Untitled document
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 November 2017 taking into account amendments up to Part 66 Manual of Standards Amendment Instrument 2017 (No. 3). It is a compilation of the Part 66 Manual of Standards (MOS) as amended and in force on 4 November 2017.
Prepared by the Legal Advisory, Drafting and Contracts Section, Legal Affairs, Regulatory Policy and International Strategy Branch, Civil Aviation Safety Authority, Canberra.
Compilation No. 14.
Contents
Page
Part 1........ Preliminary....................................................................................................... 2
66.1A........ Name of instrument............................................................................................ 2
66.1B........ Commencement................................................................................................. 2
66.1.......... Scope................................................................................................................ 2
66.5.......... Definitions......................................................................................................... 2
66.A.1....... Aircraft engineer licence...................................................................................... 5
Part 2........ Aircraft engineer licences for type-rated aircraft etc........................................... 5
66.A.4....... Certain type-rated aircraft types and endorsements etc......................................... 5
66.A.10..... Application — form............................................................................................ 5
66.A.20..... Privileges........................................................................................................... 6
66.A.21..... Transitional privileges........................................................................................ 13
66.A.23..... Requalification requirements.............................................................................. 14
66.A.25..... Basic knowledge and competency requirements................................................. 15
66.A.30..... Basic practical experience requirements............................................................. 16
66.A.45..... Type/task training and ratings............................................................................ 18
66.A.50..... Aircraft type practical training............................................................................ 21
66.A.55..... On the Job aircraft type Training........................................................................ 21
66.A.56..... Use of CAR 31 for removal of exclusion from a Part 66 licence on or after 27 June 2015 22
66.A.57..... Use of CAR 31 for removal of exclusion from a Part 66 rating on or after 27 June 2015 22
66.A.58..... Exemptions to facilitate the operation of certain provisions................................ 22
66.A.60..... Recognised States........................................................................................... 23
66.A.65..... Excluded States............................................................................................... 23
66.A.70..... Limitations........................................................................................................ 23
Appendix I........................................................................................................ 24
Appendix II....................................................................................................... 82
Appendix III...................................................................................................... 86
Appendix IV.................................................................................................... 100
Appendix V.................................................................................................... 108
Appendix VI.................................................................................................... 109
Appendix VII................................................................................................... 110
Appendix VIII.................................................................................................. 112
Appendix IX.................................................................................................... 118
Note to Part 66 Manual of Standards (MOS)..................................................... 142
Part 1 Preliminary
66.1A Name of instrument
This instrument is the Part 66 Manual of Standards (MOS).
66.1B Commencement
This instrument commences on 27 June 2011.
66.1 Scope
(a) This is the MOS for Part 66 of the Civil Aviation Safety Regulations1998 (CASR 1998).
(b) This MOS sets out the requirements for the issue of an aircraft engineer licence and other requirements or privileges associated with the licence.
66.5 Definitions
(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:
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.
avionics system means an aircraft system as specified in Table 1. An avionics system transfers, processes, displays or stores analogue or digital data using data lines, wireless or other data transmission medium, and includes the system’s components and connectors. Examples of avionics systems include the following:
1. autoflight;
2. communication 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 Air Transport Association (ATA) 27 “Flight Controls”);
10. fibre optic control systems.
CAR 1988, or CAR, means the Civil Aviation Regulations 1988.
CASR 1998 means the Civil Aviation Safety Regulations 1998.
CAO means Civil Aviation Order.
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. 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.
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.
Part 66 licence means an aircraft engineer licence issued under Part 66 of CASR 1998.
Part 66 rating means a rating on an aircraft engineer licence, issued under Part 66 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; and
2. 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; and
2. 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; and
3. 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; and
4. 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.
RPL has the same meaning as in section 147.A.07 of the Part 147 Manual of Standards (as amended).
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; or
2. 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.
66.A.1 Aircraft engineer licence
(a) This MOS specifies the requirements for the issue of an aircraft engineer licence in 1 or more of the following categories:
1. Category A;
2. Category B1;
3. Category B2;
4. Category C.
(b) Categories A and B1 may be endorsed with the following subcategories for maintenance on combinations of aeroplanes, helicopters, turbine and piston engines:
1. A1 and B1.1 aeroplanes turbine;
2. A2 and B1.2 aeroplanes piston;
3. A3 and B1.3 helicopters turbine;
4. A4 and B1.4 helicopters piston.
Part 2 Aircraft engineer licences for type-rated aircraft etc.
66.A.4 Certain type-rated aircraft types and endorsements etc.
(a) Subject to paragraph (f), for paragraph 66.015 (2) (e) of CASR 1998, an aircraft type specified in a cell in column 2 of a table in Appendix IX, with a type certificate holder (if any) mentioned in the corresponding cell in column 1, and a commercial designation (if any) mentioned in the corresponding cell in column 3, is specified as a type rated aircraft type for an aircraft engineer licence in Category B1, B2 or C.
(b) Subject to paragraph (f), for an aircraft type specified in a cell in column 2 of a table in Appendix IX, an aircraft engineer licence in Category B1, B2 or C may be endorsed with the type-rating endorsement mentioned in the corresponding cell in column 4.
(c) Each mention of “Various” in a cell in column 2 of a table in Appendix IX is to be read as “A small/non-rated aircraft with the engine mentioned in the corresponding cell in column 4.”.
(d) If a Note referred to in a cell in column 4 of a table in Appendix IX contains the statement: “This is a rule.”, the contents of the Note have legal effect for the cell in the table as if they were contained in a paragraph of this section.
66.A.10 Application — form
An application for an aircraft engineer licence, or an application for a variation of an aircraft engineer licence, must be made to CASA in the form approved by CASA.
66.A.20 Privileges
(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 avionics 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.
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, between 27 June 2015 and 3 July 2020:
(i) satisfies the requirements of each of paragraphs 66.A.25 (i), 66.A.30 (f), and 66.A.45 (j) of this MOS; and
(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, is 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.
Note 27 June 2015 was the operative date for use of regulation 31 of CAR 1988 to obtain an equivalent AME licence (see paragraphs 66.A.25 (i), 66.A.30 (f) and 66.A.45 (j) of this MOS). 3 July 2020 is the date of repeal of regulation 202.345 of CASR 1998 which enables transitional use of regulation 31 to qualify for Category B1 (and B2) licences (see subregulation 202.345 (3) inserted by item 30 of the Civil Aviation Legislation Amendment (Part 66) Regulation 2015).
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.
