent — X — — — — — X — X X X position determining 34-50 Dependent — — — — — — — X — X X X position determining 34-60 Flight management — X — — — — — X X X X X computing 35 Oxygen 35-10 Crew X X X X — X — — — — — — 35-20 Passengers X X — X — — — — — — — — 35-30 Portable X — — — — — — — — — — — 36 Pneumatic 36-10 Distribution X X — X — X — X — — — — 36-20 Indicating — X — X — X X X — — — X 37 Vacuum 37-10 Distribution — X — X — X — — — — — — 37-20 Indicating — X — X — X — X — — — X 38 Water/waste 38-10 Potable — X X X — — — X — — — — 38-20 Wash — — — — — — — — — — — — 38-30 Waste — — — — — — — — X X X X disposal 38-40 Air supply X X — — — — — — — — — — 41 Water ballast 41-10 Storage X — — — — — — — — — — — 41-20 Dump X — — — — — — — — — — — 41-30 Indication X — — — — — — — — — — X 42 Integrated — — — — — X X X X X X X modular avionics 44 Cabin systems 44-20 In-flight — entertainment — X — — — — — X X X X system 44-30 External — communication — X — — — — — X X X X system 44-40 Cabin mass — — — — — — — — X X X X memory system

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 44-50 Cabin — — — — — — — X — X X X monitoring system 44-60 Miscellaneous — — — — — — — X — X X X cabin system 45 Onboard — X — — — — — X — X X X maintenance system 46 Information Systems 46-10 Aeroplane general information — — — — — — — X — X X X systems 46-20 Flight deck — X — — — — — X — X X X information systems 46-30 Maintenance — X — — — — — X — X X X information systems 46-40 Passenger cabin information — X — — — — — X — X X X systems 46-50 Miscellaneous — — — — — — — X — X X X information systems

text: Airframe structures:

text: 52 Doors 52-10 X — X X X — — — — — — — Passenger/crew 52-20 Emergency X — X X X — — — — — — — exits 52-30 Cargo X — — — — — — — — — — — 52-40 Service and X — — — — — — — — — — — miscellaneous 52-50 Fixed interior X — — — — — — — — — — — 52-60 Entrance X — — — — — — — — — — — stairs 52-70 Monitoring — X — — — — X X — — — X and operation 52-80 Landing gear X — X — — — — — — — — — 53 Fuselage X — — — — X — — — — — — 54 Nacelles/pylons X — — — — — — — — — — — 55 Stabilisers X — — — — — — — — — — — 56 Windows X — — — — X — — — — — — 57 Wings X — — — — — — — — — — —

text: Auxiliary power units (APUs):

text: 49 Auxiliar power unit 49-10 Power plant X X — X X X — X — — — — 49-20 Engine X X — X — — — — — — — —

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 49-30 Engine fuel — X — X — — — — — — — — and control 49-40 — X — — — — X — — — — X Ignition/starting 49-50 Air X — — — — — — — — — — — 49-60 Engine — — — — — — — — — — — X controls 49-70 Indicating — X — — — — — — — — — — 49-80 Exhaust X — — — — — — — — — — — 49-90 Oil — — X — — — — — — — — —

text: Turbine engines:

text: 70 Standard practices and engine X — — — — X — — — — — — performance 71 Power plant X — X — — — — — — — — — 71-10 Cowling X — X X — — — — — — 71-20 Mounts X — — — — — — — — — — — 71-30 Fire seals X — — — — — — — — — — — 71-40 Attach fittings X — — — — — — — — — — — 71-50 Electrical — — — — — — X X — X X X harness 71-60 Air intakes X — — — — — — — — — — 72T Engine turbine / X — X X — — — — — — — — turboprop / ducted fan / unducted fan 73 Engine fuel and control 73-10 Distribution X — — — — — — — — — — — 73-20 Controlling — — — X X — X X X — X X (FADEC) 73-30 Indicating X X — — X — — X — — — X 74 Ignition 74-10 Electrical — — — — — — X X X X X X power 74-20 Distribution X X — — — — X X — — — X 74-30 Switching X X — X — — X X — — — X 75 Air 75-10 Engine anti- — — — — — — X X — X X X icing 75-20 Cooling X — — — — — — — — — — — 75-30 Compressor — — — — — — — — — — — X control 75-40 Indicating — X — — — — — X — — — X 76 Engine controls

