Part 66 Manual of Standards (MOS) (as amended)made under regulation 66.015 of the Civil Aviation Safety Regulations 1998.This compilation was prepared on 3 July 2026 and includes amendments F2026L00794 and F2026L00893. It is a compilation of the Part 66 Manual of Standards (MOS), as amended and in force on 3 July 2026.Prepared by the Legal Services Branch, Legal Division, Civil Aviation Safety Authority, Canberra.Compilation No. 28Contents
(a) Unless otherwise defined in this MOS, words and phrases have the same meaning as in Part 66 of CASR 1998.(b) In this MOS:AMC/GM for CASR Part 66 means the CASA publication titled Acceptable Means of Compliance (AMC) and Guidance Material (GM) CASR Part 66, as existing from time to time.AME licence means an aircraft maintenance engineer (AME) licence under regulation 31 of CAR 1988 as in force immediately before 27 June 2011.APU means auxiliary power unit.ATA means Air Transport Association of America.Note ATA is a publication referencing standard, commonly used for all commercial aircraft documentation.avionic LRU, or avionic line replaceable unit, is an aircraft avionic part that satisfies all of the following requirements:1. it must have no mechanical input from, or output to, another part or mechanism;2. it must contain only electrical, electronic, instrument or radio parts, or software, or a combination of any such part or parts and software, designed to provide control, monitor or display functions, or a combination of such functions;3. it must not require any of the following in order to be installed, secured or connected to the aircraft:(i) specialist knowledge or techniques;(ii) specialised equipment;(iii) rigging, or functional testing or adjustment, using specialised equipment external to the aircraft or brought on board the aircraft, to ensure that it is functioning properly.avionic system means an aircraft system, as specified in Table 1 in section 66.A.20, which transfers, processes, displays or stores analogue or digital data, using data lines, data buses, coaxial cables, or wireless or other data transmission media, and includes the system’s components and connectors.Note The following are examples of avionic systems:1. auto flight;2. communication, radar and navigation;3. instruments;4. in-flight entertainment systems;5. integrated modular avionics (IMA);6. cabin systems;7. on-board maintenance systems;8. information systems;9. fly-by-wire systems (related to flight control systems (ATA27));10. fibre-optic control systems.Basic Practical Experience Exclusion Removal Logbook means the CASA Part 66 Basic Practical Experience Exclusion Removal Logbook, as it exists from time to time.Basic Practical Experience Logbook means the CASA Part 66 Basic Practical Experience Logbook, as it exists from time to time.CAR 1988, or CAR, means the Civil Aviation Regulations 1988.CASR 1998, or CASR, means the Civil Aviation Safety Regulations 1998.CAO means Civil Aviation Order.category B1 modular licence means a category B1 licence granted:(a) under regulation 66.026 of CASR subject to the exclusion of at least 1 aircraft system or subset of an aircraft system; and(b) after the commencement of the Part 66 Manual of Standards and Part 147 Manual of Standards Amendment Instrument 2023 (No. 1).category B2 modular licence means a category B2 licence granted:(a) under regulation 66.026 of CASR subject to the exclusion of at least 1 aircraft system or subset of an aircraft system; and(b) after the commencement of the Part 66 Manual of Standards and Part 147 Manual of Standards Amendment Instrument 2023 (No. 1).cell, when mentioned for a table, means an individual, undivided unit (regardless of its size) into which a column of the table is subdivided.COA holder means a person who holds a certificate of approval under regulation 30 of CAR 1988.electrical system means the aircraft electrical power supply source, plus the distribution system to the different components contained in the aircraft and relevant connectors. Electrical systems are specified in Table 1 in section 66.A.20. When working on cables (including coaxial cables) and connectors which are part of these electrical systems, the following typical practices are included in the privileges:1. continuity, insulation and bonding techniques and testing;2. crimping and testing of crimped joints;3. connector pin removal and insertion;4. wiring protection techniques.large aircraft has the same meaning as in the CASR Dictionary.lighting systems are part of the electrical system.MEA means manufacturing and engineering assessment.Note MEA is part of a code assigned to each nationally endorsed Australian training package to identify the particular industry the training package covers.modular licence means a category B1 modular licence or a category B2 modular licence.Modular Licence Basic Practical Experience Logbook means the CASA Part 66 Modular Licence Basic Practical Experience Logbook, as it exists from time to time.MTO means maintenance training organisation under Part 147 of CASR 1998.non-rated aircraft has the same meaning as in paragraph (b) of the definition of aircraft type in regulation 66.010 of CASR 1998.powerplant means an aircraft engine.practical consolidation training (PCT) means a practical training course:1. conducted by a maintenance training organisation in accordance with section 66.A.50 and Appendix III; and2. that is approved in writing by CASA.Note In considering whether to approve a PCT course, CASA will take into account whether the course elements reflect the elements of a best practice PCT program as described in Advisory Circular 147-1 Practical Consolidation Training.recognition of prior learning (RPL) for licence category training, aircraft type training, category A aircraft task training and foreign or military qualifications under Part 66 of CASR 1998:(a) has the same meaning given by section 147.A.07 of the Part 147 Manual of Standards (as amended); and(b) may be prescribed by CASA, a Part 147 Maintenance Training Organisation (MTO) or a Part 145 Approved Maintenance Organisation (AMO).regulation 31 means paragraphs 31 (4) (b), (c) and (e) of CAR 1988, as in force immediately before 27 June 2011, and includes:1. regulation 31C of CAR 1988, as in force immediately before 27 June 2011; and2. each of the following CAOs, as in force immediately before 27 June 2011:(i) CAO 100.91;(ii) CAO 100.92;(iii) CAO 100.93;(iv) CAO 100.94;(v) CAO 100.95; and3. each of the following Specification instruments for an associated CAO, as in force or existing immediately before 27 June 2015:(i) CASA 202/14 for CAO 100.91;(ii) CASA 203/14 for CAO 100.92;(iii) CASA 204/14 for CAO 100.93;(iv) CASA 205/14 for CAO 100.94;(v) CASA 206/14 for CAO 100.95; and4. each of the following Airworthiness Advisory Circulars (AAC) with which its associated CAO was expressed to be read, as it existed immediately before 27 June 2015:(i) AAC Part 9-91 for CAO 100.91;(ii) AAC Part 9-92 for CAO 100.92;(iii) AAC Part 9-93 for CAO 100.93;(iv) AAC part 9-94 for CAO 100.94;(v) AAC Part 9-95 for CAO 100.95.simple test means a test described in maintenance data that meets all of the following criteria:1. the serviceability of the system can be verified using aircraft controls, switches, built-in test equipment (BITE), central maintenance computer (CMC) or external test equipment not involving special training;2. the outcome of the test is a unique go/no-go indication or parameter. No interpretation of the test result or interdependence of different values is allowed.small aircraft has the same meaning as in the CASR Dictionary.subsystem means a system which, while capable of functioning on its own, is part of a larger system and includes, for this MOS:1. the electrical subsystem comprised of electrical parts, appliances and motors, within mechanical, powerplant and structural systems; or2. the instrument subsystem comprised of avionic systems within mechanical, powerplant and structural systems.this MOS means the Part 66 Manual of Standards.troubleshooting means the published approved fault isolation maintenance procedures and actions outlined in maintenance data, used as necessary in order to identify the root cause of a defect or malfunction. It may include the use of BITE or external test equipment. Troubleshooting may involve avionic LRU changes, however, it does not involve multiple avionic LRU changes in pursuit of a system fault, unless the changes are made in accordance with a published approved fault isolation maintenance procedure (e.g. Troubleshooting Manual, Fault Isolation Manual procedure).(c) Unless the contrary intention appears, the term carry out maintenance includes, within its normal meaning, both the supervision of maintenance and carrying out the physical tasks of maintenance.
(a) The maintenance certification and certificate of release to service privileges of each category of licence are as follows:1. A person who holds a Category A licence endorsed with a subcategory may perform maintenance certification for that subcategory maintenance if:(i) the person carried out the maintenance; and(ii) the maintenance is maintenance of a kind mentioned in Appendix II of the Part 145 MOS;2. A person who holds a Category A licence endorsed with a subcategory may issue a certificate of release to service for maintenance if:(i) the maintenance was carried out by the person; or(ii) the maintenance and its maintenance certification were carried out by another person who holds a Category A licence with the appropriate subcategory; and(iii) the maintenance was maintenance of a kind mentioned in Appendix II of the Part 145 MOS; and(iv) the aircraft being maintained is covered by the subcategory of licence held;3. A reference to maintenance in subparagraphs (a) 1 or 2 does not include:(i) supervision of maintenance; or(ii) for a subcategory A1 licence, maintenance of a propeller-driven aeroplane unless the subcategory A1 licence holder:(A) holds a B1.1 subcategory endorsement that permits the holder to perform maintenance certification on the propeller system of a propeller-driven aeroplane; or(B) is positively endorsed in the subcategory A1 to provide such maintenance.4. Subject to paragraph 66.A.45 (b), a person who holds a Category B1 licence endorsed with a subcategory may perform maintenance certification for that subcategory maintenance if:(i) the person carried out the subcategory maintenance; and(ii) the maintenance is any of the following:(A) work on an aircraft system designated in Table 1, as structural, powerplant, mechanical or electrical;(B) unless the licence is specifically subject to an avionics LRU exclusion, replacement of an avionic line replaceable unit that requires only simple tests to prove its serviceability;(BA) updating the software in an avionic system, provided that:(I) the system has a discrete test facility to confirm the success of the updating; and(II) the serviceability of any other system affected by the updating is also confirmed; and(III) only simple tests are necessary to verify the serviceability of the system and any other system affected by the updating;(C) category A licence tasks of a kind mentioned in Appendix II of the Part 145 MOS for the aircraft type rating or ratings held(D) functional checks of avionic systems that can be conducted as a simple test;(E) troubleshooting of avionic systems that can be conducted as a simple test;(F) as a daily, or manufacturer’s equivalent, inspection, or as an extended diversion time operation (EDTO) pre-flight inspection;(G) scheduled routine inspection of fibre-reinforced plastic composite structures — but not including an inspection in which specialised equipment is used, or in which repairs to the composite structure are carried out;(H) inspection using an NDT method — but only if limited to liquid penetrant inspection using aerosol-packed materials; and(iii) subject to subparagraph 4A, the maintenance is not of an aircraft system or subset that is excluded from the licence.4A. For sub-sub-subparagraph 66.A.20 (a) 4. (ii) (F), despite any exclusions annotated on a licence, a daily or manufacturers’ equivalent inspection also includes:(i) check of the condition and security of attachment of wiring, plumbing, parts and appliances; and(ii) maintenance of instrument, or electrical, parts and appliances forming part of the powerplant, mechanical or structural system, limited to:(A) external mechanical adjustments to facilitate correct operation of powerplant or mechanical or structural systems; and(B) replacement of instrument, or electrical, parts and appliances, connected by simple twist or terminal connectors — excluding instrument, or electrical parts and appliances, where maintenance involves functional tests and adjustments requiring the use of external specialised test equipment.5. A person who holds a Category B1 licence endorsed with a subcategory may issue a certificate of release to service for aircraft covered by a subcategory endorsed on the licence, after maintenance of the aircraft, if the maintenance was not base maintenance carried out on a large aircraft;5A. A person who:(i) on or before 30 June 2021, satisfied the requirements of each of repealed paragraphs 66.A.25 (i), 66.A.30 (f), and 66.A.45 (j) of this MOS; andNote Repealed paragraphs 66.A.25 (i), 66.A.30 (f) and 66.A.45 (j) were repealed by the Part 66 Manual of Standards Instrument 2024 (No. 1).(ii) but for the repeal of regulation 31 would, thereby, have qualified for the issue of an aircraft maintenance engineer licence with the former engine category Group 1 or Group 2 rating, or the former airframe category Group 1, 2 or 19 rating; and(iii) on this basis, was issued with a Category B1 licence;may perform maintenance certifications and issue certificates of release to service for the following maintenance:(iv) all electrical maintenance on an aircraft fitted with a single generator and approved for V.F.R. operations only;(v) all instrument system maintenance for aircraft general instruments (but excluding RMI, inertial navigation and multi-axis autopilots) on an aircraft approved for V.F.R. operations only;(vi) periodic inspections for aircraft radio systems on an aircraft approved for V.F.R. operations only.6. A person who holds a Category B2 licence may perform maintenance certification for Category B2 maintenance carried out on an aircraft if:(i) the person carried out the maintenance; and(ii) the maintenance was carried out:(A) on an aircraft system designated in Table 1 as avionic or electrical; or(B) on an instrument or electrical sub system of an aircraft system designated in Table 1 as structural, powerplant or mechanical; or(C) as a category A licence task of a kind mentioned in Appendix II of the Part 145 MOS within the limits of tasks specifically endorsed on the certification authorisation referred to in subparagraph 145.A.35 (b) 1 of the Part 145 MOS. This certification privilege is restricted to work that the licence holder has personally performed in the maintenance organisation which issued the certification authorisation and is limited to the type ratings for a large aircraft endorsed in the B2 licence; or(D) to replace an avionic line replaceable unit that only requires simple tests to prove its serviceability, unless the licence is specifically subject to an avionics LRU exclusion; or(E) as a daily, or manufacturer’s equivalent, inspection, or as an extended diversion time operation (EDTO) pre-flight inspection; and(iii) subject to subparagraph 6A, the maintenance was not of an aircraft system or subset that is excluded from the licence.6A. For sub-sub-subparagraph 66.A.20 (a) 6. (ii) (E), despite any exclusions annotated on a licence, a daily or manufacturers’ equivalent inspection also includes:(i) check of the condition and security of attachment of wiring, plumbing, parts and appliances; and(ii) maintenance of instrument, or electrical, parts and appliances forming part of the powerplant, mechanical or structural system, limited to:(A) external mechanical adjustments to facilitate correct operation of powerplant or mechanical or structural systems; and(B) replacement of instrument, or electrical, parts and appliances, connected by simple twist or terminal connectors — excluding instrument, or electrical parts and appliances, where maintenance involves functional tests and adjustments requiring the use of external specialised test equipment.7. A person who holds a Category B2 licence may issue a certificate of release to service for aircraft covered by the licence if the maintenance was not base maintenance carried out on a large aircraft;8. A person who holds a Category C licence may issue a certificate of release to service for base maintenance carried out on a large aircraft for the aircraft in its entirety, if:(i) the maintenance was carried out on a large aircraft; and(ii) the Category C holder’s licence is endorsed with the type rating for the large aircraft.Table 1Aircraft systems, designations and conditions for Category B1 and Category B2 licencesAircraft system (and ATA chapter reference) | Designation of system | Conditions or limitationsPressurisation, air-conditioning and equipment cooling systems (ATA21) | Mechanical (B1) | For a Category B2 licence, pressurisation control systems.Autopilot (ATA22) | Avionic (B2)Communications (ATA23), including ELT and underwater locating beacon (ATA25-60) | Avionic (B2)Generator and/or constant speed drive/IDG systems (ATA24) | Electrical (B1/B2) and Powerplant (B1)Electrical power supply systems, including a ram air turbine, if electrical (ATA24) | Electrical(B1 and B2)Equipment, furnishings and emergency equipment (ATA25) | Mechanical (B1) | Except ELT and underwater locating beacon (ATA 25-60) — see (ATA23).Fire, smoke, overheat detecting and extinguishing systems (ATA26) | Mechanical (B1)Flight control systems (ATA27) | Mechanical (B1) | For a category B1 licence — except system operation – fly-by-wire.Flight control systems – system operation – fly-by-wire (ATA27) | Avionic (B2) | For a Category B2 licence — limited to the avionic subsystem of the flight control system.Fuel systems (ATA28) | Mechanical (B1)Hydraulic power systems, including ram air turbine (ATA29) | Mechanical (B1)Ice and rain protection systems (ATA30) | Mechanical (B1)Ice and rain protection systems (ATA30-20) | Mechanical and Powerplant (B1) | Powerplant — for powerplant cowling anti-icing.Indicating and recording systems (ATA31) | Avionic (B2)Landing gear (ATA32) | Mechanical (B1)Wheels and brakes (ATA32-40) | Mechanical (B1)Lighting (ATA33) | Electrical (B1 and B2)Navigation systems:GeneralRadio interfaceACARS, SELCAL, INS/IRSCompassFlight manage-ment systemDoppler systems(ATA34)Avionic (B2)For a Category B1 licence — compass swings, if endorsed on the licence.Oxygen system (ATA35) | Mechanical (B1) | For a Category B2 licence, if endorsed on the licence.Pneumatic system (ATA36) | Mechanical (B1)Vacuum (ATA37) | Mechanical (B1)Waste water (ATA38) | Mechanical (B1)Integrated modular avionics (ATA42) | Avionic (B2)Cabin systems(ATA44) | Avionic (B2)Central maintenance system (ATA45) | Avionic (B2)Information systemsATIMSNetwork server(ATA46)Avionic (B2)Nitrogen generation system or inert gas system (ATA47) | Mechanical (B1)APU (ATA49) | Powerplant (B1)Cargo and accessory compartments (ATA50) | Mechanical (B1)Structures — General (ATA51)Structural (B1)Structures — general, but excluding wooden structures and fabric surfaces unless:(a) for wooden structures — the holder has obtained the relevant optional units of competency mentioned in section 66.A.25 of this MOS; orNote These optional units of competency are marked W in Appendix IV.(b) for fabric surfaces — the holder has obtained the relevant optional units of competency mentioned in section 66.A.25 of this MOS.Note These optional units of competency are marked Z in Appendix IV.Structures — general(c) for a category B2 licence — closing of cowlings and refitment of quick access inspection panels.Doors (ATA52) | Structural (B1)Fuselage (ATA53) | Structural (B1)Nacelles and pylons (ATA54) | Structural (B1)Stabilisers (ATA55) | Structural (B1)Windows (ATA56) | Structural (B1)Wings (ATA57) | Structural (B1)Propeller — rotor (ATA60) | Mechanical (B1)Propeller — propulsion (ATA61)Powerplant (B1)For a Category B1 licence, only if the holder has obtained the relevant optional units of competency mentioned in section 66.A.25 of this MOS.Note These optional units of competency are marked P in Appendix IV.Rotor (ATA62) | Mechanical (B1)Rotor drives (ATA63) | Mechanical (B1)Tail rotor (ATA64) | Mechanical (B1)Tail rotor drive (ATA65) | Mechanical (B1)Folding blades and pylon (ATA66) | Mechanical (B1)Rotor flight control (ATA67) | Mechanical (B1)Powerplant (ATA71) | Powerplant (B1)Engine turbine/turbo-prop and fans (ATA72) | Powerplant (B1)Engine-mounted accessories: gear boxes, gears, pumps and attached engine-mounted and driven components(ATA72-60) | Powerplant (B1)Engine fuel and control — carbura-tion/injection system (ATA73) | Powerplant (B1)FADEC (ATA73A) | Avionic (B2)Ignition system (ATA74) | Powerplant (B1)Air systems and control (ATA75) | Powerplant (B1)Engine control system (ATA76) | Powerplant (B1)Engine indicating system (ATA77) | Powerplant (B1) and Avionic (B2)Exhaust — thrust reverser (ATA78) | Powerplant (B1)Lubrication system (ATA79) | Powerplant (B1)Starting system (ATA80) | Powerplant (B1)Supercharging system (ATA81) | Powerplant (B1)Power augmentation (ATA82) | Powerplant (B1)Accessory drives (ATA83) | Powerplant (B1)
(a) This section sets out the basic knowledge and competency requirements that must be met by a person who applies for:1. an aircraft engineer licence in a category or subcategory; or2. the addition of a category or subcategory to the person’s licence other than a modular licence; or3. if the licence is a modular licence, the removal of at least 1 exclusion from the licence in order to obtain a category or subcategory on the licence, or an extension of licence privileges.(b) If the application is in relation to a Category A licence, or Category B1 or Category B2 licence other than a modular licence, or for the addition of a subcategory to a licence, the applicant must demonstrate, by examination conducted by CASA or an MTO:1. knowledge of each module, applicable for the category or subcategory, in accordance with Part 2 of Appendix I; and2. the level of knowledge for each sub-module, applicable for the category or subcategory, in accordance with Part 3 of Appendix I.(ba) If the application is in relation to a modular licence, or for the removal of at least 1 exclusion in order to obtain a category or subcategory on, or extension of privileges of, a modular licence, the applicant must demonstrate, by examination conducted by CASA or an MTO:1. knowledge of each module or sub-module, applicable for the category or subcategory, and any extension, in accordance with Part 2A of Appendix I; and2. the level of knowledge for each sub-module, applicable for the category or subcategory, in accordance with Part 3 of Appendix I.(c) The level of knowledge mentioned in subparagraphs (b) 2. and (ba) 2. must be demonstrated to the examination standard mentioned in Appendix II.(d) Subject to paragraph (db), paragraph (da) applies if:1. the applicant does not hold a Category B1 or B2 licence; and2. the application is for a Category C licence.(da) The applicant must demonstrate, by examination conducted by CASA or an MTO, the same matters mentioned in paragraph (b) and to the same examination standard mentioned in paragraph (c), as if the application is in relation to a Category B1 or B2 licence.(db) Paragraph (da) does not apply if the applicant holds an academic degree mentioned in subparagraph (h) 1.(e) The knowledge mentioned in paragraphs (b) and (ba) may be gained by:1. the training of the applicant by an MTO; or2. self-study by the applicant.(ea) The applicant must have undertaken the training or self-study mentioned in paragraph (e), and passed the examinations for the modules mentioned in paragraph (b), during the 10-year period before the date of the application.(eb) Subject to paragraph (ec), if the applicant was trained by an MTO, the applicant must hold each unit of competency listed and coded in Appendix IV that is marked “X”, or stated to be its equivalent, for the relevant category or subcategory of aircraft engineer licence.(ec) If the application is for a modular licence and the applicant was trained by an MTO, the applicant must hold each unit of competency relevant to the modular licence, including with any extension of privileges, that is listed and coded in Appendix X that is marked “X”, or stated to be its equivalent, for the relevant category or subcategory of modular licence, including any extension.(ed) For paragraphs (eb) and (ec), stated to be its equivalent means published on the national register of vocational education and training (VET) website at <training.gov.au> as the current unit that supersedes and is equivalent to the unit listed and coded in the Appendix mentioned in the paragraph.Note CASA updates Appendix IV or Appendix X, as applicable, as soon as possible to include the new numbering and title of the current unit published on the <training.gov.au> website.(f) Subject to paragraph (fa), in addition to the units of competency that are required under this section for a subcategory B1.1 or B1.2 licence, an applicant for the privilege that includes wooden structures or fabric surfaces or propellers, who was trained by an MTO, must hold each relevant optional unit of competency listed and coded in Appendix IV to this MOS that is marked:1. W — for wooden structures for the subcategory; and2. Z — for fabric surfaces for the subcategory; and3. P — for propellers for the subcategory.(fa) If an applicant who was trained by an MTO applies for the privilege that includes wooden structures or fabric surfaces or propellers, and the application relates to a subcategory B1.1 or B1.2 modular licence, the applicant must hold, in addition to the units of competency required under this section for the relevant subcategory of the modular licence, each relevant optional unit of competency listed and coded in Appendix X that is marked:1. W — for wooden structures for the subcategory; and2. Z — for fabric surfaces for the subcategory; and3. P — for propellers for the subcategory.(g) A person may be taken to hold the necessary qualifications or units of competency as set out above if an MTO has conducted a recognition of prior learning assessment in accordance with that MTO’s course plan and exposition.(h) The academic qualifications required to satisfy the basic knowledge requirements for grant of a category C licence are:1. an academic degree (as a minimum, a 3 year bachelor of technology degree) in an aeronautical, mechanical, structural, electrical, electronic or avionics discipline obtained from a university or other higher educational institution recognised by CASA.(i) An applicant for removal of an exclusion of an aircraft system or subset from a category or subcategory of aircraft engineer licence, who is being trained by an MTO, must complete the units of competency mentioned in Appendix VIII for removal of the exclusion, via training conducted by the MTO, before the exclusion is removed.