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 1
Aircraft systems, designations and conditions for Category B1 and Category B2 licences
Aircraft system (and ATA chapter reference) Designation of system Conditions or limitations Pressurisation, 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:
· General
· Radio interface
· ACARS, SELCAL, INS/IRS
· Compass
· Flight manage-ment system
· Doppler 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 systems
· ATIMS
· Network 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; or
Note 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) 66.A.21 Transitional privileges
Despite Table 1 in section 66.A.20 and the exclusions annotated on a licence issued under Part 66 of CASR 1998, a person mentioned in a cell in column 1 of Table 2, who holds a Category B1 licence, may perform maintenance certifications and issue certificates of release to service for the maintenance mentioned for the person in the corresponding cell or cells in column 2, but only:
1. for an aircraft mentioned in the corresponding cell in column 3; and
2. subject to the limitations (if any) mentioned in the corresponding cell in column 4; and
3. subject to the condition mentioned in column 5.
Table 2
Person Maintenance Aircraft Limitations Condition A.
A person who held an aircraft maintenance engineer (AME) licence under regulation 31 of the Civil Aviation Regulations 1988 to which regulation 202.341, as in force immediately before 15 December 2015, applied (the old licence)
All electrical maintenance An aircraft approved for V.F.R. operations only (approved V.F.R. aircraft), and fitted with a single generator Not applicable (NA) Provided that the old licence and its ratings applied to the maintenance, or would have applied to the maintenance but for Part 66 of CASR 1998 (The Proviso) 1. All instrument system maintenance for aircraft general instruments (excluding RMI, inertial navigation and multi-axis autopilots)
2. Periodic inspections for aircraft radio systems
Approved V.F.R. aircraft
Approved V.F.R. aircraft
NA B.
A person who, in accordance with subregulation 202.343 (2) or 202.344 (2) of CASR 1998, as in force immediately before 15 December 2015, was taken to be entitled to the issue of an AME licence by becoming qualified for, an engine category Group 1 or 2 rating, or an airframe category Group 1, 2 or 19 rating (the old licence)
All electrical maintenance Approved V.F.R. aircraft fitted with a single generator NA The Proviso 1. All instrument system main-tenance for aircraft general instruments (excluding RMI, inertial navigation and multi-axis autopilots)
2. Periodic inspections for aircraft radio systems
66.A.23 Requalification requirements
(a) For paragraph 66.120 (2) (b) of CASR 1998, a licensed aircraft maintenance engineer is taken to comply with the requirements of that paragraph if, in the immediately preceding 2 years:
1. he or she has had a period or periods of continuous employment amounting to at least 6 months, exercising the privileges mentioned in the Part 66 Manual of Standards for his or her licence or for a rating endorsed on the licence; or
2. within a period or periods of time amounting to 6 months, he or she has had at least 550 hours of experience in exercising those privileges.
(b) For paragraph 66.120 (2) (c) of CASR 1998, the requalification requirements for an A, B1 or B2 aircraft engineer licence holder are:
1. carrying out maintenance (as an AME) of the kind that would be covered by the privileges of any of the licences held, for no less than a total of 100 days and retaining evidence of carrying out the maintenance; or
2. the holder obtains a report from an MTO authorised for category training or aircraft type training which states:
(i) that the holder has been assessed within 28 days of the date of the report; and
(ii) how the assessment was conducted — the assessment must include theory examination and practical assessment in a sampling of the range of maintenance activities that the holder is authorised by their licence and ratings to carry out; and
(iii) that the MTO has certified that the holder continues to have the knowledge and skills necessary for the holder of an aircraft engineer licence with the ratings on the licence; or
3. the holder is assessed by an AMO, or an organisation holding a certificate of approval to carry out maintenance activities issued under regulation 30 of CAR 1988, to determine that he or she continues to have the knowledge and skills necessary for the holder of an aircraft engineer licence with the ratings on the licence, and the assessment follows a process for requalifying individuals based on Australian competency-based training (CBT) standards and outlined in:
(i) for the AMO — the AMO’s exposition; or
(ii) for the organisation holding a certificate of approval under regulation 30 of CAR 1988 — the organisation’s system of quality control.
(c) For paragraph 66.120 (2) (c) of CASR 1998, the requalification requirement for a Category C licence holder is that the AMO provides the holder with suitable continuing airworthiness experience to ensure that the holder has re-established their knowledge and skill.
66.A.25 Basic knowledge and competency requirements
(a) This section sets out the requirements that must be met by a person who applies for:
1. an aircraft engineer licence in a category or subcategory; or
2. the addition of a category or subcategory to the person’s licence.
(b) The applicant must demonstrate by examination, conducted by an MTO, knowledge:
1. of each subject module that is marked as applicable for the licence category or subcategory in accordance with Part 2 of Appendix I in this MOS; and
2. of each subject or item in a module in Part 3 of Appendix I that is marked in column 2, 3 or 4 of the table by a level of knowledge numeral as being applicable for the licence category or subcategory; and
3. to the corresponding level of knowledge for the subject or item; and
4. in accordance with Appendix II of this MOS or as otherwise approved in writing by CASA.
(ba) Where the applicability symbol – (a dash) – appears in a row of a column of the table in Part 3 of Appendix I that is for a licence category or subcategory, knowledge of the subject or item mentioned in the same row is not required for the category or subcategory (as the case may be).
(c) An applicant for a subcategory A1 or B1.1 licence is not required to demonstrate, by examination, knowledge of propellers in accordance with item 17 in Part 2 of Appendix I to this MOS unless the rating is to include propellers.
(d) An applicant for a subcategory A2 or B1.2 licence is not required to demonstrate, by examination, knowledge of high speed flight in accordance with subitem 11.1.2 of subject Module 11 in Part 3 of Appendix I to this MOS.
(e) An applicant must hold each unit of competency listed and coded in Appendix IV to this MOS that is marked X or indicated as its alternative for the category or subcategory and, before holding a unit of competency, hold the qualifications or units of competency that are prerequisites for the unit.
(f) 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 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; and
2. Z — for fabric surfaces for the subcategory; and
3. 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 qualification (comprised of knowledge, competence and assessments) must have been gained within 5 years of making an application for an aircraft maintenance licence or the addition of a category or subcategory to an aircraft maintenance licence.
(ha) The academic qualifications required to satisfy the 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.
Use of CAR 31 to obtain the equivalent of an AME licence on or after 27 June 2015
(i) Despite anything in paragraphs (b) to (h) of this section, a person who, if regulation 31 were still in force, would meet the requirements of regulation 31 for the issue of an AME licence in a category mentioned in paragraph (j) is taken to meet the requirements of paragraphs (b) to (h) for the issue of the Part 66 licence that is equivalent to the licence that would have been issued for the category if regulation 31 were still in force.
(j) The licence categories mentioned in paragraph (i) are as follows:
1. a licence in category airframes;
2. a licence in category engines;
3. a licence in category radio;
4. a licence in category electrical;
5. a licence in category instruments.
66.A.30Basic practical experience requirements
(a) An applicant for an aircraft engineer licence must have acquired the following practical experience:
1. for a Category A and subcategories B1.2 and B1.4 licences — practical maintenance experience in carrying out maintenance on operating aircraft and in training as mentioned in the following table.