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 76-10 Power control — X — — X — — X — — — X (FADEC) 76-20 Emergency — — — — X — — — — — — — shutdown 77 Engine indicating — X — — X X X X — — X X 78 Exhaust 78-30 Thrust X — — X X X — X — — — X reverser 79 Oil X — X X — — — — — — — — 80 Starting X X — X X X — — — — — — 83 Accessory X — X X — — — — — — — — gearboxes

text: Piston engines:

text: 70 Standard practices and engine X — — — — X — — — — — — performance 71 Power plant X — X — — — — — — — — — 71-10 Cowling X — X X — — — — — — — — 71-20 Mounts X — — — — — — — — — — — 71-30 Fire seals X — — — — — — — — — — — 71-40 Attach fittings X — — — — — — — — — — — 71-50 Electrical — — — — — — X X — X X X harness 71-60 Air intakes X — — — — — — — — — — — 72R Engine — X — X X — — — — — — — — reciprocating 73 Engine fuel and — X X X X X — — — — — — control 73-10 Distribution X — — — — — — — — — — — 73-20 Controlling — — — — — X X X X X X X (FADEC) 73-30 Indicating X X — — X — X X — — — X 74 Ignition 74-10 Electrical — — — X X — X — X X X X power 74-20 Distribution X X — — — — X X — — — X 74-30 Switching X X — X — — X X — — — X 76 Engine controls X X — X — X - X — — — X 77 Engine indicating — X — — X X X X — — X X 78 Exhaust X — — — — — — — — — — — 79 Oil X — X X — — — — — — — — 80 Starting X X — X X X — — — — — —

text: Requirements: % of 75 % 50 % 50 % 50 % 25 % 25 % 75 % 50 % 50 % 50 % 25 % 25 % task categories 81 Turbines (reciprocating X X X X — — — — — — — — engine) 83 Accessory X — X X — — — — — — — — gearboxes

text: Propellers:

text: 61 Propellers/ propulsion 61-10 Propeller X — X X — — — — — — — — assembly 61-20 Controlling — — — X X — — — — — — — 61-30 Braking X — — — — — — — — — — — 61-40 Indicating — X — — X X — X — — — X 61-50 Propulsor — — — — — X — — — — — — duct 61B Propeller pitch — X — X X X — — — — — — control 61C Propeller — X — — — X — X — — — X synchronising 61D Propeller — X X X X X — X — — — X electronic control 61E Propeller ice X X — — X X — — — — — — protection

text: Note: For ATA Chapter 5, select at least one task from category (a), two tasks from category (b), and three tasks from category (c): (a) Perform and/or assist in performing a scheduled maintenance check: — accomplishment of 100-hour check (general aviation (GA) aircraft); — accomplishment of a ‘daily’ or ‘weekly’, ‘service’, ‘transit’ or equivalent check; — active participation in a scheduled check, e.g.: ‘A-Check’, ‘B-Check’, ‘C-Check’ or the equivalent of a base maintenance check. (b) Review the aircraft maintenance log for correct completion: — closure of MEL/CDL items; — dent and buckle chart review, including inspections on fuselage and skin damages assessment in accordance with the SRM; — fuel or oil leakage tests. (c) Perform unscheduled inspection following: — hard landing; — overweight taxiing; — bird/hail strike; — aborted take-off; — high-energy stop; — wheel-bearing failure; — exceedance of max NLG steering angle; — landing gear shimmy/vibrations; — lightning strike / HIRF; — tail strike; — winglet strike; — severe turbulence / extreme high winds; — airframe vibrations; — ice/snow conditions; — flight control overspeed down; — hot-air duct rupture; — relief pressure panels open; — mercury spillage; — galley spill; — hydraulic fluid reaction with titanium; — cabin overpressure; — exceedance of fuel imbalance; — smoke/fumes in the cabin; — abnormal doors operations; — ferry flight maintenance; — others.

text: GM1 Appendix II to AMC to Annex III — Aircraft Type Practical Experience and On-the-Job Training — List of Tasks

text: The following list represents an example of OJT tasks for B1.1 and B2 (Aeroplanes Turbine) AML categories. The list is not exhaustive, nor tailored to a specific aircraft type, and should be reviewed and adjusted as necessary.