(a) An applicant for an aircraft engineer licence must have acquired the following practical experience:1. for a Category A, or subcategory B1.2 or B1.4, licence:(i) 3 years’ practical maintenance experience on operating aircraft, if the applicant has not undertaken any relevant technical training; orNote See AMC/GM for CASR Part 66 for information about what is relevant technical training for this sub-subparagraph.(ii) 2 years’ practical maintenance experience on operating aircraft, and completion of relevant training as a skilled worker in a technical trade; orNote See AMC/GM for CASR Part 66 for information about what is relevant training for this sub-subparagraph.(iii) 1 year’s practical maintenance experience on operating aircraft, and completion of a category training course conducted by an MTO.2. for a Category B2, or subcategory B1.1 or B1.3, licence:(i) 5 years’ practical maintenance experience on operating aircraft, if the applicant has not undertaken any relevant technical training; orNote See AMC/GM for CASR Part 66 for information about what is relevant technical training for this sub-subparagraph.(ii) 3 years’ practical maintenance experience on operating aircraft, and completion of relevant training as a skilled worker in a technical trade; orNote See AMC/GM for CASR Part 66 for information about what is relevant training for this sub-subparagraph.(iii) 2 years’ practical maintenance experience on operating aircraft, and completion of a category training course conducted by an MTO.3. for a Category C licence:(i) 3 years’ experience exercising Category B1.1, B1.3 or B2 privileges on large aircraft; or(ii) 5 years’ experience exercising Category B1.2 or B1.4 privileges on large aircraft; or(iii) for an applicant holding an academic degree mentioned in subparagraph 66.A.25 (h) 1. — 3 years’ experience working in a civil aircraft maintenance environment on a representative selection of tasks directly associated with aircraft maintenance, including at least 6 months of observation of base maintenance tasks.Note See AMC/GM for CASR Part 66 for information about what is a representative selection of tasks for this sub-subparagraph.4. for an initial modular licence:(i) 2 years’ practical maintenance experience on operating aircraft; and(ii) completion of category training, conducted by an MTO, that is relevant to the initial modular licence, or completion of the knowledge applicable for the category or subcategory of licence, in accordance with Part 2A of Appendix I, via self-study, in which case the applicant must record in the Modular Licence Basic Practical Experience Logbook evidence of their acquisition of the practical maintenance experience required under sub-subparagraph (i) for the licence.Note The Modular Licence Basic Practical Experience Logbook and the Part 66 Modular Licence – Basic Practical Experience Logbook User Guide are available on the CASA website at <www.casa.gov.au>. As at commencement of this subparagraph:the Modular Licence Basic Practical Experience Logbook was available at: <Part 66 Modular Licence Basic Practical Experience Logbook (casa.gov.au)>the User Guide was available at: <Part 66 Modular Licence – Basic Practical Experience Logbook User Guide (casa.gov.au)>.Note Subparagraphs 1. to 3. do not apply to applications for modular licences.(aa) For a Category A licence, a subcategory B1.1, B1.2, B1.3 or B1.4 licence (other than a modular licence) or a Category B2 licence (other than a modular licence), if the knowledge applicable for the category or subcategory of licence, in accordance with Part 2 of Appendix I, is being completed via self-study, the applicant must record in the Basic Practical Experience Logbook evidence of their acquisition of the practical maintenance experience required under subparagraph 66.A.30 (a) 1. or 2. for the licence.Note The Basic Practical Experience Logbook and the Part 66 Basic Practical Experience Logbook User Guide are available on the CASA website at <www.casa.gov.au>.(b) Subject to paragraph (d), if a person who holds an aircraft engineer licence (other than a modular licence) applies to CASA to add a category (other than Category C), or subcategory, to the licence, the person must have gained the minimum period of practical maintenance experience, for the category or subcategory, on operating aircraft in accordance with Table 3.Table 3Practical maintenance experience requirements for adding a category, or subcategory, to an aircraft engineer licenceTo | A1 | A2 | A3 | A4 | B1.1 | B1.2 | B1.3 | B1.4 | B2FromA1 | – | 6 months | 6 months | 6 months | 2 years | 6 months | 2 years | 1 year | 2 yearsA2 | 6 months | – | 6 months | 6 months | 2 years | 6 months | 2 years | 1 year | 2 yearsA3 | 6 months | 6 months | – | 6 months | 2 years | 1 year | 2 years | 6 months | 2 yearsA4 | 6 months | 6 months | 6 months | – | 2 years | 1 year | 2 years | 6 months | 2 yearsB1.1 | None | 6 months | 6 months | 6 months | – | 6 months | 6 months | 6 months | 1 yearB1.2 | 6 months | None | 6 months | 6 months | 2 years | – | 2 years | 6 months | 2 yearsB1.3 | 6 months | 6 months | None | 6 months | 6 months | 6 months | – | 6 months | 1 yearB1.4 | 6 months | 6 months | 6 months | None | 2 years | 6 months | 2 years | – | 2 yearsB2 | 6 months | 6 months | 6 months | 6 months | 1 year | 1 year | 1 year | 1 year | –(ba) For regulation 11.068 of CASR, it is a condition of an aircraft engineer licence that, if the licence is a modular licence and the licence holder applies to CASA for removal of at least 1 exclusion of an aircraft system or subset from the licence in order to obtain a category or subcategory on the licence, or an extension of licence privileges, the person must have, in accordance with Table 3A:1. gained the minimum period of practical maintenance experience, applicable for the category or subcategory, or extension, on operating aircraft; or2. if the applicant is completing the knowledge applicable for the category or subcategory via self-study — completed the task list if no minimum period of practical maintenance experience, applicable for the category or subcategory, or extension, is specified.Note As at the commencement of this paragraph, CASA must also receive evidence from an MTO that the holder has successfully completed the training and assessment that is required for the aircraft system or subset under section 66.A.25 for the exclusion to be removed — see section 66.072 of CASR.Table 3APractical maintenance experience requirements to obtain a category or subcategory on a modular licenceToB1.1, B1.2 Aeroplane (Airframe)B1.3, B1.4 Helicopter(Airframe)B1.1, B1.3 Power plant (Turbine)B1.2, B1.4 Power plant(Piston)B1 PropellerB1 Electrical and Instrument systems ExtensionB2 Electrical systemsB2 Instrument systemsB2 Radio systemsFromB1.1, B1.2 Aeroplane (Airframe) | — | Task list(see Note 1) | 1 year | 1 year(see Note 3) | — | 1 year(see Note 3) | 1 year | 1 year | 1 yearB1.3, B1.4 Helicopter (Airframe)Task List(see Note 1)—1 year1 year(see Note 3)—1 year(see Note 3)1 year1 year1 yearB1.1, B1.3 Power plant(Turbine)1 year1 year—task list(see Note 2)task list(see Note 4)1 year1 year1 year1 yearB1.2, B1.4 Powerplant(Piston)1 year1 yeartask list(see Note 2)——1 year1 year1 year1 yearB2 Electrical systems | 1 year | 1 year | 1 year | 1 year | — | — | — | 1 year | 1 yearB2Instrument systems1 year1 year1 year1 year——1 year—1 yearB2 Radio systems | 1 year | 1 year | 1 year | 1 year | — | — | 1 year | 1 year | —In Table 3A:task list means the sections of the Modular Licence Basic Practical Experience Logbook that set out maintenance tasks relevant to the aircraft system or subset for which the category or subcategory is to be obtained.Note 1 This is a rule. If one airframe licence is held, the addition of the second airframe licence only requires completion of the task list.Note 2 This is a rule. If one engine licence is held, addition of the second engine licence only requires completion of the task list.Note 3 The one-year period of electrical and instrument systems experience and piston engine experience may be accumulated concurrently.Note 4 This is a rule. Propeller is an option for a B1.1 licence only. Completion of the task list is required for maintenance of turbopropeller aeroplanes.(c) The experience mentioned in paragraphs (b) and (ba) must have been gained from a representative cross-section of maintenance tasks on operating aircraft relevant to the category or subcategory.Note See AMC/GM for CASR Part 66 for information about what is a representative cross-section of maintenance tasks for this paragraph.(d) The minimum period of experience mentioned in paragraph (b) is reduced by 50% if the applicant has completed a training course, relevant to the category or subcategory, conducted by an MTO.(e) At least 1 year of the experience mentioned in paragraph (a) must be recent experience gained on aircraft relevant to the category, or subcategory, of the initial licence applied for.Note See AMC/GM for CASR Part 66 for information about what is recent experience for this paragraph.(ea) Subject to paragraph (d):1. at least 3 months of the experience mentioned in paragraph (b) must be recent experience gained on aircraft relevant to the category, or subcategory, of licence sought to be added; and2. at least 3 months of the experience mentioned in paragraph (ba) must be recent experience gained on aircraft relevant to the category or subcategory, or extension of privileges, of licence sought to be obtained.Note See AMC/GM for CASR Part 66 for information about what is recent experience for this paragraph.(eb) Aircraft maintenance experience gained outside a civil aircraft maintenance environment is taken to be practical maintenance experience for paragraph (a) if an MTO certifies, in writing, to CASA that:1. the experience gained is equivalent to the practical maintenance experience; and2. the applicant has adequate additional practical maintenance experience on civil aircraft to ensure an adequate understanding of the civil aircraft maintenance environment.(ec) The experience mentioned in:1. subparagraphs (a) 1., 2. or 3., or paragraph (b) must have been gained by the applicant during the 10-year period before the date of the application for the licence or the addition of the category, or subcategory, to the licence; and2. subparagraph (a) 4. or paragraph (ba) must have been gained during the 10-year period before the date of application for the initial modular licence or the removal of an exclusion to obtain the category or subcategory on the modular licence, or extension of privileges.
(a) The holder of a Category A licence may only exercise certification privileges on a specific aircraft type following the satisfactory completion of the relevant Category A aircraft task training carried out by an appropriately approved AMO or MTO, which must include:1. practical hands on training and theoretical training as appropriate for each task authorised; and2. satisfactory completion of training demonstrated by an examination and/or by workplace assessment carried out by an AMO or MTO authorised to conduct such training.(b) The holder of a subcategory B1.1, B1.2, B1.3, B1.4, or Category B2, licence may exercise his or her certification privileges on a non-rated aircraft when the licence is endorsed with the appropriate category or subcategory for the maintenance required for that non-rated aircraft.Note The holder of a subcategory B1.1, B1.2, B1.3, B1.4, or Category B2, licence does not require a type rating to exercise his or her certification privileges on aircraft systems other than the powerplant systems of:(i) a large aircraft with a particular type of aircraft engine; or(ii) a small aircraft with a particular type of aircraft engine.(ba) The holder of a subcategory B1.1, B1.2, B1.3, B1.4, or Category B2 or C, licence must only exercise his or her certification privileges on a particular type, or type and model, of a large aircraft with a particular type of aircraft engine when the licence is endorsed with the appropriate aircraft type rating by CASA.Note These are aircraft referred to in paragraph (a) of regulation 66.010 of CASR 1998 definition of aircraft type.(bb) The holder of a subcategory B1.1, B1.2, B1.3 or B1.4 licence must only exercise his or her certification privileges on the powerplant systems of:1. a large aircraft with a particular type of aircraft engine; or2. a small aircraft with a particular type of aircraft engine;when the licence is endorsed with the appropriate aircraft type rating by CASA.Note These are aircraft referred to in paragraphs (b) and (c) of regulation 66.010 of CASR 1998 definition of aircraft type.(c) A type rating may only be issued by CASA:1. following satisfactory completion of the relevant Category B1, B2 or C aircraft type training:(i) approved by CASA; or(ii) conducted by an appropriately approved MTO; or(iii) conducted in accordance with paragraph (h); or2. if each of the following applies:(i) the applicant is a category B2 licence holder (the holder) with a rating (a type rating) for a particular type, or type and model, of large aircraft with a particular type of aircraft engine (a large aircraft type);(ii) the holder applies for a rating (the different type rating) for a large aircraft type, that is different from his or her type rating;(iii) the large aircraft type to which the different type rating would apply has the same manufacturer as the large aircraft type to which the holder’s type rating applies;(iv) CASA carries out an RPL assessment that compares the differences between the large aircraft type to which the type rating applies and the large aircraft type to which the different type rating would apply;(v) CASA determines that the B2 systems differences between the 2 large aircraft types are not such as to require further training of the holder for the issue of the different type rating.3. if each of the following applies:(i) the applicant is a category B1 licence holder (the holder) with a rating (a type rating) for a particular type, or type and model, of large aircraft with a particular type of aircraft engine (a large aircraft type);(ii) the holder applies for a rating (the different type rating) for a large aircraft type, that is different from his or her type rating;(iii) the large aircraft type to which the different type rating would apply has the same manufacturer as the large aircraft type to which the holder’s type rating applies;(iv) CASA carries out an RPL assessment that compares the differences between the large aircraft type to which the type rating applies and the large aircraft type to which the different type rating would apply;(v) CASA determines that the B1 engine (powerplant) interface differences between the 2 large aircraft types are not such as to require further training of the holder for the issue of the different type rating.Note In subparagraphs (c) 2 and (c) 3, a large aircraft type means, in accordance with paragraphs (a) and (b) of the definition of aircraft type in regulation 66.010 of CASR 1998:(a) a particular type, or type and model, of large aircraft with a particular type of aircraft engine; or(b) a large aircraft with a particular type of aircraft engine.(d) An applicant for a Category B1 or B2 aircraft type rating must complete the applicable type training in relation to paragraph 66.A.20 (a) privileges, which consists of:1. theoretical training and examination; and2. practical training and assessment as specified in sections 66.A.50 and 66.A.55.(e) Category C approved type training must comply with the requirements for such training in Appendix III to this MOS. In the case of a Category C licence holder qualified by holding an academic degree mentioned in subparagraph 66.A.25 (h) 1., the first aircraft type theoretical training must be at the Category B1 or B2 licence level. Practical training is not required.(f) Completion of approved aircraft type training, as required by paragraphs (b) to (c), must be demonstrated by an examination. The examination must comply with the requirements in Appendix III to this MOS.(g) The training and assessment for a restricted rating for an aircraft type may be in:1. a subset of the theoretical elements mentioned in Part 2 of Appendix III that are indicated for the category or subcategory by the numerical level of the type training; and2. the corresponding practical elements mentioned in Part 3 of Appendix III that are appropriate for the category or subcategory and the rating, only if the MTO provides in the course plan for the training a description of:(i) the training and assessment in the subset of theoretical elements and its corresponding practical elements; and(ii) the persons eligible to undertake the training and assessment; and(iii) the restrictions for the rating to which the training and assessment relates; and(iv) ensures that all documents required under this MOS in connection with the training and assessment, describe the rating as a restricted rating.(h) An AMO in accordance with section 145.A.37 of the Part 145 MOS, or a COA holder in accordance with Civil Aviation Order 104.0 (Certificates of approval — application, grant and conditions) (a CAR 30 organisation), may:1. deliver excluded system training and assessment for the excluded systems set out in Appendix VII; or2. for an aircraft type mentioned in column 2 of Table 2 in Appendix IX — deliver aircraft type training for a category or subcategory of licence for the aircraft, or a system or subsystem of the aircraft type; or3. for an aircraft type mentioned in column 2 of Table 2 in Appendix IX — arrange for the manufacturer of the aircraft or its engine to provide training and assessment.(i) A licensed aircraft maintenance engineer, seeking his or her first aircraft type rating in an alternate licence category or subcategory not currently held by that person, must have first completed category or subcategory basic knowledge and competency training as mentioned in section 66.A.25 for the issue of a licence in that category or subcategory for which he or she is seeking his or her first rating, as well as meeting the practical maintenance experience requirements specified in paragraph 66.A.30 (b).