Licence category Amount of practical experience A licence 2 years B1.2 or B1.4 licence 3 years
2. for Category B2 and subcategories B1.1 and B1.3 licences — practical maintenance experience in carrying out maintenance on operating aircraft and in training as mentioned in the following table.
Licence category Amount of practical experience B1.1 or B1.3 licence or B2 licence 4 years
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 in a technical discipline from a university or other higher educational institution recognised by CASA, 3 years experience carrying out maintenance on operating aircraft, including at least 6 months of observation of base maintenance tasks within that 3 year period.
(b) A person who holds a licence with a category or subcategory, who applies to CASA to add a category or subcategory to it, must provide evidence to CASA that he or she has been certified by an MTO as satisfying all of the following requirements for the category or subcategory to be added:
1. completion of the knowledge and examination requirements mentioned in Appendix I to this MOS; and
2. holding the units of competency required by Appendix IV to this MOS; and
3. having the practical maintenance experience on operating aircraft detailed in subparagraphs (a) 1 and 2.
(c) In this section:
practical maintenance experience on operating aircraft may include 1 year of category training maintenance experience, such as:
1. simulated maintenance experience using maintenance simulation technology; and
2. practical maintenance experience on representative aeronautical products during maintenance training.
(d) At least 1 year of the practical maintenance experience required for an initial issue of an aircraft engineer licence must be:
1. maintenance experience on aircraft relevant to the category or subcategory for which the licence was sought; and
2. accumulated immediately before making the application for the licence.
(e) Practical aircraft maintenance experience gained outside a civil aircraft maintenance environment can be treated as practical maintenance experience if an MTO certifies to CASA that:
1. the experience is equivalent to the practical experience required by this MOS; and
2. the applicant has sufficient additional experience with civil aircraft maintenance to ensure he or she has an understanding of the civil aircraft maintenance environment.
Use of CAR 31 to obtain the equivalent of an AME licence on or after 27 June 2015
(f) Despite anything in paragraphs (a) to (e) of this section, a person who, if regulation 31 were still in force, would meet the requirements of regulation 31 for the issue of an AME licence in a category mentioned in paragraph (g) is taken to meet the requirements of paragraphs (a) to (e) for the issue of the Part 66 licence that is equivalent to the licence that would have been issued for the category if regulation 31 were still in force.
(g) The licence categories mentioned in paragraph (f) are as follows:
1. a licence in category airframes;
2. a licence in category engines;
3. a licence in category radio;
4. a licence in category electrical;
5. a licence in category instruments.
66.A.45 Type/task training and ratings
(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; and
2. 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; or
2. 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); or
2. 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; and
2. 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 as specified in sub-subparagraph 66.A.30 (a) 3 (iii), 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; and
2. 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; or
2. 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; or
3. 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 basic practical experience requirements specified in paragraph 66.A.30 (b).
Use of CAR 31 to obtain the equivalent of a Group rating on an AME licence on or after 27 June 2015
(j) Despite anything in paragraphs (a) to (i) of this section, a person who, if regulation 31 were still in force, would meet the requirements of regulation 31 for the issue of a Group rating for a category of AME licence mentioned in paragraph (k) is taken to meet the requirements of paragraphs (a) to (i) of this section for the issue of the Part 66 rating that is equivalent to the Group rating that would have been issued for the category if regulation 31 were still in force.
(k) The licence categories and Group ratings mentioned in paragraph (j) are as follows:
1. a licence in category airframes, with a Group 1, 2, 3, 4, 5, 6, 10 or 19 rating, provided that, for Groups 1, 2 and 19, the airframe is not a type rated aircraft type;
2. a licence in category engines, with a Group 1, 2, 3, 21 or 22 rating, provided that, for Group 21 and Group 22, the engine is fitted to a small aircraft;
Note Small aircraft is defined in Part 3 of the Dictionary in CASR 1998. Part 3 contains definitions for Part 66 of CASR 1998. Under paragraph 66.5 (a) of this MOS, words and phrases generally have the same meaning as in Part 66.
3. a licence in category radio, with a Group 1, 2, 3, 4, 5, 6, 7, 9, 10 or 12 rating, provided that the airframe is not a type rated aircraft type;
4. a licence in category electrical, with a Group 1 or 2 rating, provided that the airframe is not a type rated aircraft type;
5. a licence in category instruments, with a Group 1, 3, 5, 7, 8, 9 or 10 rating, provided that the airframe is not a type rated aircraft type.
66.A.50Aircraft type practical training
(a) Aircraft type practical training and assessment must include a representative cross‑section of maintenance activities relevant to the category or subcategory.
(b) Practical training must be of fixed content and duration and, except in the case of PCT, can be conducted by either an MTO or an appropriately approved AMO. In the case of PCT, only an MTO approved to conduct PCT may deliver and assess the training. Where practical training is conducted by an appropriately approved maintenance organisation, the practical training must be first approved by CASA. The practical training must be supported by a detailed syllabus or practical worksheets/logbook showing content and duration of training.
(ba) The practical element of type training may be conducted simultaneously with the conduct of the theoretical element or provided separately as a stand-alone element.
(bb) Options for practical training include:
1. PCT; or
2. practical on course (POC) training; or
3. structured OJT performed according to a type-specific program.
(c) Practical training can be performed by demonstrations using equipment, components, simulators, other training devices or aircraft. This training does not need to involve actual servicing or repair of aircraft.
(d) Records of demonstration of practical training must be retained by the organisation conducting the practical training for at least 5 years following completion of the practical training.
(e) Practical training must meet the requirements of Appendix III to this MOS.
66.A.55 On the Job aircraft type Training
(a) In the case of a first type rating to be gained, PCT or POC alone is not acceptable for type rating endorsement. In addition to PCT or POC, an applicant must also complete on the job training (OJT).
(aa) In the case of a rating in another licence category or subcategory to be obtained after the type rating referred to in paragraph (a):
1. if using POC training, POC training must be supplemented by OJT; and
2. if using PCT training, no supplementation by OJT is required.
(b) OJT, other than that normally required as part of a PCT course, is not required in the case of a second or subsequent type rating if the practical training for the second or subsequent type rating (in the same or any other category or subcategory) is delivered using PCT.
(c) OJT:
1. may only be conducted and managed by a maintenance organisation, or a maintenance training organisation, approved by CASA to undertake such training activities; and
2. must be supported by a detailed syllabus of OJT content which includes provision for completion of the OJT to be recorded in detailed worksheets or logbooks; and
3. must be assessed and approved by CASA.
Note CASA’s assessment and approval are guided by Appendix II of the Part 66 Acceptable Means of Compliance (ACM) and Guidance Material (GM) document, and Advisory Circular AC 66-07 – Practical training options for aircraft type training and recording of recent work experience (both of which are amended from time to time).