text: Task No ATA chapter Task description B1.1 B2

text: 1 05 Time limits / maintenance Perform (assist) in A-Check X X checks 2 05 Time limits / maintenance Close MEL/CDL item X X checks 3 05 Time limits / maintenance Review Dent & Buckle chart X — checks 4 05 Time limits / maintenance Perform bird strike inspection X — checks 5 05 Time limits / maintenance Perform lightning strike inspection X X checks 6 05 Time limits / maintenance Perform tail strike inspection X — checks 7 05 Time limits / maintenance Review AD compliance X X checks 8 06 Dimensions/areas Locate component by station number X X 9 07 Lifting and shoring Jack aircraft wheel X — 10 07 Lifting and shoring Jack the aircraft X — 11 08 Levelling and weighing Level the aircraft X — 12 08 Levelling and weighing Weigh the aircraft (including W&B X — amendment) 13 08 Levelling and weighing Check the aircraft against equipment list X X 14 09 Towing and taxiing Tow the aircraft (including preparation) X — 15 10 Parking/mooring, storing Park aircraft (including applying applicable X — and return to service protections to parking duration) 16 10 Parking/mooring, storing Position aircraft in dock X — and return to service 17 11 Placards and markings Perform placards and markings inspection X X 18 12 Servicing Perform aircraft refuelling (automatic and X — manual) 19 12 Servicing Check and adjust tyre pressure X — 20 12 Servicing Check and replenish hydraulic fluid X — 21 12 Servicing Check and adjust accumulator pressure X — 22 12 Servicing Check and replenish engine oil X — 23 12 Servicing Perform landing gear servicing X — 24 12 Servicing Perform waste / potable water servicing X — 25 12 Servicing Connect ground power X X 26 12 Servicing Lubricate flight control elements X — 27 20 Standard practices Perform aircraft grounding X X 28 20 Standard practices Perform ESDS device inspection X X 21 Air conditioning … …

text: 29 21-20 Distribution Replace recirculation filter X — 30 21-40 Heating Replace combustion heater X — 31 21-20 Distribution Clean outflow valve X — 32 21-20 Distribution Replace outflow valve X — 33 21-50 Cooling Replace ACM / Air cycle unit X — 34 21-50 Cooling Replace heat exchanger X — 35 21-30 Pressurisation control Replace pressurisation controller X X 36 21-30 Pressurisation control Perform pressurisation system functional test X X 37 21-20 Distribution Perform equipment cooling system X X functional test 38 21-20 Distribution Check configuration of AVX compartment X X ventilation system 39 21-30 Pressurisation control Perform air-conditioning system functional X X test 40 21-60 Temperature control Perform temperature control system X X functional test 41 21 Air conditioning Troubleshoot faulty system X X 42 22 Autoflight Replacement of autothrottle X — servomechanisms components 43 22 Autoflight Replace actuator X — 44 22 Autoflight Replace controller X X 45 22 Autoflight Replace amplifier X X 46 22 Autoflight Replace autoflight system LRU X X 47 22 Autoflight Perform yam damper operational test X X 48 22 Autoflight Perform autopilot functional test X X 49 22 Autoflight Perform autopilot gain adjustment — X 50 22 Autoflight Check augmentation system X X 51 22 Autoflight Check operation of autothrottle X X 52 22 Autoflight Perform autoland functional test X X 53 22 Autoflight Check flight management systems X X 54 22 Autoflight Perform Mach trim functional test — X 55 22 Autoflight Upload FM data X X 56 22 Autoflight Troubleshoot faulty system — X 57 23 Communications Perform interphone system operational test X X 58 23 Communications Service interphone components X X 59 23 Communications Replace HF unit X X 60 23 Communications Replace VHF unit X X 61 23 Communications Replace antenna X X 62 23 Communications Perform voice recorder operational test X X 63 23 Communications Replace voice recorder X X 64 23 Communications Perform static discharge components X X inspection 65 23 Communications Perform radio functional test — X 66 23 Communications Perform SELCAL operational test X X 67 23 Communications Perform co-axial cable repair — X 68 23 Communications Perform ELT operational test X X 69 23 Communications Troubleshoot faulty system — X