Level of knowledge for the categoryA | B1 | B22.1 Matter | 1 | 1 | 1Nature of matter: the chemical elements, structure of atoms, molecules;Chemical compounds;States: solid, liquid and gaseous;Changes between states.2.2 Mechanics2.2.1 Statics | 1 | 2 | 1Forces, moments and couples, representation as vectors;Centre of gravity;Elements of theory of stress, strain and elasticity: tension, compression, shear and torsion;Nature and properties of solid, fluid and gas;Pressure and buoyancy in liquids (barometers).2.2.2 Kinetics | 1 | 2 | 1Linear movement: uniform motion in a straight line, motion under constant acceleration (motion under gravity);Rotational movement: uniform circular motion (centrifugal and centripetal forces);Periodic motion: pendular movement;Simple theory of vibration, harmonics and resonance;Velocity ratio, mechanical advantage and efficiency.2.2.3 Dynamics(a) | 1 | 2 | 1Mass;Force, inertia, work, power, energy (potential, kinetic and total energy), heat, efficiency;(b) | 1 | 2 | 2Momentum, conservation of momentum;Impulse;Gyroscopic principles;Friction: nature and effects, coefficient of friction (rolling resistance).2.2.4 Fluid dynamics(a) | 2 | 2 | 2Specific gravity and density;(b) | 1 | 2 | 1Viscosity, fluid resistance, effects of streamlining;Effects of compressibility on fluids;Static, dynamic and total pressure: Bernoulli’s Theorem, venturi.2.3 Thermodynamics(a) | 2 | 2 | 2Temperature: thermometers and temperature scales: Celsius, Fahrenheit and Kelvin, heat definition;(b) | — | 2 | 2Heat capacity, specific heat;Heat transfer: convection, radiation and conduction;Volumetric expansion;First and second law of thermodynamics;Gases: ideal gases laws, specific heat at constant volume and constant pressure, work done by expanding gas;Isothermal, adiabatic expansion and compression, engine cycles, constant volume and constant pressure, refrigerators and heat pumps;Latent heats of fusion and evaporation, thermal energy, heat of combustion.2.4 Optics (light) | — | 2 | 2Nature of light, speed of light;Laws of reflection and refraction: reflection at plane surfaces, reflection by spherical mirrors, refraction, lenses;Fiberoptics.2.5 Wave motion and sound | — | 2 | 2Wave motion: mechanical waves, sinusoidal wave motion, interference phenomena, standing waves;Sound: speed of sound, production of sound, intensity, pitch and quality, Doppler effect.
Level of knowledge for the categoryA | B1 | B23.1 Electron theory | 1 | 1 | 1Structure and distribution of electrical charges within atoms, molecules, ions, compounds;Molecular structure of conductors, semiconductors and insulators.3.2 Static electricity and conduction | 1 | 2 | 2Static 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 vacuum.3.3 Electrical terminology | 1 | 2 | 2The 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 | 1Production of electricity by the following methods: light, heat, friction, pressure, chemical action, magnetism and motion.3.5 DC sources of electricity | 1 | 2 | 2Construction and basic chemical action of: primary cells, secondary cells, lead acid cells, nickel cadmium cells, other Alkaline cells;Cells connected in series and parallel;Internal resistance and its effect on a battery;Construction, materials and operation of thermocouples;Operation of photo-cells.3.6 DC circuits | — | 2 | 2Ohms Law, Kirchoff’s Voltage and Current Laws;Calculations using the above laws to find resistance, voltage and current;Significance of the internal resistance of a supply.3.7 Resistance and resistor(a) | — | 2 | 2Resistance and affecting factors;Specific resistance;Resistor colour code, values and tolerances, preferred values, wattage ratings;Resistors in series and parallel;Calculation of total resistance using series parallel and series parallel combinations;Operation and use of potentiometers and rheostats;Operation of Wheatstone Bridge;(b) | — | 1 | 1Positive and negative temperature coefficient conductance;Fixed resistors, stability, tolerance and limitations, methods of construction;Variable resistors, thermistors, voltage dependent resistors;Construction of potentiometers and rheostats;Construction of Wheatstone Bridge.3.8 Power | — | 2 | 2Power, work and energy (kinetic and potential);Dissipation of power by a resistor;Power formula;Calculations involving power, work and energy.3.9 Capacitance and capacitor | — | 2 | 2Operation and function of a capacitor;Factors affecting capacitance area of plates, distance between plates, number of plates, dielectric and dielectric constant, working voltage, voltage rating;Capacitor types, construction and function;Capacitor colour coding;Calculations of capacitance and voltage in series and parallel circuits;Exponential charge and discharge of a capacitor, time constants;Testing of capacitors.3.10 Magnetism(a) | — | 2 | 2Theory of magnetism;Properties of a magnet;Action of a magnet suspended in the Earth’s magnetic field;Magnetisation and demagnetisation;Magnetic shielding;Various types of magnetic material;Electromagnets construction and principles of operation;Hand clasp rules to determine: magnetic field around current carrying conductor.(b) | — | 2 | 2Magneto-motive force, field strength, magnetic flux density, permeability, hysteresis loop, retentivity, coercive force reluctance, saturation point, eddy currents;Precautions for care and storage of magnets.3.11 Inductance and inductor | — | 2 | 2Faraday’s Law;Action of inducing a voltage in a conductor moving in a magnetic field;Induction principles;Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of change of flux, number of conductor turns;Mutual induction;The effect the rate of change of primary current and mutual inductance has on induced voltage;Factors affecting mutual inductance: number of turns in coil, physical size of coil, permeability of coil, position of coils with respect to each other;Lenz’s Law and polarity determining rules;Back emf, self-induction;Saturation point;Principal uses of inductors.3.12 DC motor and generator theory | — | 2 | 2Basic motor and generator theory;Construction and purpose of components in DC generator;Operation of, and factors affecting output and direction of, current flow in DC generators;Operation of, and factors affecting output power, torque, speed and direction of rotation of DC motors;Series wound, shunt wound and compound motors;Starter generator construction.3.13 AC theory | 1 | 2 | 2Sinusoidal 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 and square waves;Single and 3 phase principles.3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits | — | 2 | 2Phase 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 | 2Transformer construction principles and operation;Transformer losses and methods for overcoming them;Transformer action under load and no-load conditions;Power transfer, efficiency, polarity markings;Calculation of line and phase voltages and currents;Calculation of power in a 3 phase system;Primary and secondary current, voltage, turns ratio, power, efficiency;Autotransformers.3.16 Filters | — | 1 | 1Operation, application and uses of the following filters: low pass, high pass, band pass, band stop.3.17 AC generators | — | 2 | 2Rotation of loop in a magnetic field and waveform produced;Operation and construction of revolving armature and revolving field type AC generators;Single phase, 2 phase and 3 phase alternators;Three phase star and delta connections advantages and uses;Permanent magnet generators.3.18 AC motors | — | 2 | 2Construction, principles of operation and characteristics of:AC synchronous and induction motors both single and polyphase;Methods of speed control and direction of rotation;Methods of producing a rotating field: capacitor, inductor, shaded or split pole.
Level of knowledge for the categoryA | B1 | B24.1 Semiconductors4.1.1 Diodes(a) | — | 2 | 2Diode symbols;Diode characteristics and properties;Diodes in series and parallel;Main characteristics and use of silicon controlled rectifiers (thyristors), light emitting diode, photo conductive diode, varistor, rectifier diodes;Functional testing of diodes;(b) | — | — | 2Materials, electron configuration, electrical properties;P and N type materials: effects of impurities on conduction, majority and minority characters;PN junction in a semiconductor, development of a potential across a PN junction in unbiased, forward biased and reverse biased conditions;Diode parameters: peak inverse voltage, maximum forward current, temperature, frequency, leakage current, power dissipation;Operation and function of diodes in the following circuits: clippers, clampers, full and half wave rectifiers, bridge rectifiers, voltage doublers and triplers;Detailed operation and characteristics of the following devices: silicon controlled rectifier (thyristor), light emitting diode, Shottky diode, photoconductive diode, varactor diode, varistor, rectifier diodes, Zener diode.4.1.2 Transistors(a) | — | 1 | 2Transistor symbols;Component description and orientation;Transistor characteristics and properties;(b) | — | — | 2Construction and operation of PNP and NPN transistors;Base, collector and emitter configurations;Testing of transistors;Basic appreciation of other transistor types and their uses;Application of transistors: classes of amplifier (A, B, C);Simple circuits including: bias, decoupling, feedback and stabilisation;Multistage circuit principles: cascades, push-pull, oscillators, multivibrators, flip-flop circuits.4.1.3 Integrated circuits(a) | — | 1 | —Description and operation of logic circuits and linear circuits and operational amplifiers;(b) | — | — | 2Description and operation of logic circuits and linear circuits;Introduction to operation and function of an operational amplifier used as: integrator, differentiator, voltage follower, comparator;Operation and amplifier stages connecting methods: resistive capacitive, inductive (transformer), inductive resistive (IR), direct;Advantages and disadvantages of positive and negative feedback.4.2 Printed circuit boards | — | 1 | 2Description and use of printed circuit boards.4.3 Servomechanisms(a) | — | 1 | —Understanding of the following terms: open and closed loop systems, feedback, follow up, analogue transducers;Principles of operation and use of the following synchro system components and features: resolvers, differential, control and torque, transformers, inductance and capacitance transmitters;(b) | — | — | 2Understanding of the following terms: open and closed loop, follow up, servomechanism, analogue, transducer, null, damping, feedback, dead band;Construction operation and use of the following synchro system components: resolvers, differential, control and torque, E and I transformers, inductance transmitters, capacitance transmitters, synchronous transmitters;Servo mechanism defects, reversal of synchro leads, hunting.
Level of knowledge for the categoryA | B1 | B26.1 Aircraft materials ferrous(a) | 1 | 2 | 1Characteristics, properties and identification of common alloy steels used in aircraft;Heat treatment and application of alloy steels;(b) | — | 1 | 1Testing of ferrous materials for hardness, tensile strength, fatigue strength and impact resistance.6.2 Aircraft materials — non-ferrous(a) | 1 | 2 | 1Characteristics, properties and identification of common non-ferrous materials used in aircraft;Heat treatment and application of non-ferrous materials;(b) | — | 1 | 1Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance.6.3 Aircraft materials — composite and non-metallic6.3.1 Composite and non-metallic other than wood and fabric(a) | 1 | 2 | 2Characteristics, properties and identification of common composite and non-metallic materials, other than wood, used in aircraft;Sealant and bonding agents;(b) | 1 | 2 | —The detection of defects and deterioration in composite and non-metallic material;Repair of composite and non-metallic material.6.3.2 Wooden structures | 1 | 2 | —Construction methods of wooden airframe structures;Characteristics, properties and types of wood and glue used in aeroplanes;Preservation and maintenance of wooden structure;Types of defects in wood material and wooden structures;The detection of defects in wooden structure;Repair of wooden structure.6.3.3 Fabric covering | 1 | 2 | —Characteristics, properties and types of fabrics used in aeroplanes;Inspections methods for fabric;Types of defects in fabric;Repair of fabric covering.6.4 Corrosion(a) | 1 | 1 | 1Chemical fundamentals;Formation by galvanic action process, microbiological, stress;(b) | 2 | 3 | 2Types of corrosion and their identification;Causes of corrosion;Material types, susceptibility to corrosion.6.5 Fasteners6.5.1 Screw threads | 2 | 2 | 2Screw nomenclature;Thread forms, dimensions and tolerances for standard threads used in aircraft;Measuring screw threads;6.5.2 Bolts, studs and screws | 2 | 2 | 2Bolt 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 | 2Tab and spring washers, locking plates, split pins, pal-nuts, wire locking, quick release fasteners, keys, circlips, cotter pins.6.5.4 Aircraft rivets | 1 | 2 | 1Types of solid and blind rivets: specifications and identification, heat treatment.6.6 Pipes and unions(a) | 2 | 2 | 2Identification of, and types of, rigid and flexible pipes and their connectors used in aircraft;(b) | 2 | 2 | 1Standard unions for aircraft hydraulic, fuel, oil, pneumatic and air system pipes.6.7 Springs | — | 2 | 1Types of springs, materials, characteristics and applications.6.8 Bearings | 1 | 2 | 2Purpose of bearings, loads, material, construction;Types of bearings and their application.6.9 Transmissions | 1 | 2 | 2Gear 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 | 1Types of cables;End fittings, turn buckles and compensation devices;Pulleys and cable system components;Bowden cables;Aircraft flexible control systems.6.11 Electrical cables and connectors | 1 | 2 | 2Cable types, construction and characteristics;High tension and co-axial cables;Crimping;Connector types, pins, plugs, sockets, insulators, current and voltage rating, coupling, identification codes.
Level of knowledge for the categoryA | B1 | B27.1 Safety precautions — aircraft and workshop | 3 | 3 | 3Aspects of safe working practices including precautions to take when working with electricity, gases especially oxygen, oils and chemicals;Instruction in the remedial action to be taken in the event of a fire or another accident with one or more of these hazards including knowledge on extinguishing agents.7.2 Workshop practices | 3 | 3 | 3Care of tools, control of tools, use of workshop materials;Dimensions, allowances and tolerances, standards of workmanship;Calibration of tools and equipment, calibration standards.7.3 Tools | 3 | 3 | 3Common hand tool types;Common power tool types;Operation and use of precision measuring tools;Lubrication equipment and methods;Operation, function and use of electrical general test equipment.7.4 Avionic general test equipment | — | 2 | 3Operation, function and use of avionic general test equipment.7.5 Engineering drawings, diagrams and standards | 1 | 2 | 2Drawing types and diagrams, their symbols, dimensions, tolerances and projections;Identifying title block information;Microfilm, microfiche and computerised presentations;Specification 100 of the ATA;Aeronautical and other applicable standards including ISO, AN, MS, NAS and MIL;Wiring diagrams and schematic diagrams.7.6 Fits and clearances | 1 | 2 | 1Drill sizes for bolt holes, classes of fits;Common system of 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 | 3Continuity, insulation and bonding techniques and testing;Use of crimp tools: hand and hydraulic operated;Testing of crimp joints;Connector pin removal and insertion;Co-axial cables: testing and installation precautions;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;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 and 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 of 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 handling7.14.1 Sheet Metal | — | 2 | —Marking out, and calculation of, bend allowance;Sheet metal working including bending and forming;Inspection of sheet metal work.7.14.2 Composite and non-metallic | — | 2 | —Bonding practices;Environmental conditions;Inspection methods.7.15 Welding, brazing, soldering and bonding(a) | — | 2 | 2Soldering methods, inspection of soldered joints;(b) | — | 2 | —Welding and brazing methods;Inspection of welded and brazed joints;Bonding methods and inspection of bonded joints.7.16 Aircraft weight and balance(a) | — | 2 | 2Centre of gravity and balance limits calculation: use of relevant documents;(b) | — | 2 | —Preparation of aircraft for weighing;Aircraft weighing.7.17 Aircraft handling and storage | 2 | 2 | 2Aircraft taxiing and towing and associated safety precautions;Aircraft jacking, chocking, securing and associated safety precautions;Aircraft storage methods;Refuelling and defuelling procedures;De-icing and 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) | 2 | 3 | 2Types of defects and visual inspection techniques;Corrosion removal, assessment and reprotection;(b) | — | 2 | —General repair methods, Structural Repair Manual;Ageing, fatigue and corrosion control programs;(c) | — | 2 | 1Non-destructive inspection techniques including: penetrant, radiographic, eddy current, ultrasonic and borescope methods;(d) | 2 | 2 | 2Disassembly and re-assembly techniques;(e) | — | 2 | 2Trouble shooting techniques.7.19 Abnormal events(a) | 2 | 2 | 2Inspections following lightning strikes and HIRF penetration.(b) | 2 | 2 | —Inspections following abnormal events such as heavy landings and flight through turbulence.7.20 Maintenance procedures | 1 | 2 | 2Maintenance planning;Modification procedures;Stores procedures;Certification and release procedures;Interface with aircraft operation;Maintenance inspection, quality control and quality assurance;Additional maintenance procedures;Control of life limited components.