(ca) For paragraph (c), the maintenance organisation approved by CASA must be:
1. an approved maintenance organisation (AMO) issued with an approval under regulation 145.030 of CASR 1998 to carry out maintenance activities; or
2. an organisation holding a certificate of approval to carry out maintenance activities issued under regulation 30 of the Civil Aviation Regulations 1988.
(d) OJT must be supervised and assessed by approved assessors.
(e) OJT must comply with the requirements of Appendix III to this MOS.
66.A.56 Use of CAR 31 for removal of exclusion from a Part 66 licence on or after 27 June 2015
(a) This section applies to a person (the Part 66 licence holder) who holds a Part 66 licence that is subject to the exclusion of a particular aircraft system or a subset of an aircraft system (a particular exclusion).
Note Part 66 licence holder includes a person who holds a Part 66 licence subject to a particular exclusion, as a result of the operation of paragraphs 66.A.25 (i) and 66.A.30 (f) of this MOS.
(b) If the Part 66 licence holder would meet the requirements of regulation 31 for the issue of a category of AME licence mentioned in paragraph 66.A.25 (i) or 66.A.30 (f) without a particular exclusion, were regulation 31 still in force, then the holder is taken to meet the requirements of sections 66.A.25 and 66.A.30 of this MOS for the issue of the Part 66 licence without the particular exclusion.
66.A.57 Use of CAR 31 for removal of exclusion from a Part 66 rating on or after 27 June 2015
(a) This section applies to a person (the Part 66 rating holder) who holds a Part 66 rating that is subject to the exclusion of a particular aircraft system or a subset of an aircraft system (a particular exclusion).
Note Part 66 rating holder includes a person who holds a Part 66 rating subject to a particular exclusion, as a result of the operation of paragraph 66.A.45 (j) of this MOS.
(b) If the Part 66 rating holder would meet the requirements of regulation 31 for the issue of a Group rating on a category of AME licence without the particular exclusion, were regulation 31 still in force, then the holder is taken to meet the requirements of section 66.A.45 of this MOS for the issue of the Part 66 rating without the particular exclusion.
66.A.58 Exemptions to facilitate the operation of certain provisions
(a) A person to whom paragraph 66.A.25 (i), paragraph 66.A.30 (f) or section 66.A.56 of this MOS applies is exempt from subregulation 66.072 (3) of CASR 1998.
(b) A person to whom paragraph 66.A.45 (j) or section 66.A.57 of this MOS applies is exempt from each of the following provisions of CASR 1998:
1. paragraph 66.080 (1) (b);
2. subregulations 66.080 (2) and (3);
3. paragraphs 66.095 (1) (c) and (2) (d);
4. regulation 66.100; and
5. paragraph 66.110 (2) (a).
(c) Each exemption mentioned in paragraphs (a) and (b) expires at the end of 25 June 2020.
66.A.60 Recognised States
For the purposes of regulation 66.030 of CASR 1998, recognised States are set out in Appendix V.
66.A.65 Excluded States
For the purposes of regulation 66.060 of CASR 1998, excluded States are set out in Appendix VI.
66.A.70 Limitations
(a) Limitations introduced on an aircraft maintenance licence are exclusions from the certification privileges and apply to the aircraft in its entirety.
(b) Exclusions annotated on a category can be removed by gaining the section 66.A.25 basic knowledge and competency requirements relevant to the exclusion removal.
(c) Exclusions annotated on a rating can be removed by CASA after satisfactorily completing, as required:
1. paragraph 66.A.45 (d) training and examination; with
2. section 66.A.50 practical training and assessment; or
3. section 66.A.55 on the job training and assessment.
The training, assessment and examination may be provided by an MTO or, if described in its Part 145 AMO exposition, by an AMO if the exclusion removal has been permitted under subparagraph 66.100 (a) (ii) of CASR 1998, using a training and assessment regime provided in accordance with paragraph 145.025 (3) (c) of CASR 1998.
(d) For the purposes of subregulation 66.095 (2), and Subpart 202.GG, of CASR 1998, exclusions on type ratings, that an AMO may be authorised to provide training, assessment and authorisations for, are set out in Appendix VII.
(e) Units of competency are required as mentioned in Appendix VIII before the removal of an exclusion from a category or subcategory of licence in accordance with paragraph (b).
Appendix I
CASA knowledge syllabus
Part 1 — Levels of knowledge
Levels of knowledge
The level of knowledge for a module, or part of a module, for a Category A, B1 or B2 licence is indicated in Part 3 of this Appendix by the allocation of a numerical indicator (1, 2 or 3) against the module or part. A level of knowledge has the meaning given to it below.
Level 1
A familiarisation with the principal elements of the subject such that the following objectives are met.
Objectives:
1 The applicant must be familiar with the basic elements of the subject.
2 The applicant must be able to give a simple description of the whole subject, using common words and examples.
3 The applicant must be able to use typical terms.
Level 2
A general knowledge of the theoretical and practical aspects of the subject and an ability to apply that knowledge, such that the following objectives are met.
Objectives:
1 The applicant must be able to understand the theoretical fundamentals of the subject.
2 The applicant must be able to give a general description of the subject using, as appropriate, typical examples.
3 The applicant must be able to use mathematical formulae in conjunction with physical laws describing the subject.
4 The applicant must be able to read and understand sketches, drawings and schematics describing the subject.
5 The applicant must be able to apply his or her knowledge in a practical manner using detailed procedures.
Level 3
A detailed knowledge of the theoretical and practical aspects of the subject, and a capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner, such that the following objectives are met.
Objectives:
1 The applicant must know the theory of the subject and interrelationships with other subjects.
2 The applicant must be able to give a detailed description of the subject using theoretical fundamentals and specific examples.
3 The applicant must understand and be able to use mathematical formulae related to the subject.
4 The applicant must be able to read, understand and prepare sketches, simple drawings and schematics describing the subject.
5 The applicant must be able to apply his or her knowledge in a practical manner using manufacturer’s instructions.
6 The applicant must be able to interpret results from various sources and measurements and apply corrective action where appropriate.
Part 2 — Knowledge module requirements
Qualification on basic subjects for each category or subcategory of licence must be in accordance with the following table. Applicable subjects are indicated by an X.
Subject modules
A or B1 aeroplane with:
A or B1 helicopter with:
B2
Turbine engine(s)
Piston engine(s)
Turbine engine(s)
Piston engine(s)
Avionics
1 Mathematics X X X X X 2 Physics X X X X X 3 Electrical fundamentals X X X X X 4 Electronic fundamentals X X X X X 5 Digital techniques electronic instrument systems X X X X X 6 Materials and hardware X X X X X 7 Maintenance practices X X X X X 8 Basic aerodynamics X X X X X 9 Human factors X X X X X 10 Aviation legislation X X X X X 11 Aeroplane aerodynamics, structures and systems X X 12 Helicopter aerodynamics, structures and systems X X 13 Aircraft structures and systems X 14 Propulsion —
avionic systemsX 15 Gas turbine engine X X 16 Piston engine X X 17 Propeller X X Part 3 — Details of modules and levels of knowledge
Module 1 Mathematics
Level of knowledge for the category
A
B1
B2
1.1 Arithmetic 1 2 2 Arithmetical terms and signs, methods of multiplication and division, fractions and decimals, factors and multiples, weights, measures and conversion factors, ratio and proportion, averages and percentages, areas and volumes, squares, cubes, square and cube roots.