text: 70 24 Electrical power Supply/remove APU power X X 71 24 Electrical power Remove/install battery X X 72 24 Electrical power Charge battery X X 73 24 Electrical power Perform battery charger operational test X X 74 24 Electrical power Perform standby power system functional X X test 75 24 Electrical power Replace IDG oil filter X X 76 24 Electrical power Remove/install IDG X X 77 24 Electrical power Perform IDG functional test X X 78 24 Electrical power Replace switch X X 79 24 Electrical power Replace CB X X 80 24 Electrical power Replace voltage regulator — X 81 24 Electrical power Perform voltage regulator functional test X X 82 24 Electrical power Perform electrical feeder cable repair — X 83 25 Equipment and furnishings Perform emergency equipment inspection X X 84 25 Equipment and furnishings Replace carpets X — 85 25 Equipment and furnishings Perform crew seats operational test X — 86 25 Equipment and furnishings Replace crew seats X — 87 25 Equipment and furnishings Replace passenger seats X — 88 25 Equipment and furnishings Perform seats and seat belts inspection X — 89 25 Equipment and furnishings Check ELT for compliance with applicable X X regulations 90 25 Equipment and furnishings Perform escape slide inspection X — 91 25 Equipment and furnishings Remove/install escape slide X — 92 25 Equipment and furnishings Perform upholstery repair X — 93 25 Equipment and furnishings Remove/install interior panels X — 94 25 Equipment and furnishings Remove/install cargo compartment panels X — 95 25 Equipment and furnishings Perform cargo loading system inspection X — 96 25 Equipment and furnishings Perform cargo loading system functional test X X 97 25 Equipment and furnishings Replace cargo loading system actuator X — 98 26 Fire protection Check fire bottle content X — 99 26 Fire protection Remove/install fire bottle X — 100 26 Fire protection Replace fire bottle squib X — 101 26 Fire protection Check portable fire-extinguisher content X — 102 26 Fire protection Perform smoke detection system functional X X test 103 26 Fire protection Perform smoke detectors inspection X X 104 26 Fire protection Remove/install smoke detectors X X 105 26 Fire protection Perform fire protection system inspection X X 106 26 Fire protection Perform fire protection system functional X X test 107 26 Fire protection Perform engine fire detection system X X inspection 108 26 Fire protection Troubleshoot faulty system X X 109 27 Flight controls Perform horizontal stabiliser components X — inspection 110 27 Flight controls Perform horizontal stabiliser operational test X X

text: 111 27 Flight controls Remove/install horizontal stabiliser X — 112 27 Flight controls Perform elevator components inspection X — 113 27 Flight controls Perform elevator operational test X X 114 27 Flight controls Remove/install elevator X — 115 27 Flight controls Perform aileron components inspection X — 116 27 Flight controls Perform aileron operational test X X 117 27 Flight controls Remove/install aileron X — 118 27 Flight controls Perform rudder components inspection X — 119 27 Flight controls Perform rudder operational test X X 120 27 Flight controls Remove/install rudder X — 121 27 Flight controls Remove/install trim tab X — 122 27 Flight controls Perform LE flap components inspection X — 123 27 Flight controls Perform LE flap operational test X X 124 27 Flight controls Perform LE devices alternate operation X X 125 27 Flight controls Remove/install LE flap X — 126 27 Flight controls Perform TE flap components inspection X — 127 27 Flight controls Perform TE flap operational test X X 128 27 Flight controls Perform TE devices alternate operation X X 129 27 Flight controls Remove/install TE flap X — 130 27 Flight controls Perform spoiler components inspection X — 131 27 Flight controls Perform spoiler operational test X X 132 27 Flight controls Remove/install spoiler X — 133 27 Flight controls Perform slat component inspection X — 134 27 Flight controls Perform slat operational test X X 135 27 Flight controls Remove/install slat X — 136 27 Flight controls Replace control cable and fittings X — 137 27 Flight controls Perform control cable tension adjustment X — 138 27 Flight controls Remove/install actuator X — 139 27 Flight controls Remove/install powered control unit X — 140 27 Flight controls Perform flight controls functional test X X 141 27 Flight controls Perform stall warning system functional test X X 142 27 Flight controls Perform control column operational test X X 143 27 Flight controls Deactivate/reactivate servo control X - 144 27 Flight controls Check / adjust gearbox oil level X - 145 27 Flight controls Troubleshoot faulty system X X 146 28 Fuel systems Perform fuel/defuel system components X — inspection 147 28 Fuel systems Fuel quantity indicating system functional X X test 148 28 Fuel systems Perform fuel transfer between tanks X — 149 28 Fuel systems Perform booster pump inspection X — 150 28 Fuel systems Remove/install booster pump X — 151 28 Fuel systems Remove/install fuel selector X — 152 28 Fuel systems Perform fuel tank inspection X — 153 28 Fuel systems Remove/install fuel control valve X —