Level of knowledge for the categoryA1 | B1.1 | B211.1 Theory of flight | —11.1.1 Aeroplane aerodynamics and flight controls | 1 | 2Operation, and effect, of the following:roll control: ailerons and spoilerspitch control: elevators, stabilators, variable incidence stabilisers and canardsyaw control, rudder limiters;Control using elevons, ruddervators;High-lift devices, slots, slats, flaps, flaperons;Drag-inducing devices, spoilers, lift dumpers, speed brakes;Effects of wing fences, sawtooth leading edges;Boundary layer control, using vortex generators, stall wedges or leading-edge devices;Operation and effect of trim tabs, balance and anti-balance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels.11.1.2 High-speed flight | 1 | 2 | —Speed of sound, subsonic flight, transonic flight, supersonic flight;Mach number, critical Mach number, compressibility buffet, shockwave, aerodynamic heating, area rule;Factors affecting airflow in engine intakes of high-speed aircraft;Effects of sweepback on critical Mach number.11.2 Airframe structures — general concepts(a) | 2 | 2 | —Airworthiness requirements for structural strength;Structural classification, primary, secondary and tertiary;Fail-safe, safe-life and damage-tolerance concepts;Zonal and station identification systems;Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;Drains and ventilation provisions;System installation provisions;Lightning-strike protection provision;Aircraft bonding;(b) | 1 | 2 | —Construction methods of stressed-skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive protection, wing, empennage and engine attachments;Structure assembly techniques: riveting, bolting, bonding;Methods of surface protection, such as chromating, anodising, painting;Surface cleaning;Airframe symmetry: methods of alignment and symmetry checks.11.3 Airframe structures — aeroplanes11.3.1 Fuselage (ATA52/53/56) | 1 | 2 | —Construction and pressurisation sealing;Wing, stabiliser, pylon and undercarriage attachments;Seat installation and cargo loading system;Doors and emergency exits: construction, mechanisms, operation and safety devices;Windows and windscreen construction and mechanisms.11.3.2 Wings (ATA57) | 1 | 2 | —Construction;Fuel storage;Landing gear, pylon, control surface and high-lift/drag attachments.11.3.3 Stabilisers (ATA55) | 1 | 2 | —Construction;Control surface attachment.11.3.4 Flight control surfaces (ATA55/57) | 1 | 2 | —Construction and attachment;Balancing — mass and aerodynamic.11.3.5 Nacelles and pylons (ATA54) | 1 | 2 | —Construction;Firewalls;Engine mounts.11.4 Air-conditioning and cabin pressurisation (ATA21)11.4.1 Air supply | 1 | 2 | —Sources of air supply, including engine bleed, APU and ground cart.11.4.2 Air-conditioning | 1 | 3 | —Air-conditioning systems;Air cycle and vapour cycle machines;Distribution systems;Flow, temperature and humidity control system.11.4.3 Pressurisation | 1 | 3 | —Pressurisation systems;Control and indication, including control and safety valves;Cabin pressure controllers.11.4.4 Safety and warning devices | 1 | 3 | —Protection and warning devices.11.5 Instruments and avionic systems11.5.1 Instrument systems (ATA31) | 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;Angle of attack indication, stall warning systems;Glass cockpit;Other aircraft system indication.11.5.2 Avionic systems | 1 | 1 | —Fundamentals of system layouts, and operation of the following:Auto flight (ATA22)Communications (ATA23)Navigation systems (ATA34).11.6 Electrical power (ATA24) | 1 | 3 | —Batteries installation and operation;DC-power generation;AC-power generation;Emergency-power generation;Voltage regulation;Power distribution;Inverters, transformers, rectifiers;Circuit protection;External/ground power.11.7 Equipment and furnishings (ATA25)(a) | 2 | 2 | —Emergency equipment requirements;Seats, harnesses and belts;(b) | 1 | 1 | —Cabin layout;Equipment layout;Cabin furnishing installation;Cabin entertainment equipment;Galley installation;Cargo handling and retention equipment;Airstairs.11.8 Fire protection (ATA26)(a) | 1 | 3 | —Fire and smoke detection and warning systems;Fire extinguishing systems;System tests;(b) | 1 | 2 | —Portable fire extinguisher.11.9 Flight controls (ATA27) | 1 | 3 | —Primary controls: aileron, elevator, rudder, spoiler;Trim control;Active load control;High-lift devices;Lift dump, speed brakes;System operation: manual, hydraulic, pneumatic, electrical, fly-by-wire;Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks systems;Balancing and rigging;Stall protection/warning system.11.10 Fuel systems (ATA28) | 1 | 3 | —System layout;Fuel tanks;Supply systems;Dumping, venting and draining;Cross-feed and transfer;Indications and warnings;Refuelling and defuelling;Longitudinal balance fuel systems.11.11 Hydraulic power (ATA29) | 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.11.12 Ice and rain protection (ATA30) | 1 | 3 | —Ice formation, classification and detection;Anti-icing systems: electrical, hot air and chemical;De-icing systems: electrical, hot air, pneumatic and chemical;Rain repellent;Probe and drain heating;Wiper systems.11.13 Landing gear (ATA32) | 2 | 3 | —Construction, shock absorbing;Extension and retraction systems: normal and emergency;Indications and warning;Wheels, brakes, antiskid and autobraking;Tyres;Steering;Air-ground sensing.11.14 Lights (ATA33) | 2 | 3 | —External: navigation, anti-collision, landing, taxiing, ice;Internal: cabin, cockpit, cargo;Emergency.11.15 Oxygen (ATA35) | 1 | 3 | —System layout: cockpit, cabin;Sources, storage, charging and distribution;Supply regulation;Indications and warnings.11.16 Pneumatic/vacuum (ATA36) | 1 | 3 | —System layout;Sources: engine/APU, compressors, reservoirs, ground supply;Pressure and vacuum pumps;Pressure control;Distribution;Indications and warnings;Interfaces with other systems.11.17 Water/waste (ATA38) | 2 | 3 | —Water system layout, supply, distribution, servicing and draining;Toilet system layout, flushing and servicing;Corrosion aspects.11.18 On-board maintenance systems (ATA45) | 1 | 2 | —Central maintenance computers;Data-loading system;Electronic library system;Printing;Structure monitoring (damage-tolerance monitoring).11.19 Integrated modular avionics (ATA42) | 1 | 2 | —Functions that may be typically integrated in the Integrated modular avionics (IMA) modules include: 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;Core system;Network components.11.20 Cabin systems (ATA44) | 1 | 2 | —The units and components which furnish a means of entertaining the passengers and providing communication within the aircraft (cabin intercommunication data system (CIDS)), and between the aircraft cabin and ground stations (cabin network service (CNS)). These include voice, data, music and video transmissions.The CIDS provides an interface between cockpit/cabin crew and cabin systems. These systems support data exchange of the different related Line Replaceable Units (LRUs) and they are typically operated via Flight Attendant Panels (FAPs).The CNS is typically on a server, interfacing with systems, including the following:data/radio communicationcabin 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 the following:access to pre-departure/departure reportsemail/intranet/internet accesspassenger database.11.21 Information systems (ATA46) | 1 | 2 | —The units and components which furnish a means of storing, updating and retrieving digital information, traditionally provided on paper, microfilm or microfiche. These 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 the following:air traffic and information management systemsnetwork server systemsaircraft general information systemflight deck information systemmaintenance information systempassenger cabin information systemmiscellaneous information system.
Note The scope of this module must reflect the technology of aeroplanes relevant to a subcategory A2, or B1.2, aircraft engineer licence.Level of knowledge for the categoryA2 | B1.2 | B211.1 Theory of flight | —11.1.1 Aeroplane aerodynamics and flight controls | 1 | 2Operation and effect of the following:roll control: ailerons and spoilerspitch control: elevators, stabilators, variable incidence stabilisers and canardsyaw control, rudder limiters;Control using elevons, ruddervators;High-lift devices, slots, slats, flaps, flaperons;Drag-inducing devices, spoilers, lift dumpers, speed brakes;Effects of wing fences, sawtooth leading edges;Boundary layer control, using vortex generators, stall wedges or leading-edge devices;Operation and effect of trim tabs, balance and anti-balance (leading) tabs, servo tabs, spring tabs, mass balance, control surface bias, aerodynamic balance panels.11.1.2 High-speed flight – N/A | — | — | —11.2 Airframe structures — general concepts(a) | 2 | 2 | —Airworthiness requirements for structural strength;Structural classification, primary, secondary and tertiary;Fail-safe, safe-life and damage-tolerance concepts;Zonal and station identification systems;Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;Drains and ventilation provisions;System installation provisions;Lightning-strike protection provision;Aircraft bonding;(b) | 1 | 2 | —Construction methods of stressed-skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive protection, wing, empennage and engine attachments;Structure assembly techniques: riveting, bolting, bonding;Methods of surface protection, such as chromating, anodising, painting;Surface cleaning;Airframe symmetry: methods of alignment and symmetry checks.11.3 Airframe structures — aeroplanes11.3.1 Fuselage (ATA52/53/56) | 1 | 2 | —Construction and pressurisation sealing;Wing, tailplane, pylon and undercarriage attachments;Seat installation;Doors and emergency exits: construction and operation;Windows and windscreen attachment.11.3.2 Wings (ATA57) | 1 | 2 | —Construction;Fuel storage;Landing gear, pylon, control surface and high-lift/drag attachments.11.3.3 Stabilisers (ATA55) | 1 | 2 | —Construction;Control surface attachment.11.3.4 Flight control surfaces (ATA55/57) | 1 | 2 | —Construction and attachment;Balancing — mass and aerodynamic.11.3.5 Nacelles and pylons (ATA54) | 1 | 2 | —Construction;FirewallsEngine mounts.11.4 Air-conditioning and cabin pressurisation (ATA21) | 1 | 3 | —Pressurisation and air-conditioning systems;Cabin pressure controllers;Protection and warning devices;Heating systems.11.5 Instruments and avionic systems11.5.1 Instrument systems (ATA31) | 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;Angle of attack indication, stall warning systems;Glass cockpit;Other aircraft system indication.11.5.2 Avionic systems | 1 | 1 | —Fundamentals of system layouts, and operation of the following:auto flight (ATA22)communications (ATA23)navigation systems (ATA34).11.6 Electrical power (ATA24) | 1 | 3 | —Batteries installation and operation;DC-power generation;Voltage regulation;Power distribution;Circuit protection;Inverters, transformers.11.7 Equipment and furnishings (ATA25)(a) | 2 | 2 | —Emergency equipment requirements;Seats, harnesses and belts;(b) | 1 | 1 | —Cabin layout;Equipment layout;Cabin furnishing installation;Cabin entertainment equipment;Galley installation;Cargo handling and retention equipment;Airstairs.11.8 Fire protection (ATA26)(a) | 1 | 3 | —Fire and smoke detection and warning systems;Fire extinguishing systems;System tests;(b) | 1 | 2 | —Portable fire extinguisher.11.9 Flight controls (ATA27) | 1 | 3 | —Primary controls: aileron, elevator, rudder;Trim tabs;High-lift devices;System operation: manual;Gust locks;Balancing and rigging;Stall warning system.11.10 Fuel systems (ATA28) | 1 | 3 | —System layout;Fuel tanks;Supply systems;Cross-feed and transfer;Indications and warnings;Refuelling and defuelling.11.11 Hydraulic power (ATA29) | 1 | 3 | —System layout;Hydraulic fluids;Hydraulic reservoirs and accumulators;Pressure generation: electric, mechanical;Filters;Pressure control;Power distribution;Indication and warning systems.11.12 Ice and rain protection (ATA30) | 1 | 3 | —Ice formation, classification and detection;De-icing systems: electrical, hot air, pneumatic and chemical;Probe and drain heating;Wiper systems.11.13 Landing gear (ATA32) | 2 | 3 | —Construction, shock absorbing;Extension and retraction systems: normal and emergency;Indications and warning;Wheels, brakes, antiskid and autobraking;Tyres;Steering;Air-ground sensing.11.14 Lights (ATA33) | 2 | 3 | —External: navigation, anti-collision, landing, taxiing, ice;Internal: cabin, cockpit, cargo;Emergency.11.15 Oxygen (ATA35) | 1 | 3 | —System layout: cockpit, cabin;Sources, storage, charging and distribution;Supply regulation;Indications and warnings.11.16 Pneumatic and vacuum (ATA36) | 1 | 3 | —System layout;Sources: engine/APU, compressors, reservoirs, ground supply;Pressure and vacuum pumps;Pressure control;Distribution;Indications and warnings;Interfaces with other systems.11.17 Water and waste (ATA38) | 2 | 3 | —Water system layout, supply, distribution, servicing and draining;Toilet system layout, flushing and servicing;Corrosion aspects.
Level of knowledge for the categoryA3A4B1.3B1.4B212.1 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 settling, overpitching;Auto-rotation;Ground effect.12.2 Flight control systems | 2 | 3 | —Cyclic control;Collective control;Swashplate;Yaw control: Anti-torque control, tail rotor, bleed air;Main rotor head: design and operation features;Blade dampers: function and construction;Rotor blades: main and tail rotor blade construction and attachment;Trim control, fixed and adjustable stabilisers;System operation: manual, hydraulic, electrical and fly-by-wire;Artificial feel;Balancing and rigging.12.3 Blade tracking and vibration analysis | 1 | 3 | —Rotor alignment;Main and tail rotor tracking;Static and dynamic balancing;Vibration types, vibration reduction methods;Ground resonance.12.4 Transmission | 1 | 3 | —Gearboxes, main and tail rotors;Clutches, freewheel units and rotor brake;Tail rotor drive shafts, flexible couplings, bearings, vibration dampers and bearing hangers.12.5 Airframe structures(a) | 2 | 2 | —Airworthiness requirements for structural strength;Structural classification, primary, secondary and tertiary;Fail safe, safe life, damage tolerance concepts;Zonal and station identification systems;Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;Drains and ventilation provisions;System installation provisions;Lightning strike protection provision;(b) | 1 | 2 | —Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads, frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning and anti-corrosive protection;Pylon, stabiliser and undercarriage attachments;Seat installation;Doors: construction, mechanisms, operation and safety devices;Windows and windscreen construction;Fuel storage;Firewalls;Engine mounts;Structure assembly techniques: riveting, bolting, bonding;Methods of surface protection, such as chromating, anodising, painting;Surface cleaning;Airframe symmetry: methods of alignment and symmetry checks.12.6 Air-conditioning (ATA21)12.6.1 Air supply | 1 | 2 | —Sources of air supply including engine bleed and ground cart.12.6.2 Air-conditioningAir-conditioning systems;Distribution systems;Flow and temperature control systems;Protection and warning devices.13—12.7 Instruments and avionic systems12.7.1 Instrument systems (ATA31) | 1 | 2 | —Pitot static: altimeter, air speed indicator, vertical speed indicator;Gyroscopic: artificial horizon, attitude director, direction indicator, horizontal situation indicator, turn and slip indicator, turn coordinator;Compasses: direct reading, remote reading;Vibration indicating systems — HUMS;Glass cockpit;Other aircraft system indication.12.7.2 Avionic systems | 1 | 1 | —Fundamentals of system layouts and operation of:Auto flight (ATA22);Communications (ATA23);Navigation Systems (ATA34).12.8 Electrical power (ATA24) | 1 | 3 | —Batteries installation and operation;DC power generation, AC power generation;Emergency power generation;Voltage regulation, circuit protection;Power distribution;Inverters, transformers, rectifiers;External and ground power.12.9 Equipment and furnishings (ATA25)(a) | 2 | 2 | —Emergency equipment requirements;Seats, harnesses and belts;Lifting systems;(b) | 1 | 1 | —Emergency flotation systems;Cabin layout, cargo retention;Equipment layout;Cabin furnishing installation.12.10 Fire protection (ATA26) | 1 | 3 | —Fire and smoke detection and warning systems;Fire extinguishing systems;System tests.12.11 Fuel systems (ATA28) | 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 (ATA29) | 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.12.13 Ice and rain protection (ATA30) | 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 (ATA32) | 2 | 3 | —Construction, shock absorbing;Extension and retraction systems: normal and emergency;Indications and warning;Wheels, tyres, brakes;Steering;Air-ground sensing;Skids, floats.12.15 Lights (ATA33) | 2 | 3 | —External: navigation, landing, taxiing, ice;Internal: cabin, cockpit, cargo; emergency.12.16 Pneumatic and vacuum (ATA36) | 1 | 3 | —System layout;Sources: engine, compressors, reservoirs, ground supply;Pressure control;Distribution;Indication sand warnings;Interfaces with other systems.12.17 Integrated modular avionics (ATA42) | 1 | 2 | —Functions that may be typically integrated in the integrated modular avionics (IMA) modules include: 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;Core system;Network components.12.18 On-board maintenance systems (ATA45) | 1 | 2 | —Central maintenance computers;Data loading system;Electronic library system;Printing;Structure monitoring (damage tolerance monitoring).12.19 Information systems (ATA46) | 1 | 2 | —The units and components which furnish a means of storing, updating and retrieving digital information, traditionally provided on paper, microfilm or microfiche. These include units that are dedicated to the information storage and retrieval function such as the electronic library mass storage and controller. These 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; network server system; aircraft general information system; flight deck information system; maintenance information system; passenger cabin information system; miscellaneous information system.
Level of knowledge for the categoryA | B1 | B213.1 Theory of flight(a) Aeroplane aerodynamics and flight controls | — | — | 1Operation and effect of:roll control: ailerons and spoilers;pitch control: elevators, stabilators, variable incidence stabilisers and canards;yaw control, rudder limiters;Control using elevons, ruddervators;Highlift devices: slots, slats, flaps;Drag inducing devices: spoilers, lift dumpers, speed brakes;Operation and effect of trim tabs, servo tabs, control surface bias;(b) High speed flight | — | — | 1Speed of sound, subsonic flight, transonic flight, supersonic flight, Mach number, critical Mach number;(c) Rotary wing aerodynamics | — | — | 1Terminology;Operation and effect of cyclic, collective and anti-torque controls.13.2 Structures — general concepts(a) | — | — | 1Fundamentals of structural systems;(b) | — | — | 2Zonal and station identification systems; electrical bonding;Lightning strike protection provision.13.3 Autoflight (ATA22) | — | — | 3Fundamentals of automatic flight control including working principles and current terminology;Command signal processing;Modes of operation: roll, pitch and yaw channels;Yaw dampers;Stability augmentation system in helicopters;Automatic trim control;Autopilot navigation aids interface;Autothrottle systems;Automatic landing systems: principles and categories, modes of operation, approach, glide slope, land, go-around, system monitors and failure conditions.13.4 Communication and navigation (ATA23/34) | — | — | 3Fundamentals of radio wave propagation, antennas, transmission lines, communication, receiver and transmitter.Working principles of following systems:Very high frequency (VHF) communication;High frequency (HF) communication;Audio;Emergency locator transmitters;Cockpit voice recorder;Very high frequency omnidirectional range (VOR);Automatic direction finding (ADF);Instrument landing system (ILS);Microwave landing system (MLS);Flight director systems; Distance measuring equipment (DME);Doppler navigation;Area navigation, RNAV systems;Flight management systems;Global positioning system (GPS), Global navigation satellite systems (GNSS);Inertial navigation system;Air traffic control transponder, secondary surveillance radar;Traffic alert and collision avoidance system (TCAS);Weather avoidance radar;Radio altimeter;ARINC communication and reporting.13.5 Electrical power (ATA24) | — | — | 3Batteries installation and operation;DC power generation;AC power generation;Emergency power generation;Voltage regulation;Power distribution;Inverters, transformers, rectifiers;Circuit protection;External and ground power.13.6 Equipment and furnishings (ATA25) | — | — | 3Electronic emergency equipment requirements;Cabin entertainment equipment.13.7 Flight controls (ATA27)(a) | — | — | 2Primary controls: aileron, elevator, rudder, spoiler;Trim control;Active load control;High lift devices;Lift dump, speed brakes;System operation: manual, hydraulic, pneumatic;Artificial feel, Yaw damper, Mach trim, rudder limiter, gust locks;Stall protection systems;(b) | — | — | 3System operation: electrical, fly-by-wire.13.8 Instruments (ATA31) | — | — | 3Classification;Atmosphere;Terminology;Pressure measuring devices and systems;Pitot static systems;Altimeters;Vertical speed indicators;Airspeed indicators;Machmeters;Altitude reporting and alerting systems;Air data computers;Instrument pneumatic systems;Direct reading pressure and temperature gauges;Temperature indicating systems;Fuel quantity indicating systems;Gyroscopic principles;Artificial horizons;Slip indicators;Directional gyros;Ground proximity warning systems;Compass systems;Flight data recording systems;Electronic flight instrument systems;Instrument warning systems including master warning systems and centralised warning panels;Stall warning systems and angle of attack indicating systems;Vibration measurement and indication;Glass cockpit.13.9 Lights (ATA33) | — | — | 3External: navigation, landing, taxiing, ice;Internal: cabin, cockpit, cargo;Emergency.13.10 On-board maintenance systems (ATA45) | — | — | 3Central maintenance computers;Data loading system;Electronic library system;Printing;Structure monitoring (damage tolerance monitoring).13.11 Air-conditioning and cabin pressurisation (ATA21)13.11.1 Air supply | — | — | 2Sources of air supply including engine bleed, APU and ground cart.13.11.2 Air-conditioningAir-conditioning systems;Air cycle and vapour cycle machines;Distribution systems;Flow, temperature and humidity control system.————————231313.11.3 Pressurisation | — | — | 3Pressurisation systems;Control and indication including control and safety valves;Cabin pressure controllers.13.11.4 Safety and warning devices | — | — | 3Protection and warning devices.13.12 Fire protection (ATA26)(a)Fire and smoke detection and warning systems;Fire extinguishing systems;System tests;——3(b)Portable fire extinguisher.——113.13 Fuel systems (ATA28)System layout;Fuel tanks;Supply systems;Dumping, venting and draining;Cross-feed and transfer;Indications and warnings;Refuelling and defuelling;Longitudinal balance fuel systems.————————————————1111232313.14 Hydraulic power (ATA29)System layout;Hydraulic fluids;Hydraulic reservoirs and accumulators;Pressure generation: electrical, mechanical, pneumatic;Emergency pressure generation;Filters;Pressure control;Power distribution;Indication and warning systems;Interface with other systems.————————————————————111331313313.15 Ice and rain protection (ATA30) | — | — | —Ice formation, classification and detection;Anti-icing systems: electrical, hot air and chemical;De-icing systems: electrical, hot air, pneumatic and chemical;Rain repellent;Probe and drain heating;Wiper systems.————————————22313113.16 Landing gear (ATA32)Construction, shock absorbing;Extension and retraction systems: normal and emergency;Indications and warnings;Wheels, brakes, antiskid and autobraking;Tyres;Steering;Air-ground sensing.——————————————133313313.17 Oxygen (ATA35)System layout: cockpit, cabin;Sources, storage, charging and distribution;Supply regulation;Indications and warnings.————————333313.18 Pneumatic/vacuum (ATA36)System layout;Sources: engine/APU, compressors, reservoirs, ground supply;Pressure control;Distribution;Indications and warnings;Interfaces with other systems.————————————22313313.19 Water/waste (ATA38) | — | — | 2Water system layout, supply, distribution, servicing and draining;Toilet system layout, flushing and servicing.13.20 Integrated modular avionics (ATA42) | — | — | 3Functions 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;Core system;Network components.13.21 Cabin systems (ATA44) | — | — | 3The units and components which furnish a means of entertaining the passengers and providing communication within the aircraft (cabin intercommunication data system) and between the aircraft cabin and ground stations (cabin network service). These include voice, data, music and video transmissions.The cabin intercommunication data system provides an interface between cockpit/cabin crew and cabin systems. These systems support data exchange of the different related LRUs and they are typically operated via flight attendant panels.The cabin network service typically consists on a server, typically interfacing with, among others, the following systems: data/radio communication, in-flight entertainment system.The cabin network service may host functions such as:access to pre-departure/departure reportse-mail/intranet/internet accesspassenger databasecabin core systemin-flight entertainment systemexternal communication systemcabin monitoring systemcabin mass memory systemmiscellaneous cabin system.13.22 Information systems (ATA46) | — | — | 3The units and components which furnish a means of storing, updating and retrieving digital information traditionally provided on paper, microfilm or microfiche. These include units that are dedicated to the information storage and retrieval function such as the electronic library mass storage and controller. These 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; network server systems; aircraft general information system; flight deck information system; maintenance information system; passenger cabin information system; miscellaneous information system.