1.2 Algebra (a) 1 2 2 Evaluating simple algebraic expressions, addition, subtraction, multiplication and division, use of brackets, simple algebraic fractions; (b) — 1 1 Linear equations and their solutions;
Indices and powers, negative and fractional indices;
Binary and other applicable numbering systems;
Simultaneous equations and second degree equations with one unknown;
Logarithms.
1.3 Geometry (a) — 1 1 Simple geometrical constructions; (b) 2 2 2 Graphical representation, nature and uses of graphs, graphs of equations and functions; (c) — 2 2 Simple trigonometry, trigonometrical relationships, use of tables and rectangular and polar coordinates. Module 2 Physics
Level of knowledge for the category
A
B1
B2
2.1 Matter 1 1 1 Nature of matter: the chemical elements, structure of atoms, molecules;
Chemical compounds;
States: solid, liquid and gaseous;
Changes between states.
2.2 Mechanics 2.2.1 Statics
1
2
1
Forces, moments and couples, representation as vectors;
Centre of gravity;
Elements of theory of stress, strain and elasticity: tension, compression, shear and torsion;
Nature and properties of solid, fluid and gas;
Pressure and buoyancy in liquids (barometers).
2.2.2 Kinetics
1
2
1
Linear 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 1 Mass;
Force, inertia, work, power, energy (potential, kinetic and total energy), heat, efficiency;
(b) 1 2 2 Momentum, conservation of momentum;
Impulse;
Gyroscopic principles;
Friction: nature and effects, coefficient of friction (rolling resistance).
2.2.4 Fluid dynamics
(a) 2 2 2 Specific gravity and density; (b) 1 2 1 Viscosity, 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 2 Temperature: thermometers and temperature scales: Celsius, Fahrenheit and Kelvin, heat definition;
(b) — 2 2 Heat capacity, specific heat;
Heat transfer: convection, radiation and conduction;
Volumetric expansion;
First and second law of thermodynamics;
Gases: ideal gases laws, specific heat at constant volume and constant pressure, work done by expanding gas;
Isothermal, adiabatic expansion and compression, engine cycles, constant volume and constant pressure, refrigerators and heat pumps;
Latent heats of fusion and evaporation, thermal energy, heat of combustion.
2.4 Optics (light) — 2 2 Nature 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 2 Wave motion: mechanical waves, sinusoidal wave motion, interference phenomena, standing waves;
Sound: speed of sound, production of sound, intensity, pitch and quality, Doppler effect.
Module 3 Electrical fundamentals
Level of knowledge for the category
A
B1
B2
3.1 Electron theory 1 1 1 Structure 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 2 Static electricity and distribution of electrostatic charges;
Electrostatic laws of attraction and repulsion;
Units of charge, Coulomb’s Law;
Conduction of electricity in solids, liquids, gases and vacuum.
3.3 Electrical terminology 1 2 2 The following terms, their units and factors affecting them: potential difference, electromotive force, voltage, current, resistance, conductance, charge, conventional current flow, electron flow. 3.4 Generation of electricity 1 1 1 Production of electricity by the following methods: light, heat, friction, pressure, chemical action, magnetism and motion. 3.5 DC sources of electricity 1 2 2 Construction and basic chemical action of: primary cells, secondary cells, lead acid cells, nickel cadmium cells, other Alkaline cells;
Cells connected in series and parallel;
Internal resistance and its effect on a battery;
Construction, materials and operation of thermocouples;
Operation of photo-cells.
3.6 DC circuits — 2 2 Ohms Law, Kirchoff’s Voltage and Current Laws;
Calculations using the above laws to find resistance, voltage and current;
Significance of the internal resistance of a supply.
3.7 Resistance and resistor (a) — 2 2 Resistance 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 1 Positive and negative temperature coefficient conductance;
Fixed resistors, stability, tolerance and limitations, methods of construction;
Variable resistors, thermistors, voltage dependent resistors;
Construction of potentiometers and rheostats;
Construction of Wheatstone Bridge.
3.8 Power — 2 2 Power, 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 2 Operation and function of a capacitor;
Factors affecting capacitance area of plates, distance between plates, number of plates, dielectric and dielectric constant, working voltage, voltage rating;
Capacitor types, construction and function;
Capacitor colour coding;
Calculations of capacitance and voltage in series and parallel circuits;
Exponential charge and discharge of a capacitor, time constants;
Testing of capacitors.
3.10 Magnetism (a) — 2 2 Theory 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 2 Magneto-motive force, field strength, magnetic flux density, permeability, hysteresis loop, retentivity, reluctance, saturation point, eddy currents, coercive force;
Precautions for care and storage of magnets.
3.11 Inductance and inductor — 2 2 Faraday’s Law;
Action of inducing a voltage in a conductor moving in a magnetic field;
Induction principles;
Effects of the following on the magnitude of an induced voltage: magnetic field strength, rate of change of flux, number of conductor turns;
Mutual induction;
The effect the rate of change of primary 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 2 Basic motor and generator theory;
Construction and purpose of components in DC generator;
Operation of, and factors affecting output and direction of, current flow in DC generators;
Operation of, and factors affecting output power, torque, speed and direction of rotation of DC motors;
Series wound, shunt wound and compound motors;
Starter generator construction.
3.13 AC theory 1 2 2 Sinusoidal waveform: phase, period, frequency, cycle;
Instantaneous, average, root mean square, peak, peak to peak current values and calculations of these values, in relation to voltage, current and power;
Triangular and square waves;
Single and 3 phase principles.
3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits — 2 2 Phase relationship of voltage and current in L, C and R circuits, parallel, series and series parallel;
Power dissipation in L, C and R circuits;
Impedance, phase angle, power factor and current calculations;
True power, apparent power and reactive power calculations.
3.15 Transformers — 2 2 Transformer construction principles and operation;
Transformer losses and methods for overcoming them;
Transformer action under load and no-load conditions;
Power transfer, efficiency, polarity markings;
Calculation of line and phase voltages and currents;
Calculation of power in a 3 phase system;
Primary and secondary current, voltage, turns ratio, power, efficiency;
Autotransformers.
3.16 Filters — 1 1 Operation, application and uses of the following filters: low pass, high pass, band pass, band stop. 3.17 AC generators — 2 2 Rotation 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 2 Construction, 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.