text: 154 28 Fuel systems Remove/install fuel level indicator X — 155 28 Fuel systems Remove/install fuel line X — 156 28 Fuel systems Remove/install flame arrestor X — 157 28 Fuel systems Remove/install water drain valve X — 158 28 Fuel systems Perform fuel content calculation X — 159 28 Fuel systems Check fuel quantity gauge calibration X — 160 28 Fuel systems Perform fuel feed/selectors functional test X X 161 28 Fuel systems Perform fuel dump system functional test X X 162 28 Fuel systems Troubleshoot faulty system X X 163 29 Hydraulic power Perform hydraulic system components X — inspection 164 29 Hydraulic power Check hydraulic system indication X x 165 29 Hydraulic power Perform hydraulic system functional test X X 166 29 Hydraulic power Check auxiliary system indication X x 167 29 Hydraulic power Perform auxiliary system functional test X X 168 29 Hydraulic power Depressurise/pressurise hydraulic reservoirs X — 169 29 Hydraulic power Perform pressurisation module leak check X — 170 29 Hydraulic power Perform shut-off valve operational test X X 171 29 Hydraulic power Replace hydraulic filter X — 172 29 Hydraulic power Replace engine-driven pump X — 173 29 Hydraulic power Replace hydraulic system valve X — 174 29 Hydraulic power Replace hydraulic system line X — 175 29 Hydraulic power Perform power transfer unit operational test X X 176 29 Hydraulic power Remove/install power transfer unit X — 177 29 Hydraulic power Troubleshoot faulty system X X 178 30 Ice and rain protection Perform windshield wiper system X — components inspection 179 30 Ice and rain protection Replace windshield wiper X — 180 30 Ice and rain protection Replace windshield wiper motor X — 181 30 Ice and rain protection Adjust windshield wiper tension X — 182 30 Ice and rain protection Perform ice detection components X — inspection 183 30 Ice and rain protection Check ice detection indication X X 184 30 Ice and rain protection Perform de-icing/anti-icing system X — components inspection 185 30 Ice and rain protection Perform de-icing/anti-icing system functional X X test 186 30 Ice and rain protection Replace de-icing/anti-icing valve X — 187 30 Ice and rain protection Replace solenoid valve X X 188 30 Ice and rain protection Perform probe heating system components X — inspection 189 30 Ice and rain protection Perform probe heating system functional test X X 190 30 Ice and rain protection Perform window heating system component X — inspection 191 30 Ice and rain protection Perform window heating system functional X X test 192 30 Ice and rain protection Troubleshoot faulty system X X

text: 193 31 Indicating/recording Perform flight data recorder system X X systems components inspection 194 31 Indicating/recording Perform flight data recorder system X X systems operational test 195 31 Indicating/recording Remove/install flight data recorder X X systems 196 31 Indicating/recording Remove/install clock X X systems 197 31 Indicating/recording Remove/install master caution unit X X systems 198 31 Indicating/recording Perform flight data recorder data retrieval X X systems 199 31 Indicating/recording Perform data acquisition unit functional test X X systems 200 31 Indicating/recording Remove/install data acquisition unit X X systems 201 31 Indicating/recording Perform warning system functional test X X systems 202 31 Indicating/recording Perform EIS operational test X X systems 203 31 Indicating/recording Troubleshoot faulty system — X systems 204 32 Landing gear Perform tyres and brakes inspection X — 205 32 Landing gear Replace brake unit X — 206 32 Landing gear Perform wheels assembly X — 207 32 Landing gear Perform wheels inspection X — 208 32 Landing gear Replace wheels X — 209 32 Landing gear Replace steering actuator X — 210 32 Landing gear Perform NLG steering rigging X — 211 32 Landing gear Perform autobrake system components X — inspection 212 32 Landing gear Perform autobrake system functional test X X 213 32 Landing gear Perform landing gear alternate brake control X — components inspection 214 32 Landing gear Perform landing gear alternate brake control X X functional test 215 32 Landing gear Perform parking brake components X — inspection 216 32 Landing gear Perform parking brake functional test X X 217 32 Landing gear Perform antiskid operational test X X 218 32 Landing gear Perform landing gear extension/retraction X — system components inspection 219 32 Landing gear Replace landing gear retraction actuator X — 220 32 Landing gear Perform landing gear extension/retraction X X system functional test 221 32 Landing gear Replace uplock/downlock assembly X — 222 32 Landing gear Perform sensor adjustment X X 223 32 Landing gear Perform landing gear operational test X X 224 32 Landing gear Perform landing gear abnormal operational X X test 225 32 Landing gear Replace landing gear door X —