Level of knowledge for the categoryA | B1 | B215.1 Fundamentals | 1 | 2 | —Potential energy, kinetic energy, Newton’s laws of motion, Brayton cycle;The relationship between force, work, power, energy, velocity, acceleration;Constructional arrangement and operation of turbojet, turbofan, turbo shaft, turboprop.15.2 Engine performance | — | 2 | —Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption;Engine efficiencies;By-pass ratio and engine pressure ratio;Pressure, temperature and velocity of the gas flow;Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations.15.3 Inlet | 2 | 2 | —Compressor inlet ducts;Effects of various inlet configurations;Ice protection.15.4 Compressors | 1 | 2 | —Axial and centrifugal types;Constructional features and operating principles and applications;Fan balancing;Operation;Causes and effects of compressor stall and surge;Methods of airflow control: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades;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;Fuel additives;Safety precautions.15.10 Lubrication systems | 1 | 2 | —System operation and layout and components.15.11 Fuel systems | 1 | 2 | —Operation of engine control and fuel metering systems including: electronic engine control (FADEC), systems layout and components.15.12 Air systems | 1 | 2 | —Operation of engine air distribution and anti-ice control systems, including internal cooling, sealing and external air services.15.13 Starting and ignition systemsOperation of engine start systems and components;Ignition systems and components;Maintenance safety requirements.12—15.14 Engine indication systemsExhaust gas temperature and 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.12—15.15 Power augmentation systems | — | 1 | —Operation and applications;Water injection, water methanol;Afterburner systems.15.16 Turbo-prop engines | 1 | 2 | —Gas coupled and free turbine and gear coupled turbines;Reduction gears;Integrated engine and propeller controls;Over speed safety devices.15.17 Turbo-shaft engines | 1 | 2 | —Arrangements drive systems, reduction gearing, couplings, control systems.15.18 Auxiliary power units (APUs) | 1 | 2 | —Purpose, operation, protective systems.15.19 Powerplant installation | 1 | 2 | —Configuration of fire walls, cowlings, acoustic panels engine mounts, anti-vibration mounts, hoses, pipes, feeders, connectors, wiring looms, control cables and rods, lifting points and drains.15.20 Fire protection systems | 1 | 2 | —Operation of detection and 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 engine manufacturer;Compressor washing and cleaning;Foreign object damage.15.22 Engine storage and preservation | — | 2 | —Preservation and depreservation for the engine and accessories and systems.
Basic knowledge examination standard1 General1.1 All basic examinations must be carried out using the multi-choice question format and essay questions as specified below. The incorrect alternatives must seem equally plausible to anyone ignorant of the subject. All of the alternatives should be clearly related to the question and of similar vocabulary, grammatical construction and length. In numerical questions, the incorrect answers should correspond to procedural errors such as corrections applied in the wrong sense or incorrect unit conversions: they must not be mere random numbers.1.2 Each multi-choice question must have 3 alternative answers of which only 1 must be the correct answer and the candidate must be allowed a time per module which is based upon a nominal average of 75 seconds per question.1.3 Each essay question requires the preparation of a written answer and the candidate must be allowed 20 minutes to answer each such question.1.4 Suitable essay questions must be drafted and evaluated using the knowledge syllabus in Appendix I, Modules 7, 9 and 10.1.5 Each question will have a model answer drafted for it, which will also include any known alternative answers that may be relevant for other subdivisions.1.6 The model answer will also be broken down into a list of important points known as Key Points.1.7 The pass mark for each module, or sub-module, multi-choice part of the examination is 75%.1.8 The pass mark for each essay question is 75% in that the candidate’s answer must contain 75% of the required key points addressed by the question and no significant error related to any required key point.1.9 If either the multi-choice part or the essay part is failed, then it is only necessary to retake the multi-choice or essay part, as appropriate.1.10 Penalty marking systems must not be used to determine whether a candidate has passed.1.11 A module examination that a candidate has failed for the first time may be retaken by the candidate at any time after the date of the candidate’s first attempt of the module examination.1.11A A module examination that a candidate has failed for the second time may not be retaken by the candidate for at least 30 days after the date of the candidate’s second attempt of the module examination.1.11B After a set of 3 failed attempts at a module examination, a candidate may not retake the module examination for at least 6 months after the date of the candidate’s last failed attempt of the module examination.1.11C If clause 1.11B applies and a candidate fails their next attempt of the module examination that was retaken after the “standdown” period of at least 6 months mentioned in clause 1.11B:(a) clause 1.11 applies in relation to the timing of the candidate’s following attempt of the module examination as if it was the candidate’s second attempt of the module examination; and(b) if the candidate fails the module examination attempt mentioned in paragraph (a), clause 1.11A applies to the timing of the candidate’s next attempt of the module examination as if it was the candidate’s third attempt.Note The intent of clause 1.11C is to apply the “timing cycle” set out in clauses 1.11 to 1.11B to each set of 3 failed module examinations.1.12 The period mentioned in paragraph 66.A.25 (ea) for the passing of a module examination does not apply if the examination has been passed by a candidate in relation to another category, or subcategory, of aircraft engineer licence held by the candidate.1.13 After each set of 3 failed attempts by a candidate of a module examination, the candidate must give, after the last of the 3 failed attempts, written notice of the following to the body (an MTO or CASA) to which the candidate applies to sit the examination again:(a) the number, and dates, of attempts by the candidate of the examination;(b) for each examination attempt notified by the candidate — details of the body (an MTO or CASA) that conducted the examination.Note The MTO or CASA, as applicable, is responsible for verifying the number, and dates, of attempts by the candidate of the examination.2 Number of questions for each module2.1 Module 1, Mathematics:Category A – 16 multi-choice and 0 essay questions. Time allowed 20 minutes.Category B1 – 32 multi-choice and 0 essay questions. Time allowed 40 minutes.Category B2 – 32 multi-choice and 0 essay questions. Time allowed 40 minutes.2.2 Module 2, Physics:Category A – 32 multi-choice and 0 essay questions. Time allowed 40 minutes.Category B1 – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.Category B2 – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.2.3 Module 3, Electrical fundamentals:Category A – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B1 – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.Category B2 – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.2.4 Module 4, Electronic fundamentals:Category A – None.Category B1 – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B2 – 40 multi-choice and 0 essay questions. Time allowed 50 minutes.2.5 Module 5, Digital techniques/electronic instrument systems:Category A – 16 multi-choice and 0 essay questions. Time allowed 20 minutes.Subcategories B1.1 and B1.3 – 40 multi-choice and 0 essay questions. Time allowed 50 minutes.Subcategories B1.2 and B1.4 – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B2 – 72 multi-choice and 0 essay questions. Time allowed 90 minutes.2.6 Module 6, Materials and hardware:Category A – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.Category B1 – 72 multi-choice and 0 essay questions. Time allowed 90 minutes.Category B2 – 60 multi-choice and 0 essay questions. Time allowed 75 minutes.2.7 Module 7, Maintenance practices:Category A – 72 multi-choice and 2 essay questions. Time allowed 90 minutes plus 40 minutes.Category B1 – 80 multi-choice and 2 essay questions. Time allowed 100 minutes plus 40 minutes.Category B2 – 60 multi-choice and 2 essay questions. Time allowed 75 minutes plus 40 minutes.2.8 Module 8, Basic aerodynamics:Category A – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B1 – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B2 – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.2.9 Module 9, Human factors:Category A – 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes.Category B1 – 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes.Category B2 – 20 multi-choice and 1 essay question. Time allowed 25 minutes plus 20 minutes.2.10 Module 10, Aviation legislation:Category A – 32 multi-choice and 1 essay question. Time allowed 40 minutes plus 20 minutes.Category B1 – 40 multi-choice and 1 essay question. Time allowed 50 minutes plus 20 minutes.Category B2 – 40 multi-choice and 1 essay question. Time allowed 50 minutes plus 20 minutes.2.11 Module 11A, Turbine aeroplane aerodynamics, structures and systems:Category A – 108 multi-choice and 0 essay questions. Time allowed 135 minutes.Category B1 – 140 multi-choice and 0 essay questions. Time allowed 175 minutes.Category B2 – None.Module 11B, Piston aeroplane aerodynamics, structures and systems:Category A – 72 multi-choice and 0 essay questions. Time allowed 90 minutes.Category B1 – 100 multi-choice and 0 essay questions. Time allowed 125 minutes.Category B2 – None.2.12 Module 12, Helicopter aerodynamics, structures and systems:Category A – 100 multi-choice and 0 essay questions. Time allowed 125 minutes.Category B1 – 128 multi-choice and 0 essay questions. Time allowed 160 minutes.Category B2 – None.2.13 Module 13, Aircraft aerodynamics, structures and systems:Category A – None.Category B1 – None.Category B2 – 180 multi-choice and 0 essay questions. Time allowed 225 minutes. Questions and time allowed may be split into 2 examinations, as appropriate.Category B2 modular – for a category B2 modular licence mentioned in column 1 of an item in the following table, the number of multi-choice questions mentioned in column 2 of the item and the time allowed mentioned in column 3 of the item.TableItemColumn 1Category B2 modular licenceColumn 2Number of multi-choice questionsColumn 3Time allowed (minutes)1ELECTRICAL SYSTEMS(sub-modules 13.1, 13.2, 13.5 to 13.7, 13.9 to 13.16, 13.18, and 13.19).1001252INSTRUMENT SYSTEMS(sub-modules 13.1 to 13.4, 13.7, 13.8, 13.17, 13.20 to 13.22).1201503RADIO SYSTEMS(sub-modules 13.1, 13.2, 13.4, 13.20 to 13.22).60752.14 Module 14, Propulsion:Category A – None.Category B1 – None.Category B2 – 24 multi-choice and 0 essay questions. Time allowed 30 minutes.2.15 Module 15, Gas turbine engine:Category A – 60 multi-choice and 0 essay questions. Time allowed 75 minutes.Category B1 – 92 multi-choice and 0 essay questions. Time allowed 115 minutes.Category B2 – None.2.16 Module 16, Piston engine:Category A – 52 multi-choice and 0 essay questions. Time allowed 65 minutes.Category B1 – 72 multi-choice and 0 essay questions. Time allowed 90 minutes.Category B2 – None.2.17 Module 17, Propeller:Category A – 20 multi-choice and 0 essay questions. Time allowed 25 minutes.Category B1 – 32 multi-choice and 0 essay questions. Time allowed 40 minutes.Category B2 – None.