Module 4 Electronic fundamentals
Level of knowledge for the category
A
B1
B2
4.1 Semiconductors 4.1.1 Diodes
(a) — 2 2 Diode symbols;
Diode characteristics and properties;
Diodes in series and parallel;
Main characteristics and use of silicon controlled rectifiers (thyristors), light emitting diode, photo conductive diode, varistor, rectifier diodes;
Functional testing of diodes;
(b) — — 2 Materials, electron configuration, electrical properties;
P and N type materials: effects of impurities on conduction, majority and minority characters;
PN junction in a semiconductor, development of a potential across a PN junction in unbiased, forward biased and reverse biased conditions;
Diode parameters: peak inverse voltage, maximum forward current, temperature, frequency, leakage current, power dissipation;
Operation and function of diodes in the following circuits: clippers, clampers, full and half wave rectifiers, bridge rectifiers, voltage doublers and triplers;
Detailed operation and characteristics of the following devices: silicon controlled rectifier (thyristor), light emitting diode, Shottky diode, photoconductive diode, varactor diode, varistor, rectifier diodes, Zener diode.
4.1.2 Transistors (a) — 1 2 Transistor symbols;
Component description and orientation;
Transistor characteristics and properties;
(b) — — 2 Construction and operation of PNP and NPN transistors;
Base, collector and emitter configurations;
Testing of transistors;
Basic appreciation of other transistor types and their uses;
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) — — 2 Description and operation of logic circuits and linear circuits;
Introduction to operation and function of an operational amplifier used as: integrator, differentiator, voltage follower, comparator;
Operation and amplifier stages connecting methods: resistive capacitive, inductive (transformer), inductive resistive (IR), direct;
Advantages and disadvantages of positive and negative feedback.
4.2 Printed circuit boards — 1 2 Description 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) — — 2 Understanding 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.
Module 5 Digital techniques electronic instrument systems
Level of knowledge for the category
A
B1
B2
5.1 Electronic instrument systems 1 2 3 Typical systems arrangements and cockpit layout of electronic instrument systems.
5.2 Numbering systems — 1 2 Numbering systems: binary, octal and hexadecimal;
Demonstration of conversions between the decimal and binary, octal and hexadecimal systems and vice versa.
5.3 Data conversion — 1 2 Analogue data, digital data;
Operation and application of analogue to digital, and digital to analogue converters, inputs and outputs, limitations of various types.
5.4 Data buses — 2 2 Operation of data buses in aircraft systems, including knowledge of ARINC and other specifications.
5.5 Logic circuits (a) — 2 2 Identification of common logic gate symbols, tables and equivalent circuits;
Applications used for aircraft systems, schematic diagrams.
(b) — — 2 Interpretation of logic diagrams.
5.6 Basic computer structure (a) 1 2 — Computer terminology (including bit, byte, software, hard ware, CPU, IC and various memory devices such as RAM, ROM, PROM);
Computer technology (as applied in aircraft systems);
(b) — — 2 Computer related terminology;
Operation, layout and interface of the major components in a microcomputer including their associated bus systems;
Information contained in single and multi address instruction words;
Memory associated terms;
Operation of typical memory devices;
Operation, advantages and disadvantages of the various data storage systems.
5.7 Microprocessors — — 2 Functions performed and overall operation of a microprocessor;
Basic operation of each of the following microprocessor elements: control and processing unit, clock, register, arithmetic logic unit.
5.8 Integrated circuits — — 2 Operation and use of encoders and decoders;
Function of encoder types;
Uses of medium, large and very large scale integration.
5.9 Multiplexing — — 2 Operation, application and identification in logic diagrams of multiplexers and demultiplexers.
5.10 Fibre optics — 1 2 Advantages and disadvantages of fibre optic data transmission over electrical wire propagation;
Fibre optic data bus;
Fibre optic related terms, terminations;
Couplers, control terminals, remote terminals;
Application of fibre optics in aircraft systems.
5.11 Electronic displays — 2 2 Principles of operation of common types of displays used in modern aircraft, including cathode ray tubes, light emitting diodes and liquid crystal display.
5.12 Electrostatic sensitive devices 1 2 2 Special handling of components sensitive to electrostatic discharges;
Awareness of risks and possible damage, component and personnel anti‑static protection devices.
5.13 Software management control — 2 2 Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programs.
5.14 Electromagnetic environment — 2 2 Influence of the following phenomena on maintenance practices for electronic system:
EMC-electromagnetic compatibility;
EMI-electromagnetic interference;
HIRF-high intensity radiated field;
Lightning and lightning protection.
5.15 Typical electronic and digital aircraft systems — 2 2 General arrangement of typical electronic and digital aircraft systems and associated BITE testing such as:
· ACARS-ARINC communication and addressing and reporting system
· ECAM-electronic centralised aircraft monitoring
· EFIS-electronic flight instrument system
· EICAS-engine indication and crew alerting system
· FBW-fly-by-wire
· FMS-flight management system
· GPS-global positioning system
· IRS-inertial reference system
· TCAS-traffic alert collision avoidance system.
Appendix IX See paragraphs 66.A.1 (c) and (d)
Type rated aircraft types and type rating endorsements for Category B1, B2 or C licences
Note Large aircraft (aeroplanes over 5 700 kg maximum take-off weight (MTOW), multi-engine helicopters, and aircraft (including, where appropriate, a particular engine type) that CASA has designated as requiring a type rating, generally form the basis of the type rated aircraft types listed in Appendix IX. CASA has also designated certain small aircraft and specific engines as requiring a type rating on the basis that, taking into account issues such as complexity, new technology, ATSB recommendations or other safety issues, type training will enhance aviation safety.