text: 226 32 Landing gear Replace landing gear control cable X — 227 32 Landing gear Replace landing gear safety sensor X — 228 32 Landing gear Replace landing gear shock strut X — 229 32 Landing gear Replace shimmy damper X — 230 32 Landing gear Perform air–ground system functional test X X 231 32 Landing gear Troubleshoot faulty system X X 232 33 Lights Perform interior lights inspection X X 233 33 Lights Perform interior lights operational test X X 234 33 Lights Replace interior lights X X 235 33 Lights Replace push-button switch X X 236 33 Lights Perform cargo lights X X 237 33 Lights Perform cargo lights operational test X X 238 33 Lights Replace cargo lights X X 239 33 Lights Perform exterior lights inspection X X 240 33 Lights Perform exterior lights operational test X X 241 33 Lights Replace exterior lights X X 242 33 Lights Perform emergency lights inspection X X 243 33 Lights Perform emergency lights operational test X X 244 33 Lights Replace emergency lights X X 245 33 Lights Perform landing lights inspection X X 246 33 Lights Perform landing lights operational test X X 247 33 Lights Replace landing lights X X 248 33 Lights Perform navigation lights inspection X X 249 33 Lights Perform navigation lights operational test X X 250 33 Lights Replace navigation lights X X 251 33 Lights Perform logo lights inspection X X 252 33 Lights Perform logo lights operational test X X 253 33 Lights Replace logo lights X X 254 33 Lights Troubleshoot faulty system X X 255 34 Navigation Perform Pitot-static system components X X inspection 256 34 Navigation Replace Pitot-static probe — X 257 34 Navigation Perform static and total air pressure drain — X fitting 258 34 Navigation Perform static pressure port inspection — X 259 34 Navigation Replace static pressure port — X 260 34 Navigation Replace VOR/ILS — X 261 34 Navigation Perform VOR/ILS functional test — X 262 34 Navigation Replace DME — X 263 34 Navigation Perform DME functional test — X 264 34 Navigation Perform inertial reference system functional — X test 265 34 Navigation Replace inertial reference unit — X 266 34 Navigation Perform altimeter functional test — X 267 34 Navigation Replace altimeter — X

text: 268 34 Navigation Perform air data computer functional test — X 269 34 Navigation Replace air data computer — X 270 34 Navigation Perform air speed indicator functional test — X 271 34 Navigation Replace air speed indicator — X 272 34 Navigation Perform weather radar functional test — X 273 34 Navigation Replace weather radar — X 274 34 Navigation Perform TCAS functional test — X 275 34 Navigation Replace TCAS — X 276 34 Navigation Perform ATC transponder functional test — X 277 34 Navigation Replace ATC transponder — X 278 34 Navigation Perform EGPWS functional test — X 279 34 Navigation Replace EGPWS — X 280 34 Navigation Perform ADF functional test — X 281 34 Navigation Replace ADF — X 282 34 Navigation Perform satellite communications system — X functional test 283 34 Navigation Update FM system database — X 284 34 Navigation Perform magnetic compass calibration X X 285 34 Navigation Troubleshoot faulty system — X 286 35 Oxygen Perform crew oxygen system components X — inspection 287 35 Oxygen Service crew oxygen system X — 288 35 Oxygen Perform crew oxygen system functional test X X 289 35 Oxygen Perform passenger oxygen system inspection X — 290 35 Oxygen Service passenger oxygen system X — 291 35 Oxygen Perform passenger oxygen system functional X X test 292 35 Oxygen Replace regulator X — 293 35 Oxygen Replace valve X — 294 35 Oxygen Replace oxygen generator X — 295 35 Oxygen Replace discharge disk X — 296 35 Oxygen Replace protective breathing equipment X — 297 35 Oxygen Perform auto-deployment test X X 298 35 Oxygen Troubleshoot faulty system X X 299 36 Pneumatic Perform pneumatic system components X — inspection 300 36 Pneumatic Perform pneumatic system functional test X X 301 36 Pneumatic Perform pneumatic system leakage test X — 302 36 Pneumatic Replace filter X — 303 36 Pneumatic Replace duct X — 304 36 Pneumatic Remove/install shut-off valve X — 305 36 Pneumatic Remove/install regulating valve X — 306 36 Pneumatic Remove/install regulator X — 307 36 Pneumatic Troubleshoot faulty system X X 308 37 Vacuum Perform vacuum system components X — inspection