Type training and assessment standardsPart 1 — Type training levelsThe 3 levels set out below describe the objectives, the depth of training, and the level of questions that the training is intended to achieve.Level 1A brief overview of the airframe, systems and powerplant, as outlined in the systems description section of the Aircraft Maintenance Manual/Instructions for Continued Airworthiness.Course objectives:On completion of the course, the student will be able to:(a) provide a simple description of the whole subject, using common words, examples, and typical terms, and identify safety precautions related to the airframe, its systems and powerplant; and(b) identify aircraft manuals, and maintenance practices important to the airframe, its systems and powerplant; and(c) define the general layout of the aircraft’s major systems; and(d) define the general layout and characteristics of the powerplant; and(e) identify special tooling and test equipment used with the aircraft.Level 2Basic system overview of controls, indicators, principal components – including their location and purpose – servicing and minor troubleshooting, general knowledge of the theoretical and practical aspects of the subject.Course objectives:In addition to the information contained in the Level 1 training, at the completion of Level 2 training, the student will be able to:(a) understand the theoretical fundamentals, and apply knowledge in a practical manner using detailed procedures; and(b) recall the safety precautions to be observed when working on or near the aircraft, powerplant and systems; and(c) describe systems and aircraft handling procedures, particularly access, power availability and sources; and(d) identify the locations of the principal components; and(e) explain the normal functioning of each major system, including terminology and nomenclature; and(f) perform the procedures for servicing associated with the aircraft for the following systems: fuel, powerplants, hydraulics, landing gear, water/waste and oxygen; and(g) demonstrate proficiency in the use of crew reports and on-board reporting systems (minor troubleshooting), and determine aircraft airworthiness as per the MEL/CDL; and(h) demonstrate the use, interpretation and application of appropriate documentation, including instructions for continued airworthiness, maintenance manual, and illustrated parts catalogue.Level 3Detailed description, operation, component location, removal and installation, and BITE and troubleshooting procedures to maintenance manual level.Course objectives:In addition to the information contained in Level 1 and Level 2 training, at the completion of Level 3, the student will be able to:(a) demonstrate a theoretical knowledge of aircraft systems and structures and interrelationships with other systems, provide a detailed description of the subject using theoretical fundamentals and specific examples, and interpret results from various sources and measurements, and apply corrective action where appropriate; and(b) perform system, powerplant, component, and functional checks as specified in the aircraft maintenance manual; and(c) demonstrate the use of, interpret, and apply appropriate documentation, including structural repair manual, and troubleshooting manual; and(d) correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level; and(e) describe procedures for replacement of components unique to aircraft type.Part 2 — Type training theoretical elementsAlthough aircraft type training includes both theoretical and practical elements, courses can be approved for the theoretical element, the practical element or for a combination of both.Theoretical element1 Objective:On completion of a theoretical training course, the student must be able to demonstrate, to the levels identified in the Appendix III syllabus, the detailed theoretical knowledge of the aircraft’s applicable systems, structure, operations, maintenance, repair, and troubleshooting according to approved maintenance data. The student must be able to demonstrate the use of manuals and approved procedures, including the knowledge of relevant inspections and limitations.2 Level of training:Training levels are those levels defined in Part 1 above. After the first type course for Category C certifying staff, all subsequent courses need only be to Level 1. During a Level 3 theoretical training, Level 1 and Level 2 training material may be used to teach the full scope of the chapter if required. However, during the training the majority of the course material and training time must be at the higher level.3 Duration:The theoretical training minimum tuition hours are contained in the following table:Category | HoursAeroplanes with a maximum take-off mass above 30 000 kg | B1.1 | 150B1.2 | 120B2 | 100C | 30Aeroplanes with a maximum take-off mass equal to, or less than, 30 000 kg and above 5 700 kg | B1.1 | 120B1.2 | 100B2 | 100C | 25Large helicopters | B1.3 | 120B2 | 100C | 25(a) For the purpose of the table above, tuition hour means 60 minutes of teaching and excludes any breaks, examination, revision, preparation and aircraft visits.(b) Hours prescribed in the table above apply only to theoretical courses for complete aircraft/engine combinations according to the type rating as defined by CASA.Minimum participation time is at least 90% of the tuition hours of the theoretical training course. Additional training may be given by the training organisation in order to meet the minimum participation time. The number of tuition hours per day for the theoretical training must not exceed 8 hours, which must be performed during regular office hours; in exceptional cases, deviation from this standard may be envisaged when justified. This maximum number of hours is also applicable for the combination of theoretical and practical training, when they are performed at the same time.4 Justification of course duration:When applying for approval of a Part 147 course, or a course to be approved directly by CASA, the proposed hour duration must be justified and shown to cover the full syllabus by a training needs analysis based on:(a) the design of the aircraft type, its maintenance needs and the types of operation; and(b) detailed analysis of applicable chapters – see contents table below; and(c) detailed competency analysis showing that the objectives as stated in paragraph 2.1 (a) above are fully met; and(d) information based on approved type design, if necessary.Tuition hours of differences courses, and other training course combinations, such as combined B1/B2 courses, must be justified to CASA by the training needs analysis as described above.5 Content:As a minimum, the elements in the syllabus below, that are specific to the aircraft type, must be covered. Additional elements introduced due to type variations, technological changes etc. must also be included. The training syllabus should be focused on mechanical, powerplant, structural and electrical aspects for B1 personnel, and electrical and avionic aspects for B2.Introductory elements of training — all aircraftATA chapter | Theory elements | Aeroplane turbine | Aeroplane piston | Helicopter turbine | Helicopter piston | AvionicsB1.1 | C | B1.2 | C | B1.3 | C | B1.4 | C | B205 | Time limits and main-tenance checks | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 106 | Dimensions and areas, for example weights, maximum take-off weight (MTOW) | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 107 | Lifting and shoring | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 108 | Levelling and weigh-ing | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 109 | Towing and taxiing | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 110 | Parking, mooring, storing and return to service | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 111 | Placards and mark-ings | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 112 | Servicing | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 120 | Standard practices – only type particular | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1Helicopters18 | Vibration and noise analysis (blade tracking) | — | — | — | — | 3 | 1 | 3 | 1 | —25 | Emergency flotation equipment | — | — | — | — | 3 | 1 | 3 | 1 | 153 | Airframe structure (helicopter) | — | — | — | — | 3 | 1 | 3 | 1 | —60 | Standard practices rotor | — | — | — | — | 3 | 1 | 3 | 1 | —62 | Rotor(s) | — | — | — | — | 3 | 1 | 3 | 1 | 162A | Rotors –monitoring and indicating | — | — | — | — | 3 | 1 | 3 | 1 | 363 | Rotor drive(s) | — | — | — | — | 3 | 1 | 3 | 1 | 163A | Rotor drive(s) – monitoring and indicating | — | — | — | — | 3 | 1 | 3 | 1 | 364 | Tail rotor | — | — | — | — | 3 | 1 | 3 | 1 | 164A | Tail rotor – monitoring and indicating | — | — | — | — | 3 | 1 | 3 | 1 | 365 | Tail rotor drive | — | — | — | — | 3 | 1 | 3 | 1 | 165A | Tail rotor drive monitoring and indicating | — | — | — | — | 3 | 1 | 3 | 1 | 366 | Folding blades and pylon | — | — | — | — | 3 | 1 | 3 | 1 | —67 | Rotors flight control | — | — | — | — | 3 | 1 | 3 | 1 | —Aircraft structures27A | Flight control surfaces (all) | 3 | 1 | 3 | 1 | — | — | — | — | 151 | Standard practices and struc-tures (damage classifica-tion, assess-ment and repair) | 3 | 1 | 3 | 1 | — | — | — | — | 152 | Doors | 3 | 1 | 3 | 1 | — | — | — | — | 153 | Fuselage | 3 | 1 | 3 | 1 | — | — | — | — | 154 | Nacelles and pylons | 3 | 1 | 3 | 1 | — | — | — | — | 155 | Stabilisers | 3 | 1 | 3 | 1 | — | — | — | — | 156 | Windows | 3 | 1 | 3 | 1 | — | — | — | — | 157 | Wings | 3 | 1 | 3 | 1 | — | — | — | — | 1Zonal and station identifica-tion systems | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1Aircraft systems21 | Air-con-ditioning | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 321-10/20 | Air supply | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 221B | Pressurisa-tion | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 321C | Safety and warning devices | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 322 | Autoflight | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 323 | Communi-cations | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 324 | Electrical power | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 325 | Equipment and furnish-ings | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 125A | Electronic equipment including emergency equipment | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 326 | Fire protection | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 327 | Flight controls | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 227A | Systems operation: electrical and fly-by-wire | 3 | 1 | — | — | — | — | — | — | 328 | Fuel systems | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 228-40 | Fuel systems – monitoring and indicat-ing | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 329 | Hydraulic power | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 229A | Hydraulic power – monitoring and indicat-ing | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 330 | Ice and rain protection | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 331 | Indicating and record-ing systems | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 331A | Instrument systems | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 332 | Landing gear | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 232A | Landing gear – monitoring and indicat-ing | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 333 | Lights | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 334 | Navigation | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 335 | Oxygen | 3 | 1 | 3 | 1 | — | — | — | — | 236 | Pneumatic | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 236A | Pneumatic – monitoring and indicat-ing | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 337 | Vacuum | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 238 | Water and waste | 3 | 1 | 3 | 1 | — | — | — | — | 241 | Water ballast | 3 | 1 | 3 | 1 | — | — | — | — | 142 | Integrated modular avionics | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 344 | Cabin systems | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 345 | On-board mainten-ance sys-tems (except if the element is covered in the element for ATA chapter 31) | 3 | 1 | 3 | 1 | 3 | 1 | — | — | 346 | Information systems | 2 | 1 | 2 | 1 | 2 | 1 | 2 | 1 | 350 | Cargo and accessory compart-ments | 3 | 1 | 3 | 1 | 3 | 1 | 3 | 1 | 1Turbine engines49 | Airborne auxiliary power (APUs) | 3 | 1 | — | — | — | — | — | — | 270 | Standard practices –engines | 3 | 1 | — | — | 3 | 1 | — | — | 170A | Construc-tional arrange-ment and operation (namely, installation, inlet, com-pressors, combustion section, turbine section, bear-ings and seals, lubri-cations systems) | 3 | 1 | — | — | 3 | 1 | — | — | 170B | Engine perform-ance | 3 | 1 | — | — | 3 | 1 | — | — | 171 | Powerplant | 3 | 1 | — | — | 3 | 1 | — | — | 172 | Engine turbine and turboprop and ducted fan and unducted fan | 3 | 1 | — | — | 3 | 1 | — | — | 173 | Engine fuel and control | 3 | 1 | — | — | 3 | 1 | — | — | 173A | FADEC | 3 | 1 | — | — | 3 | 1 | — | — | 374 | Ignition | 3 | 1 | — | — | 3 | 1 | — | — | 375 | Air | 3 | 1 | — | — | 3 | 1 | — | — | 176 | Engine control | 3 | 1 | — | — | 3 | 1 | — | — | 177 | Engine indicating systems | 3 | 1 | — | — | 3 | 1 | — | — | 378 | Exhaust | 3 | 1 | — | — | 3 | 1 | — | — | 179 | Oil | 3 | 1 | — | — | 3 | 1 | — | — | 180 | Starting | 3 | 1 | — | — | 3 | 1 | — | — | 182 | Water injections | 3 | 1 | — | — | 3 | 1 | — | — | 183 | Accessory gearboxes | 3 | 1 | — | — | 3 | 1 | — | — | 184 | Propulsion augmenta-tion | 3 | 1 | — | — | 3 | 1 | — | — | 1Piston engines70 | Standard practices — engines | — | — | 3 | 1 | — | — | 3 | 1 | 170A | Construc-tional arrangement and operation (carburettors, fuel injection systems, induction, exhaust and cooling systems, supercharging/turbocharging, lubrication systems) | — | — | 3 | 1 | — | — | 3 | 1 | 170B | Engine per-formance | — | — | 3 | 1 | — | — | 3 | 1 | 171 | Powerplant | — | — | 3 | 1 | — | — | 3 | 1 | 173 | Engine fuel and control | — | — | 3 | 1 | — | — | 3 | 1 | 173A | FADEC | — | — | 3 | 1 | — | — | 3 | 1 | 374 | Ignition | — | — | 3 | 1 | — | — | 3 | 1 | 376 | Engine control | — | — | 3 | 1 | — | — | 3 | 1 | 177 | Engine indicating Systems | — | — | 3 | 1 | — | — | 3 | 1 | 379 | Oil | — | — | 3 | 1 | — | — | 3 | 1 | 180 | Starting | — | — | 3 | 1 | — | — | 3 | 1 | 181 | Turbines | — | — | 3 | 1 | — | — | 3 | 1 | 182 | Water injections | — | — | 3 | 1 | — | — | 3 | 1 | 183 | Accessory gearboxes | — | — | 3 | 1 | — | — | 3 | 1 | 184 | Propulsion augmenta-tion | — | — | 3 | 1 | — | — | 3 | 1 | 1Aeroplane propellers60A | Standard practices – propeller | 3 | 1 | 3 | 1 | — | — | — | — | 161 | Propellers/Propulsion | 3 | 1 | 3 | 1 | — | — | — | — | 161A | Propeller construction | 3 | 1 | 3 | 1 | — | — | — | — | —61B | Propeller pitch control | 3 | 1 | 3 | 1 | — | — | — | — | —61C | Propeller synchronis-ing | 3 | 1 | 3 | 1 | — | — | — | — | 161D | Propeller electronic control | 2 | 1 | 2 | 1 | — | — | — | — | 361E | Propeller ice protection | 3 | 1 | 3 | 1 | — | — | — | — | —61F | Propeller mainten-ance | 3 | 1 | 3 | 1 | — | — | — | — | 1Part 3 — Practical elements1 The representative cross-section of maintenance activities mentioned in section 66.A.50 may include training in maintenance of the aircraft, rigging, adjustments, replacement of line replaceable units, troubleshooting, rectification of minor defects and testing of systems covering each element of the course.2 The structured OJT practical element of type training may include targeted experience recorded within a schedule of experience or competency-based assessment of a schedule of practical tasks.3 Irrespective of how the practical training element is conducted, it must consist of the performance of representative maintenance tasks drawn from the type training and examination syllabus, at the indicated level, and their assessment in order to meet the following objectives:(a) ensure safe performance of maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example, troubleshooting, repairs, adjustments, replacements and functional checks;(b) correctly use all technical literature and documentation for the aircraft;(c) correctly use specialist and special tooling and test equipment, perform removal and replacement of components and modules unique to type, including any on-wing maintenance activity.Part 4A Theory element — examination standardWhere aircraft type training is required, the examination must be written and comply with the following:(a) Format of the examination is of the multiple-choice type. Each multi-choice question must have 3 alternative answers of which only 1 must be the correct answer. The time for answering is based upon a nominal average of 90 seconds per question.(b) Alternative answers must seem equally possible to anyone with no knowledge of the subject. All of the alternatives should be clearly related to the question and of similar vocabulary, grammatical construction and length.(c) In numerical questions, the incorrect answers must correspond to procedural errors such as the use of incorrect sense (+ versus -) or incorrect measurement units: they must not be mere random numbers.(d) Subject to paragraph (j), the level of each question should be the one defined in Part 2 “type training standard”.(e) The examination must be of the closed book type. No reference material is permitted. An exception will be made for the case of examining a B1 or B2 candidate’s ability to interpret technical documents.(f) The number of questions must be at least 1 question per hour of instruction, with a minimum of 1 question per chapter. CASA will assess number and level of questions on a sampling basis when approving the course. The number of questions for each level must be consistent with the effective training hours spent teaching at that level.(g) The minimum examination pass mark is 75%. When the type training examination is split into several examinations, each examination must be passed with at least a 75% pass mark. For it to be possible to achieve exactly a 75% pass mark, the number of questions in the examination must be a multiple of 4.(h) Penalty marking is not to be used to determine whether a candidate has passed.(i) End of module phase examinations cannot be used as part of the final examination unless they contain the correct number and level of questions required.(j) It is accepted that during a Level 3 examination, Level 1 and Level 2 questions may be used to examine the full scope of the course material. However, during the examination it is not acceptable to use more than 25% of questions at any lower level such that the intention of the higher examination level is reduced.Note Penalty marking means deducting marks for an incorrect answer.B Practical element — assessment standard1 For assessment of practical elements of type training, the assessment must be oral, written or practical assessment based, or a combination of all of these. Conduct of the assessment method must be in accordance with the AMO’s or MTO’s exposition.2 Practical assessment must determine a person’s competence to perform a task based on a sample of subjects drawn from the type training and examination syllabus, at the indicated level.3 A written report must be made by the assessor to explain why the candidate has passed or failed.4 The assessment must ensure that the following objectives are met:(a) accurately and confidently discuss the aircraft and its systems;(b) ensure safe performance of maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example, troubleshooting, repairs, adjustments, replacements, rigging and functional checks such as engine run etc., if required;(c) correctly use all technical literature and documentation for the aircraft;(d) correctly use specialist and special tooling and test equipment, perform removal and replacement of components and modules unique to type, including any on-wing maintenance activity.