Table 1
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)AIRBUS
A318-110 Series
A319-110 Series
A320-111
A320-210 Series
A321-110 Series
A321-210 Series
Airbus A318/A319/A320/A321 (CFM56)
A319-130 Series
A320-230 Series
A321-130 Series
A321-230 Series
Airbus A319/A320/A321 (IAE V2500)
A330-200 Series
A330-300 Series
Airbus A330
(GE CF6)A330-220 Series
A330-320 Series
Airbus A330
(PW 4000)A330-240 Series
A330-340 Series
Airbus A330
(RR RB 211 Trent 700)A350-900 Series Airbus A350
(RR Trent XWB)
A380-840 Series
Airbus A380
(RR RB211 Trent 900)AIRCRAFT INDUSTRIES
L-420
Let L-420
(Walter M601) Note 2ATR-GIE
Avions de Transport RégionalATR 42-200
ATR 42-300
ATR 42-200/300 Series
(PWC PW120)ATR 42-400
ATR 42-400/500/72-212A
(PWC PW120)ATR 42-500 42-500 ATR 42-400/500/72-212A
(PWC PW120)ATR 42-500 42-600 ATR 42-400/500/72-212A
(PWC PW120)ATR 72-212 A 72-500 ATR 42-400/500/72-212A
(PWC PW120)ATR 72-212 A 72-600 ATR 42-400/500/72-212A
(PWC PW120)BAE SYSTEMS (OPERATIONS) LTD BAe 146 Series 100
BAe 146 Series 200
BAe 146 Series 300
AVRO 146-RJ70
AVRO 146-RJ85
AVRO 146-RJ100
AVRO 146-RJ115
BAe 146/AVRO 146‑RJ
(Honeywell ALF500 Series)HS.748 Series 1
HS.748 Series 2
HS 748 Series 2A
HS 748 Series 2B
HS748
(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)
B707-100 Long Body Boeing 707/720
(PW JT3)B707-100B Long Body Boeing 707/720
(PW JT3)B707-100B Short Body Boeing 707/720
(PW JT3)B707-300B Series
B707-300C Series
B720
B720B
Boeing 707/720
(PW JT3)B717-200 MD 717-200
(RRD BR700‑715)B727 Series
B727-100 Series
B727C Series
B727-100C Series
B727-200 Series
Boeing 727
(PW JT8D)B737-300
B737-400
B737-500
Boeing 737-300/400/500 (CFM56) B737-600
B737-700
B737-800
B737-900
B737-900ER
Boeing 737-600/700/800/900 (CFM56) B737-7/8/9 Boeing 737-7/8/9 (CFM LEAP-1B) B747-400
B747-400D
B747-400F/SF/BCF
Boeing 747-400
(GE CF6)B747-400
B747-400F/SF/BCF
Boeing 747-400
(PW 4000)B747-400
B747-400F/SF/BCF
Boeing 747-400
(RR RB211)B757-200
B757-200PF
B757-300
Boeing 757-200/300
(RR RB211)B767-200
B767-300
Boeing 767-200/300
(PW 4000)B767-200
B767-300
Boeing 767-200/300
(PW JT9D)B767-200
B767-300
B767-300F
B767-400ER
Boeing 767‑200/300/400
(GE CF6)B777-200
B777-200LR
B777-300ER
Boeing 777-200/300
(GE 90)B777F Freighter Boeing 777-200/300
(GE 90)B777-200
B777-300
Boeing 777-200/300
(RR RB211 Trent 800)B787-8
B787-9
Dreamliner Boeing 787-8/-9
(GE GEnx)B787-8
B787-9
Dreamliner Boeing 787-8/-9
(RR RB211 Trent 1000)BOMBARDIER
BOMBARDIER
BD-100-1A10 Challenger 300
Challenger 350
Bombardier BD-100-1A10
(Honeywell AS907)BD-700-1A10 Global Express Bombardier BD-700 Series
(RRD BR710)BD-700-1A10 Global 6000 Bombardier BD-700 Series
(RRD BR710)BD-700-1A11 Global 5000 Bombardier BD-700 Series
(RRD BR710)BD-700-1A11 Global 5000 GVFD Bombardier BD-700 Series
(RRD BR710)CL-600-1A11 Challenger 600 Bombardier CL-600-1A11 (Honeywell ALF502) CL600-2A12
(601 Variant)Challenger 601 Bombardier CL‑600 ‑2A12/-2B16 (variant CL 601/601-3A/3R)
(GE CF34)CL600-2B16
(601-3A Variant)Challenger
601-3ABombardier CL‑600 ‑2A12/-2B16 (variant CL 601/601‑3A/3R)
(GE CF34)CL600-2B16
(601-3R Variant)Challenger
601-3RBombardier CL‑600 ‑2A12/-2B16 (variant CL 601/601-3A/3R)
(GE CF34)CL600-2B16
(604 Variant)Challenger 604
(MSN < 5701)Bombardier CL‑600 ‑2B16
(variant CL 604)
(GE CF34)CL600-2B16
(604 Variant)
Challenger 605 (MSN > 5701) Bombardier CL‑600 ‑2B16
(variant CL 604)
(GE CF34)CL600-2B19 Regional Jet Series 100 Bombardier CL-600-2B19
(GE CF34)DHC-8-102
DHC-8-103
DHC-8-106
DHC-8
Series 100
Bombardier
DHC-8-100/200/300
(PWC PW 120)DHC-8-201
DHC-8-202
DHC-8
Series 200Bombardier
DHC-8-100/200/300
(PWC PW 120)DHC-8-301
DHC-8-311
DHC-8-314
DHC-8-315
DHC-8
Series 300Bombardier
DHC-8-100/200/300
(PWC PW 120)DHC-8-401
DHC-8-402
DHC-8
Series 400Bombardier
DHC-8-400
(PWC PW150)CESSNA
AIRCRAFT
CompanyCESSNA
AIRCRAFT
Company510 Cessna 510
(PWC PW615)525 Citation Jet CJ1
Citation M2
Cessna 525/525A
(Williams FJ44)525A Citation Jet CJ2 Cessna 525/525A
(Williams FJ44)525B Citation Jet CJ3 Cessna 525B
(Williams FJ44)525C Citation Jet CJ4 Cessna 525C
(Williams FJ44)550 Citation Bravo Cessna 550/560
(PWC PW530/535)
560 Citation Encore Cessna 550/560
(PWC PW530/535)560 Citation Encore+ Cessna 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 V Cessna 550/551/560
(PWC JT15D)560 Citation Ultra Cessna 550/551/560
(PWC JT15D)560 XL Citation Excel Cessna 560XL/XLS
(PWC PW545)560 XLS Citation XLS Cessna 560XL/XLS
(PWC PW545)560 XLS+ Citation XLS+ Cessna 560XL/XLS
(PWC PW545)650 Citation III-VI Cessna 650
(Honeywell TFE731)650 Citation VII Cessna 650
(Honeywell TFE731)680 Sovereign
Sovereign+
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) DASSAULT
AVIATIONDASSAULT
AVIATIONFalcon 10 Falcon 10
(Honeywell TFE731)Fan Jet Falcon
Series C
Series D
Series E
Series F
(Basic) Fan Jet Falcon Falcon 20
(GE CF700)Mystère Falcon 20-C5
Mystère Falcon 20-D5
Mystère Falcon 20-E5
Mystère Falcon 20-F5
Falcon 20-5
(Honeywell TFE731)Fan Jet Falcon Series G
Mystère Falcon 200
Mystère Falcon 20GF
Falcon 200
(Honeywell ATF 3-6)Mystère Falcon 50 50 Falcon 50
(Honeywell TFE731)Mystère Falcon 50 50EX Falcon 50EX
(Honeywell TFE731)Mystère Falcon 900 Falcon 900C Falcon 900C
(Honeywell TFE731)Falcon 2000 Falcon 2000
(CFE 738)Falcon 2000EX Falcon 2000EX