text: 309 37 Vacuum Perform vacuum system functional test X X 310 37 Vacuum Replace vacuum pump X — 311 37 Vacuum Remove/install regulator X — 312 37 Vacuum Replace filter X — 313 37 Vacuum Troubleshoot faulty system X X 314 38 Water/waste Perform water system components X — inspection 315 38 Water/waste Perform water system functional test X X 316 38 Water/waste Depressurise/pressurise water tank X — 317 38 Water/waste Replace water pump X — 318 38 Water/waste Replace water faucet X — 319 38 Water/waste Perform water heater operational check X — 320 38 Water/waste Perform waste system components X — inspection 321 38 Water/waste Perform waste system functional test X X 322 38 Water/waste Replace waste pump X — 323 38 Water/waste Replace valve X — 324 38 Water/waste Replace tank X — 325 38 Water/waste Perform lavatory drain valve operational test X — 326 38 Water/waste Troubleshoot faulty system X X 327 45 Onboard maintenance Perform communications management unit X X system functional test 328 45 Onboard maintenance Replace communications management unit X X system 329 45 Onboard maintenance Perform communications management unit X X system data retrieval 330 45 Onboard maintenance Troubleshoot faulty system — X system 331 49 Auxiliary Power Unit Perform APU components inspection X — 332 49 Auxiliary Power Unit Perform APU functional test X X 333 49 Auxiliary Power Unit Record APU data X — 334 49 Auxiliary Power Unit Perform APU start/shutdown X X 335 49 Auxiliary Power Unit Replace APU air inlet door actuator X — 336 49 Auxiliary Power Unit Replace APU air inlet switch X — 337 49 Auxiliary Power Unit Replace APU fuel nozzle X — 338 49 Auxiliary Power Unit Replace APU igniter plug X — 339 49 Auxiliary Power Unit Perform chip detector inspection X — 340 49 Auxiliary Power Unit Perform APU emergency shutdown system X X functional test 341 49 Auxiliary Power Unit Troubleshoot faulty system X X 342 51 Structures Apply protective treatment X — 343 52 Doors Perform entry door components inspection X — 344 52 Doors Perform entry door operational test X — 345 52 Doors Remove/install entry door X — 346 52 Doors Perform crew door components inspection X — 347 52 Doors Perform crew door operational test X —

text: 348 52 Doors Perform emergency exit door components X — inspection 349 52 Doors Perform emergency exit door operational X — test 350 52 Doors Remove/install emergency exit door X — 351 52 Doors Perform cargo door components inspection X — 352 52 Doors Perform cargo door operational test X — 353 52 Doors Perform compartments doors components X — inspection 354 52 Doors Perform compartments doors operational X — test 355 52 Doors Perform snubber replacement X — 356 52 Doors Perform locking mechanism X — rigging/adjustment 357 52 Doors Perform air stair functional test X X 358 52 Doors Perform door warning system functional test X X 359 52 Doors Troubleshoot faulty system X X 360 53 Fuselage Perform radome inspection X — 361 53 Fuselage Perform damage assessment X — 362 53 Fuselage Perform structural repair X — 363 54 Nacelles/pylons Perform nacelle/pylon components X — inspection 364 54 Nacelles/pylons Remove/install nacelle strut X — 365 55 Stabilisers Perform vertical stabiliser inspection X — 366 55 Stabilisers Perform horizontal stabiliser inspection X — 367 55 Stabilisers Perform horizontal stabiliser conductive strip X — repair 368 56 Windows Perform passenger cabin windows inspection X — 369 56 Windows Remove/install passenger window X — 370 56 Windows Perform flight compartment windows X — inspection 371 56 Windows Remove/install flight compartment window X — 372 56 Windows Perform flight compartment windows X — operational test 373 57 Wings Perform wing structure inspection X — 374 57 Wings Replace wing tip X — 375 57 Wings Replace wing rib X — 376 57 Wings Perform wing structural repair X — 377 70 Standard practices and Perform fluorescent penetrant inspection X — engine performance 378 70 Standard practices and Perform engine wiring harness repair X X engine performance 379 71 Power plant Perform power plant components inspection X — 380 71 Power plant Perform powerplant removal/installation X — 381 71 Power plant Replace engine mounts X — 382 71 Power plant Perform FOD inspection X — 383 71 Power plant Remove/install engine harness X — 384 71 Power plant Perform power plant adjustment/test X — 385 71 Power plant Perform (assist) in engine dry motoring X —