Note These aeroplanes are large or designated as large — requiring type training and endorsement of type rating on the relevant licence category.Type Certificate (TC) holder | Aircraft type (aeroplanes) | Commercial designation | Type rating endorsement (aircraft type – engine in brackets)328 Support Services | 328-100 Series | Dornier 328-100(PWC PW119)AIRBUSA318-110 SeriesA319-110 SeriesA320-111A320-210 SeriesA321-110 SeriesA321-210 SeriesAirbus A318/A319/A320/A321 (CFM56)A319-130 SeriesA320-230 SeriesA321-130 SeriesA321-230 SeriesAirbus A319/A320/A321 (IAE V2500)A319-150 SeriesA320-250 SeriesA321-250 SeriesAirbus A319/A320/A321(CFM LEAP-1A)A319-170 SeriesA320-270 SeriesA321-270 SeriesAirbus A319/A320/A321(IAE PW1100G)A330-200 SeriesA330-300 SeriesAirbus A330(GE CF6)A330-220 SeriesA330-320 SeriesAirbus A330(PW 4000)A330-240 SeriesA330-340 SeriesAirbus A330(RR RB 211 Trent 700)A350-900 Series | Airbus A350(RR Trent XWB)A380-840 Series | Airbus A380(RR RB211 Trent 900)AIRBUS CANADA LIMITED PARTNERSHIP | BD-500-1A10BD-500-1A11 | A220-100A220-300 | Bombardier BD-500 Series (PW PW1500G)AIRCRAFT INDUSTRIES | L-420 | Let L-420(Walter M601) Note 2ATR-GIEAvions de Transport Régional | ATR 42-200 | ATR 42-200/300 Series(PWC PW120)ATR 42-300 | ATR 42-200/300 Series(PWC PW120)ATR 42-320 | ATR 42-200/300 Series(PWC PW120)ATR 42-400 | ATR 42-400/500/72-212A(PWC PW120)ATR 42-50042-50042-600ATR 42-400/500/72-212A(PWC PW120)ATR 72-101 | ATR 72-100/200 Series(PWC PW120)ATR 72-102 | ATR 72-100/200 Series(PWC PW120)ATR 72-201 | ATR 72-100/200 Series(PWC PW120)ATR 72-202 | ATR 72-100/200 Series(PWC PW120)ATR 72-211 | ATR 72-100/200 Series(PWC PW120)ATR 72-212 | ATR 72-100/200 Series(PWC PW120)ATR 72-212 A72-50072-600ATR 42-400/500/72-212A(PWC PW120)BAE SYSTEMS (OPERATIONS) LTDBAE SYSTEMS (OPERATIONS) LTDBAe 146 Series 100BAe 146 Series 200BAe 146 Series 300AVRO 146-RJ70AVRO 146-RJ85AVRO 146-RJ100AVRO 146-RJ115BAe 146/AVRO 146-RJ(Honeywell ALF500 Series)HS.748 Series 1HS.748 Series 2HS 748 Series 2AHS 748 Series 2BHS748(RRD Dart)Jetstream 3100 | Jetstream 31 | Jetstream 31/32(Honeywell TPE331)Jetstream 3200 | Jetstream 32/32EP | Jetstream 31/32(Honeywell TPE331)Jetstream 4100 | Jetstream 41(Honeywell TPE331)BOEING COMPANY (THE)BOEING COMPANY (THE)BOEING COMPANY (THE)B707-100Long BodyBoeing 707/720(PW JT3)B707-100B | Long Body | Boeing 707/720(PW JT3)B707-100B | Short Body | Boeing 707/720(PW JT3)B707-300B SeriesB707-300C SeriesB720B720BBoeing 707/720(PW JT3)B717-200 | MD 717-200(RRD BR700-715)B727 SeriesB727-100 SeriesB727C SeriesB727-100C SeriesB727-200 SeriesBoeing 727(PW JT8D)B737-300 | B737 Classic | Boeing 737-300/400/500(CFM56)B737-400 | B737 Classic | Boeing 737-300/400/500(CFM56)B737-500 | B737 Classic | Boeing 737-300/400/500(CFM56)B737-600 | B737 Next Generation | Boeing 737-600/700/800/900(CFM56)B737-700 | B737 Next Generation | Boeing 737-600/700/800/900(CFM56)B737-800 | B737 Next Generation | Boeing 737-600/700/800/900(CFM56)B737-900 | B737 Next Generation | Boeing 737-600/700/800/900(CFM56)B737-900ER | B737 Next Generation | Boeing 737-600/700/800/900(CFM56)B737-7 | B737 MAX | Boeing 737-7/8/9/10(CFM LEAP-1B)B737-8 | B737 MAX | Boeing 737-7/8/9/10(CFM LEAP-1B)B737-8200 | B737 MAX | Boeing 737-7/8/9/10(CFM LEAP-1B)B737-9 | B737 MAX | Boeing 737-7/8/9/10(CFM LEAP-1B)B737-10 | B737 MAX | Boeing 737-7/8/9/10(CFM LEAP-1B)B747-400B747-400DB747-400F/SF/BCFBoeing 747-400(GE CF6)B747-400B747-400F/SF/BCFBoeing 747-400(PW 4000)B747-400B747-400F/SF/BCFBoeing 747-400(RR RB211)B757-200B757-200PFB757-300Boeing 757-200/300(RR RB211)B767-200B767-300Boeing 767-200/300(PW 4000)B767-200B767-300Boeing 767-200/300(PW JT9D)B767-200B767-300B767-300FB767-400ERBoeing 767-200/300/400 (GE CF6)B777-200B777-200LRB777-300ERB777Boeing 777-200/300(GE 90)B777F | Freighter | Boeing 777-200/300(GE 90)B777-200B777-300B777Boeing 777-200/300(RR RB211 Trent 800)B787-8B787-9B787-10DreamlinerBoeing 787-8/9/10(GEnx)B787-8B787-9B787-10DreamlinerBoeing 787-8/9/10(RR RB211 Trent 1000)BOMBARDIERBOMBARDIERBD-100-1A10Challenger 300Challenger 350Bombardier BD-100-1A10(Honeywell AS907)BD-700-1A10Global ExpressGlobal 6000Global 6500Bombardier BD-700 Series(RRD BR710)BD-700-1A11Global 5000Global 5000 GVFDGlobal 5500Bombardier BD-700 Series(RRD BR710)BD-700-2A12 | Global 7500 | Bombardier BD-700-2A12(GE Passport 20)CL-600-1A11 | Challenger 600 | Bombardier CL-600-1A11 (Honeywell ALF502)CL-600-2A12(601 Variant) | Challenger 601 | Bombardier CL-600-2A12/2B16 (601/601-3A/3R Variant) (GE CF34)CL-600-2B16(601-3A Variant) | Challenger 601-3A | Bombardier CL-600-2A12/2B16 (601/601-3A/3R Variant) (GE CF34)CL-600-2B16(601-3R Variant) | Challenger 601-3R | Bombardier CL-600-2A12/2B16 (601/601-3A/3R Variant) (GE CF34)CL-600-2B16(604 Variant) | Challenger 604(MSN < 5701)Challenger 605(5701 ≤ MSN ≤ 5990)Challenger 650(MSN ≥ 6050) | Bombardier CL-600-2B16 (604 Variant) (GE CF34)CL-600-2B19(RJ Series 100) | Regional Jet Series 100/200/440/Challenger 850/CRJ SE | Bombardier CL-600-2B19/2C10/2D15/2D24/2E25 (GE CF34)CL-600-2C10(RJ 700/701/702) | Regional Jet Series 700/701/702 | Bombardier CL-600-2B19/2C10/2D15/2D24/2E25 (GE CF34)CL-600-2D15(RJ Series 705) | Regional Jet Series 705 | Bombardier CL-600-2B19/2C10/2D15/2D24/2E25 (GE CF34)CL-600-2D24(RJ Series 900) | Regional Jet Series 900 | Bombardier CL-600-2B19/2C10/2D15/2D24/2E25 (GE CF34)CL-600-2E25(RJ Series 1000) | Regional Jet Series 1000 | Bombardier CL-600-2B19/2C10/2D15/2D24/2E25 (GE CF34)DHC-8-102DHC-8-103DHC-8-106DHC-8Series 100BombardierDHC-8-100/200/300(PWC PW 120)DHC-8-201DHC-8-202DHC-8Series 200BombardierDHC-8-100/200/300(PWC PW 120)DHC-8-301DHC-8-311DHC-8-314DHC-8-315DHC-8Series 300BombardierDHC-8-100/200/300(PWC PW 120)DHC-8-401DHC-8-402DHC-8Series 400BombardierDHC-8-400(PWC PW150)CESSNA AIRCRAFT COMPANYCESSNA AIRCRAFT COMPANY510Citation MustangCessna 510(PWC PW615)525 | Citation Jet (CJ)Citation Jet1 (CJ1)Citation Jet1+ (CJ1+)Citation (M2) | Cessna 525/525A/525B(Williams FJ44)525A | Citation Jet CJ2 | Cessna 525/525A/525B(Williams FJ44)525B | Citation Jet CJ3 | Cessna 525/525A/525B(Williams FJ44)525C | Citation Jet CJ4 | Cessna 525C(Williams FJ44)550Citation BravoCessna 550/560(PWC PW530/535)550 | Citation II | Cessna 550/551/560(PWC JT15D)S550 | Citation S/II | Cessna 550/551/560(PWC JT15D)551 | Citation II | Cessna 550/551/560(PWC JT15D)560 | Citation Encore | Cessna 550/560(PWC PW530/535)560 | Citation Encore+ | Cessna 550/560(PWC PW530/535)560 | Citation V | Cessna 550/551/560(PWC JT15D)560 | Citation Ultra | Cessna 550/551/560(PWC JT15D)560 XLCitation ExcelCitation XLSCitation XLS+Cessna 560XL/XLS (PWC PW545)650Citation IIICitation VICitation VIICessna 650(Honeywell TFE731)680SovereignSovereign+Cessna 680(PWC PW306)680A | Latitude | Cessna 680 (PWC PW306)750 | Citation X | Cessna 750(RR Corp AE3007C)CIRRUS Design Corporation | SF50 single engine jet | Vision Jet | CIRRUS SF50 (Williams FJ33)DASSAULTAVIATIONDASSAULTAVIATIONFalcon 10Falcon 10(Honeywell TFE731)Fan Jet FalconSeries CSeries DSeries ESeries F(Basic) Fan Jet FalconFalcon 20(GE CF700)Mystère Falcon 20-C5Mystère Falcon 20-D5Mystère Falcon 20-E5Mystère Falcon 20-F5Falcon 20-5(Honeywell TFE731)Fan Jet Falcon Series GMystère Falcon 200Mystère Falcon 20GFFalcon 200(Honeywell ATF 3-6)Mystère Falcon 50 | 50 | Falcon 50(Honeywell TFE731)Mystère Falcon 50 | 50EX | Falcon 50EX(Honeywell TFE731)Mystère Falcon 900 | Falcon 900Falcon 900B | Falcon 900(Honeywell TFE731)Mystère Falcon 900 | F900C | Falcon 900C/EX(Honeywell TFE731)Falcon 900EX | Falcon 900C/EX(Honeywell TFE731)Falcon 2000 | Falcon 2000(CFE 738)Falcon 2000EXFalcon 2000EX(PWC PW308)Falcon 2000EXF2000EXEASyF2000DXF2000LXF2000LXSF2000SFalcon 2000EX EASy(PWC PW308C)Falcon 7XFalcon 7XFalcon 8XFalcon 7X(PW307)EADS CASAC-212-CBC-212-CCC-212-CDC-212-CEC-212-CFC-212-DDC-212-DFC-212-EEC-212-VAAviocarCASA C-212(Honeywell TPE331)CN-235CN-235-100CN-235-200CN-235-300CASA CN-235 (GE CT7)EMBRAEREMBRAEREMB-120EMB-120RTEMB-120ERBrasiliaEmbraer EMB-120(PWC PW110 Series)EMB-135BJ | Legacy 600 | Embraer EMB-135/145(RR Corp AE3007A)EMB-135BJ | Legacy 650 | Embraer EMB-135/145(RR Corp AE3007A)EMB-135EREMB-135LREMB-145EMB-145EREMB-145EUEMB-145EPEMB-145LREMB-145LUEMB-145MPEMB-145MKEmbraer EMB-135/145(RR Corp AE3007A)EMB-500 | Phenom 100 | Embraer EMB-500(PWC PW617)EMB-505Phenom 300Embraer EMB-505(PWC PW535)EMB-545 | Legacy 450 | Embraer EMB-545/550 (Honeywell AS907)EMB-550 | Legacy 500 | Embraer EMB-545/550 (Honeywell AS907)ERJ-170-100 STD | ERJ-170 | Embraer ERJ-170 Series(GE CF34)ERJ 170-100 LR | ERJ-170 | Embraer ERJ-170 Series (GE CF34)ERJ 170-200 STD | ERJ-175 | Embraer ERJ-170 Series (GE CF34)ERJ 170-200 LR | ERJ-175 | Embraer ERJ-170 Series(GE CF34)ERJ 190-100 ECJ | Lineage 1000 | Embraer ERJ-190 Series(GE CF34)ERJ 190-100 LR | ERJ-190 | Embraer ERJ-190 Series(GE CF34)ERJ 190-100 STD | ERJ-190 | Embraer ERJ-190 Series (GE CF34)ERJ 190-100 SR | ERJ-190 | Embraer ERJ-190 Series(GE CF34)ERJ 190-200 STD | ERJ-195 | Embraer ERJ-190 Series(GE CF34)ERJ 190-100 IGW | ERJ-190 AR | Embraer ERJ-190 Series(GE CF34)ERJ 190-200 IGW | ERJ-195 AR | Embraer ERJ-190 Series(GE CF34)ERJ 190-200 LR | ERJ-195 | Embraer ERJ-190 Series(GE CF34)ERJ 190-300 | ERJ-190 | Embraer ERJ-190 Series(PWC PW1900G)FOKKERSERVICES | F27 Mark 050 | Fokker 50 | Fokker 50/60 Series(PWC PW 125/127)F27 Mark 0502 | Fokker 50 | Fokker 50/60 Series(PWC PW 125/127)F27 Mark 0604 | Fokker 60 | Fokker 50/60 Series(PWC PW 125/127)F28 Mark 1000F28 Mark 1000CF28 Mark 2000F28 Mark 3000F28 Mark 3000CF28 Mark 3000RF28 Mark 3000RCF28 Mark 4000FellowshipHawker SiddeleyFokker F28 Series(RRD Spey)Fokker F28 Series(RRD Spey)F28 Mark 0070 | Fokker 70 | Fokker 70/100(RRD Tay)F28 Mark 0100 | Fokker 100 | Fokker 70/100(RRD Tay)GULFSTREAM AEROSPACE LP (GALP), c/o Israel Aircraft Industries1125 Westwind AstraAstra SPXG100Gulfstream 100Gulfstream (IAI) 100/1125/Astra SPX (Honeywell TFE731)Gulfstream G150 | Gulfstream G150 | Gulfstream (IAI) G150(Honeywell TFE731)Gulfstream G280 | Gulfstream G280 | Gulfstream (IAI) G280(Honeywell AS907)Gulfstream 200/Galaxy | Galaxy 200 | Gulfstream (IAI) 200/Galaxy(PWC PW306)GULFSTREAMAEROSPACECorporationGULFSTREAMAEROSPACECorporationGIV (G300)Gulfstream G300Gulfstream G-IV Series(RRD Tay)GIV (G400) | Gulfstream G400 | Gulfstream G-IV Series(RRD Tay)G-IV/GIV-SP | GulfstreamG-IV/GIV-SP | Gulfstream G-IV Series(RRD Tay)GIV-X (G350) | Gulfstream G350 | Gulfstream GIV-X Series(RRD Tay)GIV-X (G450) | Gulfstream G450 | Gulfstream GIV-X Series(RRD Tay)GV | Gulfstream GV | Gulfstream GV basic model(RRD BR710)GV-SP (G500) | Gulfstream G500 | Gulfstream GV-SP Series(RRD BR710)GV-SP (G550) | Gulfstream G550 | Gulfstream GV-SP Series(RRD BR710)GVI | G650 | Gulfstream GVI(RRD BR725)GVIII-G700 | G700 | Gulfstream GVIII(RRD BR730)HAWKER BEECHCRAFTHAWKER BEECHCRAFTDH.125 Series 1DH.125 Series 3DH.125 Series 400HS.125 Series 3HS.125 Series F3HS.125 Series F400HS.125 Series 600HS.125 Series 700HS.125 Series F600Hawker SiddeleyBAe 125/Series 700/800 (Honeywell TFE731)BH.125 Series 400BH.125 Series 600Beechcraft HawkerBAe 125/Series 700/800 (Honeywell TFE731)BAe.125 Series 800 | BAe 125/Series 700/800(Honeywell TFE731)Hawker 750 | Hawker 750 | BAe 125 Series 750/800XP/850XP/900XP(Honeywell TFE731)Hawker 800XP | Hawker 800XP | BAe 125 Series 750/800XP/850XP/900XP(Honeywell TFE731)Hawker 850XP | Hawker 850XP | BAe 125 Series 750/800XP/850XP/900XP(Honeywell TFE731)Hawker 900XP | Hawker 900XP | BAe 125 Series 750/800XP/850XP/900XP(Honeywell TFE731)BAe 125 SeriesHawker 1000A/BHawker 1000BAe 125 Series 1000(PWC PW305)300300LWSuper King AirBeech 300 Series(PWC PT6)B300 | Super King Air 350 | Beech 300 Series(PWC PT6)B300C | Super King Air 350 C | Beech 300 Series(PWC PT6)390 | Premier I, 1A | Beech 390(Williams FJ44)400 | Beechjet | Beech 400/Mitsubishi MU-300(PWC JT15)400A | Beechjet (Hawker XP) | Beech 400/Mitsubishi MU-300(PWC JT15)400T | Beechjet | Beech 400/Mitsubishi MU-300(PWC JT15)MU-300 | Diamond I/IA | Beech 400/Mitsubishi MU-300(PWC JT15)MU-300-10 | Diamond II | Beech 400/Mitsubishi MU-300(PWC JT15)19001900C1900DAirlinerBeech 1900(PWC PT6)HONDA AIRCRAFT COMPANY LLC | HA-420 | HondaJet | Honda HA-420(HF120)ISRAEL AIRCRAFT INDUSTRIESIAI 1124IAI 1124AWestwindIAI 1124(Honeywell TFE731)KELOWNA (Convair) | 580 | Convair 580(RR Corp 501)LEARJETLEARJET31/31ALearjet 31(Honeywell TFE731)35/35A36/36ALearjet 35/36(Honeywell TFE731)Learjet 40 | LJ40 or LJ40XR | Learjet Model 45(Honeywell TFE731)Learjet 45 | LJ45 or LJ45XR | Learjet Model 45(Honeywell TFE731)55/55B/55C | Learjet 55(Honeywell TFE731)Learjet 60 | LJ60 or LJ60XR | Learjet 60(PWC PW305)M7 AEROSPACESA226-TSA226-TCSA226-ATSA226-T(B)Fairchild SA226 Series(Honeywell TPE331)SA227-ATSA227-TTSA227-CCSA227-DCFairchild SA227 Series(Honeywell TPE331)SA227-ACSA227-BCSwearingen MetroNEXTANT AEROSPACE L.L.C. (STC)400XT400XTiNEXTANT 400XTBeech 400XT Nextant(Williams FJ44)PILATUSAIRCRAFTPC-12PC-12/45PC-12/47PC-12/47EPC-12/47GPilatus PC-12(PWC PT6)PC-24 | Pilatus PC-24(Williams FJ44)SAAB AB, SAAB Aerosystems340A(SF340A)340BSaab-Fairchild 340ASaab (SF) 340(GE CT7)SHORT BROTHERSSD3-30SD3-60SD3-SHERPASD3-60 SHERPAVariant 200Shorts SD3 Series-30/SD3-60(PWC PT6)TEXTRON AVIATION INC | 408 | SkyCourier | Cessna 408(PWC PT6)VIKING AIR | CL-215-6B11(CL-215T Variant) | Canadair CL-215(PWC PW120)NA | Various | Small/non-rated aircraft(Avco Lycoming T53) Note 1NA | Various | Small/non-rated aircraft (Bristol Siddeley Viper B/S) Note 1NA | Various | Small/non-rated aircraft(De Havilland Goblin 35) Note 1NA | Various | Small/non rated aircraft(Gen Electric J85-GE-17A) Note 1NA | Various | Small/non-rated aircraft(Honeywell TPE331) Note 1NA | Various | Small/non-rated aircraft(PWC JT15D) Note 1NA | Various | Small/non-rated aircraft(PWC PT6) Note 1NA | Various | Small/non-rated aircraft(Rolls Royce Avon) Note 1NA | Various | Allison 250 | Small/non-rated aircraft(RR Corp 250) Note 1NA | Various | General Electric H80 | Small/non-rated aircraft(Walter M601) Note 1, Note 2NA | Various | Small/non-rated aircraft(Williams FJ44) Note 1Note 1 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 1” (the endorsement) has no applicability to Category B2 and Category C. However, an aircraft engineer licence in Category B1.1 or B1.2 (as relevant) must be endorsed with the endorsement before the holder may perform maintenance certifications for the engine of the aircraft.Note 2 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 2” (that is the Walter M601 engine rating) also applies for the M601H-80 engine now designated by the manufacturer as the GE Aviation Czech H80.Table 2Note These are aircraft for which an AMO may select or control type training (theory and practical) for AMO 6 month authorisation and subsequent CASA grant of type rating on the relevant licence category.Part 1 — Aeroplanes eligible for AMO controlled or delivered type trainingNote Aeroplanes in this table were previously covered by regulation 31 of the Civil Aviation Regulations 1988 lower group ratings or are considered eligible for AMO selected manufacturer training.TC holder | Aircraft type (aeroplanes) | Commercial designation | Type rating endorsement (aircraft type – engine in brackets)BAE SYSTEMS | Jetstream 3100 | Jetstream 31 | Jetstream 31/32 (Honeywell TPE331) Note 1Jetstream 3200 | Jetstream 32/32EP | Jetstream 31/32 (Honeywell TPE331) Note 1BOEING COMPANY(THE)B757-200B757-200PFB757-300B757Boeing 757-200/300 (RR RB211) Note 4CESSNA AIRCRAFT COMPANY | 510 | Citation Mustang | Cessna 510(PWC PW615) Note 4525 | Citation Jet (CJ)Citation Jet1 (CJ1)Citation Jet1+ (CJ1+)Citation (M2) | Cessna 525/525A/525B(Williams FJ44) Note 3525A | Citation Jet CJ2 | Cessna 525/525A/525B (Williams FJ44) Note 3525B | Citation Jet CJ3 | Cessna 525/525A/525B (Williams FJ44) Note 3650 | Citation IIICitation VICitation VII | Cessna 650(Honeywell TFE731) Note 3CIRRUS Design Corporation | SF50 single engine jet | Vision Jet | CIRRUS SF50 (Williams FJ33)EMBRAEREMBRAEREMB-120EMB-120RTEMB-120ERBrasiliaEmbraer EMB-120(PWC PW110 Series) Note 1, Note 3EMB-135EREMB-135LREmbraer EMB-135/145(RR Corp AE3007A)Note 4EMB-145EREMB-145LREmbraer EMB-135/145(RR Corp AE3007A)Note 4EMB-505 | Phenom 300 | Embraer EMB-505(PWC PW535) Note 4ERJ 170-100 LR | ERJ-170 | Embraer ERJ-170 Series(GE CF34) Note 4GULFSTREAM AEROSPACE LP (GALP), c/o Israel Aircraft Industries | Gulfstream G150 | Gulfstream G150 | Gulfstream (IAI) G150 (Honeywell TFE731) Note 4Hawker Beechcraft19001900C1900DAirlinerBeech 1900(PWC PT6)B300 | Super King Air 350 | Beech 300 Series (PWC PT6) Note 4M7 AEROSPACESA226-TSA226-TCSA226-ATSA226-T(B)Fairchild SA226 Series (Honeywell TPE331) Note 1NEXTANT AEROSPACE L.L.C (STC) | 400XT400XTi | NEXTANT400XT | Beech 400XT Nextant(Williams FJ44) Note 4NA | Various | Small/non-rated aircraft (Bristol Siddeley Viper B/S) Note 2NA | Various | Small/non-rated aircraft (De Havilland Goblin 35) Note 2NANAVariousAllison 250Small/non-rated aircraft (RR Corp 250)NA | Various | Small/non-rated aircraft (Rolls Royce Avon) Note 2Note 1 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the engine type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 1” requires CASA approved type trainingNote 2 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 2” (the endorsement) has no applicability to Category B2 and Category C. However, an aircraft engineer licence in Category B1.1 or B1.2 (as relevant) must be endorsed with the endorsement before the holder may perform maintenance certifications for the engine of the aircraft.Note 3 This is a rule. AMO training for an aircraft type that is identified in column 4 by the label “Note 3” is approved for practical training only.Note 4 This is a rule. AMO training for an aircraft type that is identified in column 4 by the label “Note 4” is approved for OJT training only.Table 2Note These are aircraft for which an AMO may select or control type training (theory and practical) for AMO 6 month authorisation and subsequent CASA grant of type rating on the relevant licence category.Part 2 — Helicopters eligible for AMO controlled or delivered type trainingNote Helicopters in this table were previously covered by regulation 31 of the Civil Aviation Regulations 1988 lower group ratings or are considered eligible for AMO selected manufacturer training. An AMO may provide B1, or B2, or B1 and B2, aircraft type training for the listed helicopters (but only as annotated in the table).TC holder | Aircraft type (helicopters) | Commercial designation | Type rating endorsement (aircraft type – engine in brackets)AGUSTA WESTLANDA109EA109NA109SAW109SPAgusta A109 Series (PWC PW206/207)Note 7AB139AW139Agusta AB139/AW139 (PWC PT6) Note 7AW189 | AW189 (GE CT7)Note 7AIRBUS HELICOPTERSAS355 EAS355 FAS355 F1AS355 F2Eurocopter AS 355(RR Corp 250) Note 1AIRBUS HELICOPTERSDEUTSCHLAND GmbHAIRBUS HELICOPTERSDEUTSCHLAND GmbHBO 105 ABO 105 C/CBS-4/-5BO 105 D/DBBO 105 DB-4BO 105 DBS SeriesBO 105 LS A-1/A-3BO 105 SBO 105 series(RR Corp 250) Note3EC 135 P1EC 135 P2EC 135 P2 +EC 135 P3EC 635 P2+EC 635 P3Eurocopter EC 135(PWC PW206) Note3EC 135 T1EC 135 T2EC 135 T2+EC 135 T3EC 635 T1EC 635 T2+EC 635 T3Eurocopter EC 135 (Turbomeca Arrius 2B) Note 3, Note 6MBB-BK 117 A SeriesMBB-BK 117 B SeriesEurocopter MBB-BK 117 A/B(Honeywell LTS 101) Note 1, Note 3MBB-BK 117 C1 | Eurocopter MBB-BK 117 C1 (Turbomeca Arriel 1) Note 1, Note 3MBB-BK 117 C2 | EC145 | Eurocopter MBB-BK 117 C2 (Turbomeca Arriel 1) Note 1, Note 3, Note 6MBB-BK 117 D2MBB-BK 117 D3EC145 T2H145Eurocopter MBB-BK117 D2 (TurbomecaArriel 2) Note 1, Note 3BELL HELICOPTER CANADA222222B222UBell 222(Honeywell LTS 101) Note 1, Note2230 | Executive/Utility/EMS | Bell 230(RR Corp 250) Note 2427Bell 427(PWC PW207D) Note 1, Note 2, Note 6430 | Bell 430(RR Corp 250) Note 2, Note 6429 | Bell 429(PWC PW207D)Note 1, Note 3BELL HELICOPTER TEXTRON, INC | 222SP | Bell 222(RR Corp 250) Note 2ERICKSON INCORPORATED, DBA Erickson Air-Crane | S-64 | Erickson S-64(PW JFTD 12) Note 1, Note 3MD HELICOPTERS INC | MD900 | MD Helicopters MD900(PWC PW206/207) Note 1, Note 2, Note 3PICKERING AVIATION INCEH-60AUH-60AUH-60LS-70 SeriesEH-60A/UH-60A/UH-60L(T700-GE-700 Series)SIKORSKY AIRCRAFT | S-58 BT to JT | Sikorsky S-58(PWC PT6T) Note 1, Note 3SIKORSKY AIRCRAFTS-70AS-70BS-70CS-70 SeriesEH-60A/UH-60A/UH-60L(T700-GE-700 Series)S-92A | Sikorsky S-92A (GE CT7-8) Note 7NA | Various | Small/non-rated aircraft(Avco Lycoming T5508)NA | Various | Allison 250 | Small/non-rated aircraft (RR Corp 250) Note 4, Note 5NA | Various | Small/non-rated aircraft(Honeywell LTS101) Note 4NA | Various | small/non-rated aircraft(Honeywell TPE331) Note 1Note 1 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the engine type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 1” requires CASA approved type training.Note 2 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, B2 training for the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 2”, may only be provided by an AMO that is approved in writing by CASA to provide the training.Note 3 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, B1 training, or B2 training, or B1 and B2 training, for the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 3”, may only be provided or arranged by an AMO that is approved in writing by CASA to provide, or arrange, the training.Note 4 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 4” (the endorsement) has no applicability to Category B2 and Category C. However, an aircraft engineer licence in Category B1.3 must be endorsed with the endorsement before the holder may perform maintenance certifications for the engine of the aircraft.Note 5 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 5” (that is the RR Corp 250 engine rating) also applies for the RR250-C300/A1 engine, sometimes referred to as the RR300.Note 6 For information regarding category B2 theory/practical training, please consult CASA Maintenance Personnel Licensing (MPL) section.Note 7 This is a rule. AMO training for an aircraft type that is identified in column 4 by the label “Note 7” is approved for OJT training only.Table 3Note These are large turbine powered aircraft excluded from Part 66 of CASR 1998 type rating, and therefore, eligible to have the engines maintained by a category B1.1 licence holder with the small/non-rated aircraft (engine) rating. A category B2 licence holder may maintain these aircraft without a type rating endorsement.TC holder | Aircraft type (aeroplanes) | Commercial designation | Type rating endorsement (aircraft type – engine in brackets)AIR TRACTOR400500800Air TractorSmall/non-rated aircraft(PWC PT6) Note 1DE HAVILLAND CANADA | DHC-4 | Caribou | Small/non rated aircraft (PWC PT6) Note 1(DORNIER) RUAG AEROSPACE228-100 Series228-200 SeriesSmall/non-rated aircraft(Honeywell TPE331) Note 1Note 1 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 1” (the endorsement) has no applicability to Category B2 and Category C. However, an aircraft engineer licence in Category B1.1 or B1.2 (as relevant) must be endorsed with the endorsement before the holder may perform maintenance certifications for the engine of the aircraft.Table 5Note These are multi-engine helicopters (turbine powered), requiring type training and endorsement of type rating on the relevant licence category, and turbine engines that can be fitted to those helicopters. The small/non-rated aircraft ratings (engine ratings) are applicable to non-rated multi-engined and single-engined helicopters (turbine powered).See paragraph 66.A.1 (e) for the meaning of Various in column 2.TC holder | Aircraft type (helicopters) | Commercial designation | Type rating endorsement (aircraft type – engine in brackets)AGUSTAAS61NAS61NIAgusta AS61N/SikorskyS-61N(GE CT58)AGUSTAWESTLANDAGUSTAWESTLANDA109EA109NA109SAW109SPAgusta A109 Series(PWC PW206/207)A109A109AA109AIIA109CAgusta A109 Series(RR Corp 250)A109K2 | Agusta A109 (Turbomeca Arriel 1)A109EA109LUHAgusta A109 Series(Turbomeca Arrius 2)AB139AW139Agusta AB139/AW139 (PWC PT6)AW169 | AW169(PWC 210)AW189 | AW189(GE CT7)AB 212 | Bell 212/Agusta AB212(PWC PT6)BELL HELICOPTER TEXTRON, INC | 212214ST | Bell 214ST (GE CT7)412412EP412CFBell 412/Agusta AB412 (PWC PT6)AGUSTAAB412AB412 EPBELL HELICOPTER CANADA | 222SP | Bell 222 (RR Corp 250)222222B222UBell 222 (Honeywell LTS 101)230Executive/Utility/EMSBell 230(RR Corp 250)427Bell 427(PWC PW207D)429Bell 429(PWC PW207D)430 | Bell 430(RR Corp 250)AIRBUS HELICOPTERS | SA330 J | Eurocopter SA 330(Turbomeca Turmo)AS332 CAS332 LAS332 C1AS332 L1Eurocopter AS 332(Turbomeca Makila 1A/1A1)AS355 EAS355 FAS355 F1AS355 F2Eurocopter AS 355(RR Corp 250)AS355 NAS355 NPEurocopter AS 355(Turbomeca Arrius 1)SA 365 NSA 365 N1AS 365 N2DauphinEurocopter SA 365 N/N1, AS 365 N2(Turbomeca Arriel 1)AS 365 N3 | Dauphin | Eurocopter AS 365 N3(Turbomeca Arriel 2C)EC 175B | Eurocopter EC 175 (PWC PT6C)EC 225 LP | Eurocopter EC 225(Turbomeca Makila 2A)H160-B | Airbus HelicoptersH160 (Safran Arrano 1)AIRBUS HELICOPTERSDEUTSCHLANDGmbHAIRBUS HELICOPTERSDEUTSCHLANDGmbHBO 105 ABO 105 C/CBS-4/-5BO 105 D/DBBO 105 DB-4BO 105 DBS SeriesBO 105 LSA-1/A-3BO 105 SBO 105 series(RR Corp 250)EC 135 P1EC 135 P2EC 135 P2+EC 135 P3EC 635 P2+EC 635 P3Eurocopter EC 135(PWC PW206)EC 135 T1EC 135 T2EC 135 T2+EC 135 T3EC 635 T1EC 635 T2+EC 635 T3Eurocopter EC 135 (Turbomeca Arrius 2B)EC 135 P3H | Airbus HelicoptersEC135 P3H(PWC PW206)EC 135 T3H | Airbus HelicoptersEC135 T3H(Turbomeca Arrius 2B)MBB-BK 117 A SeriesMBB-BK 117 B SeriesEurocopter MBB-BK 117 A/B(Honeywell LTS 101) Note2MBB-BK 117 C1 | Eurocopter MBB-BK 117 C1(Turbomeca Arriel 1) Note 2MBB-BK 117 C2EC145Eurocopter MBB-BK 117 C2(Turbomeca Arriel 1) Note 2MBB-BK 117 D2MBB-BK 117 D3EC145 T2H145EurocopterMBB-BK 117 D2 (Turbomeca Arriel 2) Note 2ERICKSON INCORPORATED, DBA Erickson Air-Crane | S-64 | Erickson S-64(PW JFTD 12) Note 1, Note 3MD HELICOPTERS INC | MD900 | MD Helicopters MD900(PWC PW206/207)PICKERING AVIATION INCEH-60AUH-60AUH-60LS-70 SeriesEH-60A/UH-60A/UH-60L(T700-GE-700 Series)SIKORSKY AIRCRAFT | S-58 BT to JT | Sikorsky S-58(PWC PT6T)S-61NS-61NMAgusta AS61N/SikorskyS-61N(GE CT58)S-70AS-70BS-70CS-70 SeriesEH-60A/UH-60A/UH-60L(T700-GE-700 Series)S-76A | Sikorsky S-76A(RR Corp 250)S-76A | S-76A+ | Sikorsky S-76A(Turbomeca Arriel 1)S-76A | S-76A++ | Sikorsky S-76A(Turbomeca Arriel 1)S-76B | S-76B | Sikorsky S-76B(PWC PT6)S-76C | Sikorsky S-76C(Turbomeca Arriel 1)S-76C | S-76C+ | Sikorsky S-76C(Turbomeca Arriel 2)S-76C | S-76C++ | Sikorsky S-76C (Turbomeca Arriel 2)S-92A | Sikorsky S-92A(GE CT7-8)NA | Various | Small/non-rated aircraft (Avco Lycoming T53) Note 1NA | Various | Small/non-rated aircraft (GE CT58) Note 1NA | Various | Small/non-rated aircraft(Honeywell LTS 101) Note 1NA | Various | Small/non-rated aircraft(Honeywell TPE331) Note 1NA | Various | Small/non-rated aircraft(Lycoming T5508) Note 1NA | Various | Small/non-rated aircraft(PWC PT6) Note 1NA | Various | Allison 250 | Small/non-rated aircraft (RR Corp 250) Note 1, Note 3NA | Various | Small/non-rated aircraft (Turbomeca Arriel) Note 1NA | Various | Small/non-rated aircraft (Turbomeca Arrius) Note 1NA | Various | Small/non-rated aircraft (Turbomeca Artouste) Note 1NA | Various | Small/non-rated aircraft(Turbomeca Astazou) Note 1Note 1 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 1” (the endorsement) has no applicability to Category B2 and Category C. However, an aircraft engineer licence in Category B1.3 must be endorsed with the endorsement before the holder may perform maintenance certifications for the engine of the aircraft.Note 2 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 2” (that is the Eurocopter MBB-BK117 engine ratings) also applies for Kawasaki BKK117 helicopter models with the same engine as the Eurocopter MBB-BK117 model.Note 3 This is a rule. For an aircraft type mentioned in a cell in a row of column 2, the type rating endorsement mentioned in a cell in the same row in column 4 that is annotated “Note 3” (that is the RR Corp 250 engine rating) also applies for the RR250-C300/A1 engine, sometimes referred to as the RR300.
Year andnumber | Date of registration on FRL | Date ofcommencement | Application, saving ortransitional provisionsMOS 66 | 18 February 2011 (see F2011L00280) | 27 June 2011 | —Amendment of MOS 66 2011 | 2 June 2011 (see F2011L00910) | 3 June 2011 | —MOS 66 2011 Amendment No. 2 | 22 June 2011 (see F2011L01170) | 27 June 2011 | —MOS 66 2012 Amendment No. 1 | 10 April 2012 (see F2012L00803) | 11 April 2012 | —MOS 66 2012 Amendment No. 2 | 25 June 2012 (see F2012L01328) | 26 June 2012 | —MOS 66 2013 Amendment No. 1 | 17 July 2013 (see F2013L01399) | 18 July 2013 | Ss. 4 and 5 (see Table A)MOS 66 2014 Amendment No. 1 | 2 May 2014 (see F2014L00492) | 3 May 2014 | —MOS 66 2015 Amendment No. 1 | 26 June 2015 (see F2015L00945) | 27 June 2015 | —MOS 66 2016 Amendment No. 1 | 22 January 2016 (see F2016L00066) | 23 January 2016 | —MOS 66 2016 Amendment No. 2 | 29 March 2016 (see F2016L00390) | 30 March 2016 | —MOS 66 2016 Amendment No. 4 | 2 May 2016 (see F2016L00612) | 2 May 2016 | —MOS 66 2016 Amendment No. 5 | 29 August 2016 (see F2016L01357) | 29 August 2016 | S. 3 (see Table A)MOS 66 2017 Amendment No. 1 | 26 June 2017 (see F2017L00750) | 26 June 2017 | —MOS 66 2017 Amendment No. 2 | 3 October 2017 (see F2017L01313) | 4 October 2017 | —MOS 66 2017 Amendment No. 3 | 3 November 2017 (see F2017L01421) | 4 November 2017 | —MOS 66 2018 Amendment No. 1 | 21 May 2018 (see F2018L00640) | 22 May 2018 | S. 66.A.100MOS 66 2018 Amendment No. 2 | 16 November 2018 (see F2018L01577) | 17 November 2018 | —MOS 66 2019 Amendment No. 2 | 1 November 2019 (see F2019L01413) | 2 November 2019 | —MOS 66 2020 Amendment No. 1 | 3 July 2020 (see F2020L00874) | 4 July 2020 | —MOS 66 2020 Amendment No. 2 | 14 July 2020 (see F2020L00908) | 15 July 2020 | —MOS 66 2020 Amendment No. 3 | 24 December 2020 (see F2020L01710) | 25 December 2020 | —MOS 66 2021 Amendment No. 1 | 13 May 2021 (see F2021L00568) | 14 May 2021 | —MOS 66 2021 Amendment No. 2 | 4 January 2022 (see F2022L00007) | 5 January 2022 | —MOS 66 Amendment Instrument 2023 | 6 July 2023 (see F2023L00985) | 7 July 2023 | —Part 66 Manual of Standards and Part 147 Manual of Standards Amendment Instrument 2023 (No. 1) | 4 December 2023 (see F2023L01613) | 5 December 2023 | —Part 66 Manual of Standards Amendment Instrument 2024 (No. 1)10 December 2024 (see F2024L01634)S 3 (2) and Sch 2: 10 February 2025 (see F2025N00107)Remainder: 11 December 2024—Part 66 Manual of Standards Amendment Instrument 2025 | 16 December 2025 (see F2025L01593) | 17 December 2025 | —Part 66 Manual of Standards Amendment Instrument 2026 (No. 1) | 2 July 2026 (see F2026L00794) | 3 July 2026 | —Part 66 Manual of Standards Amendment Instrument 2026 (No. 2) | 2 July 2026 (see (F2026L00893) | 3 July 2026 | —Table of Amendmentsad. = added or inserted am. = amended rep. = repealed rs. = repealed and substitutedProvision affected | How affectedPower to make......... | am. MOS 66 2011 No. 1s. 1..................(Now numbered 66.1A) | rs. MOS 66 2011 No. 2s. 2Renumbered s. 66.1B .. | MOS 66 2011 No. 2s. 3 ................. | rep. MOS 66 2011 No. 2Schedule heading ....... | rep. MOS 66 2011 No. 2Part 1 heading ......... | ad. MOS 66 2016 No. 5MOS title.............. | rep. MOS 66 2011 No. 2Part 2 heading ......... | ad. MOS 66 2016 No. 5s. 66.1B.............. | rep. Legislation Act 2003, s. 48Ds. 66.5............... | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2015 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5, F2021L00568, F2023L01613, F2024L01634, F2025L01593, F2026L00893s. 66.6............... | ad. F2021L00568s. 66.A.1.............. | am. MOS 66 2014 No. 1, MOS 66 2016 No. 1s. 66.A.4.............. | am. MOS 66 2016 No. 5, F2020L01710, F2025L01593s. 66.A.20............. | am. MOS 66 2011 No. 2, MOS 66 2012 No. 1, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5, MOS 66 2017 No. 3, F2020L00874, F2021L00568, F2023L01613, F2024L01634s. 66.A.21............. | ad. MOS 66 2014 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5s. 66.A.23............. | am. MOS 66 2014 No. 1, MOS 66 2016 No. 1s. 66.A.25............. | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2015 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5, F2020L00874, F2021L00568, F2022L00007, F2023L01613, F2024L01634, F2026L00893s. 66.A.30............. | am. MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2015 No. 1, MOS 66 2016 No. 1, F2020L00874, F2021L00568, F2023L01613, F2024L01634, F2025L01593s. 66.A.35 | ad. F2023L01613s. 66.A.45............. | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2015 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5, F2020L00874, F2021L00568, F2024L01634s. 66.A.50............. | am. MOS 66 2012 No. 2, MOS 66 2013 No. 1s. 66.A.55............. | am. MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2016 No. 5, F2021L00568s. 66.A.56.............ad. MOS 66 2015 No. 1rs. F2024L01634s. 66.A.57.............ad. MOS 66 2015 No. 1rep. F2024L01634s. 66.A.58.............ad. MOS 66 2015 No. 1rep. F2024L01634am. MOS 66 2017 No. 1, F2020L00874s. 66.A.70.............am. MOS 66 2016 No. 1, F2023L01613, F2024L01634rs F2026L00893s. 66.A.75............. | ad. F2026L00893s. 66.A.100............ | ad. MOS 66 2018 No. 1Appendix I............. | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2016 No. 1, MOS 66 2018 No. 2, F2021L00568, F2023L01613, F2024L01634Appendix II............ | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, F2021L00568, F2023L01613, F2024L01634Appendix III............ | am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2016 No. 1Appendix IV...........am. MOS 66 2012 No. 1, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2016 No. 1, MOS 66 2018 No. 1, MOS 66 2018 No. 2, MOS 66 2019 No. 1, F2023L01613rs. MOS 66 2016 No. 5am. F2024L01634Appendix V............rs. MOS 66 2011 No. 2rs. F2026L00794Appendix VI........... | rs. MOS 66 2011 No. 2Appendix VII...........am. MOS 66 2011 No. 2, MOS 66 2016 No. 1, MOS 66 2016 No. 5rs. F2023L01613am. F2026L00893Appendix VIII...........ad. MOS 66 2013 No. 1am. MOS 66 2016 No. 1rs. MOS 66 2016 No. 5am. MOS 66 2018 No. 2, F2020L00908, F2023L01613rs. F2024L01634Appendix IX...........ad. MOS 66 2014 No. 1am. MOS 66 2016 No. 1, MOS 66 2016 No. 2, MOS 66 2016 No. 4, MOS 66 2016 No. 5, MOS 66 2017 No. 1, MOS 66 2017 No. 2, MOS 66 2017 No. 3, MOS 66 2018 No. 1, MOS 66 2018 No. 2. MOS 66 2019 No. 1, F2020L00908, F2020L01710, F2022L00007, F2023L00985, F2024L01634, F2025L01593Appendix X............ | ad. F2024L01634Table A Application, saving or transitional provisionsPart 66 Manual of Standards Amendment Instrument 2013 (No. 1)
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