text: 386 71 Power plant Perform (assist) in engine run X — 387 71 Power plant Troubleshoot faulty system X X 388 72 Engine Perform fan assembly inspection X — 389 72 Engine Remove/install fan blade X — 390 72 Engine Replace acoustical panel X — 391 72 Engine Perform engine compressor inspection X — 392 72 Engine Perform engine combustion case inspection X — 393 72 Engine Perform engine turbine inspection X — 394 72 Engine Perform gearbox assembly inspection X — 395 72 Engine Perform compressor wash X — 396 72 Engine Perform HPC borescope inspection X — 397 72 Engine Perform hot section borescope inspection X — 398 72 Engine Perform HPT borescope inspection X — 399 72 Engine Remove/install igniter X — 400 72 Engine Remove/install fuel nozzle X — 401 72 Engine Troubleshoot faulty system X X 402 73 Engine fuel and control Perform engine fuel system components X — inspection 403 73 Engine fuel and control Replace engine fuel filters X — 404 73 Engine fuel and control Replace engine-driven pump X — 405 73 Engine fuel and control Perform FADEC functional test X — 406 73 Engine fuel and control Remove/install engine electronic control X — module/unit 407 73 Engine fuel and control Troubleshoot faulty system X X 408 74 Ignition Perform ignition system components visual X — inspection 409 74 Ignition Perform ignition system functional test X X 410 74 Ignition Remove/install igniter plug X — 411 74 Ignition Remove/install ignition exciter X — 412 74 Ignition Troubleshoot faulty system X X 413 75 Air Perform engine air system components X — inspection 414 75 Air Remove/install VSV actuator X — 415 75 Air Remove/install VBV actuator X — 416 75 Air Perform engine air system functional test X X 417 76 Engine controls Perform engine controls components X — inspection 418 76 Engine controls Perform engine controls X — 419 76 Engine controls Perform engine controls functional test X X 420 76 Engine controls Perform thrust lever rigging X — 421 76 Engine controls Remove/install thrust lever X — 422 76 Engine controls Troubleshoot faulty system X X 423 77 Engine indicating Perform engine indicating components X — inspection 424 77 Engine indicating Perform engine indicating functional test X X 425 77 Engine indicating Replace engine instrument X X 426 77 Engine indicating Replace engine thermocouples X X

text: 427 77 Engine indicating Replace oil temperature bulb X X 428 77 Engine indicating Troubleshoot faulty system X X 429 78 Exhaust Perform exhaust components inspection X — 430 78 Exhaust Perform thrust reverser operational test X X 431 78 Exhaust Deactivate/reactivate thrust reverser for X — maintenance 432 78 Exhaust Remove/install thrust reverser X — 433 78 Exhaust Remove/install blocker door X — 434 78 Exhaust Replace shroud assembly X — 435 79 Oil Perform oil system components inspection X — 436 79 Oil Perform oil system functional test X X 437 79 Oil Replace oil filter X — 438 79 Oil Replace oil pump X — 439 79 Oil Replace oil cooler X — 440 79 Oil Remove/install oil pressure sensor X X 441 79 Oil Remove/install oil tank X — 442 79 Oil Troubleshoot faulty system X X 443 80 Starting Perform engine starting system components X — inspection 444 80 Starting Perform engine starting system functional X X test 445 80 Starting Replace engine start valve X — 446 80 Starting Remove/install engine starter X — 447 80 Starting Remove/install starter relay X X 448 80 Starting Troubleshoot faulty system X X