(PWC PW308)Falcon 7X Falcon 7X
(PWC PW307A)EADS CASA C-212-CB
C-212-CC
C-212-CD
C-212-CE
C-212-CF
C-212-DD
C-212-DF
C-212-EE
C-212-VA
Aviocar CASA C-212
(Honeywell TPE331)CN-235
CN-235-100
CN-235-200
CN-235-300
CASA CN-235 (GE CT7) EMBRAER
EMBRAER
EMB-120
EMB-120RT
EMB-120ER
Brasilia Embraer 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-135ER
EMB-135LR
EMB-145
EMB-145ER
EMB-145EU
EMB-145EP
EMB-145LR
EMB-145LU
EMB-145MP
EMB-145MK
Embraer EMB-135/145
(RR Corp AE3007A)EMB-500 Phenom 100 Embraer EMB-500
(PWC PW617)EMB-505 Phenom 300 Embraer EMB-505
(PWC PW535)
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)FOKKER
SERVICESFOKKER
SERVICESF27 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 1000
F28 Mark 1000C
F28 Mark 2000
F28 Mark 3000
F28 Mark 3000C
F28 Mark 3000R
F28 Mark 3000RC
F28 Mark 4000
Fellowship
Hawker Siddeley
Fokker 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)FRAKES AVIATION G73 Grumman G73
(PWC PT6)GULFSTREAM AEROSPACE LP (GALP), c/o Israel Aircraft Industries 1125 Westwind Astra
Astra SPX
G100
Gulfstream 100 Gulfstream (IAI) 100/1125/Astra SPX (Honeywell TFE731) Gulfstream G150 Gulfstream G150 Gulfstream (IAI) G150
(Honeywell TFE731)Gulfstream 200/Galaxy Galaxy 200 Gulfstream (IAI) 200/Galaxy
(PWC PW306)GULFSTREAM
AEROSPACE
CorporationGULFSTREAM
AEROSPACE
CorporationGIV (G300) Gulfstream G300 Gulfstream G-IV Series
(RRD Tay)GIV (G400) Gulfstream G400 Gulfstream G-IV Series
(RRD Tay)G-IV/GIV-SP Gulfstream
G-IV/GIV-SPGulfstream 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)HAWKER BEECHCRAFT
HAWKER BEECHCRAFT
DH.125 Series 1
DH.125 Series 3
DH.125 Series 400
HS.125 Series 3
HS.125 Series F3
HS.125 Series F400
HS.125 Series 600
HS.125 Series 700
HS.125 Series F600
Hawker Siddeley BAe 125/Series 700/800 (Honeywell TFE731) BH.125 Series 400
BH.125 Series 600
Beechcraft Hawker BAe 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 Series
Hawker 1000A/B
Hawker 1000
BAe 125 Series 1000
(PWC PW305)300
300LW
Super King Air Beech 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)1900
1900C
1900D
Airliner Beech 1900
(PWC PT6)ISRAEL AIRCRAFT INDUSTRIES IAI 1124
IAI 1124A
Westwind IAI 1124
(Honeywell TFE731)KELOWNA (Convair)
580
Convair 580
(RR Corp 501)LEARJET
31/31A
Learjet 31
(Honeywell TFE731)35/35A
36/36A
Learjet 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 AEROSPACE
M7 AEROSPACE
SA226-T
SA226-TC
SA226-AT
SA226-T(B)
Fairchild SA226 Series
(Honeywell TPE331)SA227-AT
SA227-TT
SA227-CC
SA227-DC
Fairchild SA227 Series
(Honeywell TPE331)SA227-AC
SA227-BC
Swearingen Metro NEXTANT AEROSPACE L.L.C. (STC) 400XT
400XTi
NEXTANT 400XT Beech 400XT Nextant
(Williams FJ44)PILATUS
AIRCRAFT
PC-12
PC-12/45
PC-12/47
PC-12/47E
Pilatus PC-12
(PWC PT6)SAAB AB, SAAB Aerosystems 340A(SF340A)
340B
Saab-Fairchild 340A Saab (SF) 340
(GE CT7)SHORT BROTHERS SD3-30
SD3-60
SD3-SHERPA
SD3-60 SHERPA
Variant 200 Shorts SD3 Series-30/SD3-60
(PWC PT6)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 2
Note 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 training
Note 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 1CIRRUS Design Corporation SF50 single engine jet Vision Jet CIRRUS SF50 (Williams FJ33) EMBRAER EMB-120
EMB-120RT
EMB-120ER
Brasilia Embraer EMB-120
(PWC PW110 Series) Note 1, Note 3EMB-505 Phenom 300 Embraer EMB-505
(PWC PW535) Note 4Hawker Beechcraft B300 Super King Air 350 Beech 300 Series (PWC PT6) Note 4 M7 AEROSPACE SA226-T
SA226-TC
SA226-AT
SA226-T(B)
Fairchild SA226 Series
(Honeywell TPE331) Note 1NA Various Small/non-rated aircraft
(Bristol Siddeley Viper B/S) Note 2NA Various Small/non-rated aircraft (De Havilland Goblin 35) Note 2 NA
NA
Various Allison 250 Small/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 training
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” (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 2
Note 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 training
Note 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 (aeroplanes)
Commercial designation
Type rating endorsement (aircraft type – engine in brackets)
AGUSTA WESTLAND A109E
A109N
A109S
AW109SP
Agusta A109 Series (PWC PW206/207)
Note 7AB139
AW139
Agusta AB139/AW139 (PWC PT6) Note 7 AIRBUS HELICOPTERS
DEUTSCHLAND GmbHBO 105 A
BO 105 C/CBS-4/-5
BO 105 D/DB
BO 105 DB-4
BO 105 DBS Series
BO 105 LS
A-1/A-3BO 105 S
BO 105 series
(RR Corp 250) Note 3
EC 135 P1
EC 135 P2
EC 135 P2 +
EC 135 P3
EC 635 P2+
EC 635 P3
Eurocopter EC 135
(PWC PW206) Note 3EC 135 T1
EC 135 T2
EC 135 T2+
EC 135 T3
EC 635 T1
EC 635 T2+
EC 635 T3
Eurocopter EC 135 (Turbomeca Arrius 2B) Note 3, Note 6 AIRBUS HELICOPTERS DEUTSCHLAND GmbH MBB-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 3 MBB-BK 117 C2 EC145 Eurocopter MBB‑BK 117 C2
(Turbomeca Arriel 1) Note 1, Note 3, Note 6MBB-BK 117 D2 EC145 T2
H145Eurocopter MBB-BK 117 D2 (Turbomeca Arriel 2) Note 1, Note 3 BELL HELICOPTER CANADA 222
222B
222U
Bell 222
(Honeywell LTS 101) Note 1, Note 2230 Executive/Utility/
EMSBell 230
(RR Corp 250) Note 2427 Bell 427
(PWC PW207D) Note 1, Note 2, Note 6
430 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 2MD HELICOPTERS INC MD900 MD Helicopters MD900
(PWC PW206/207) Note 1, Note 2, Note 3SIKORSKY AIRCRAFT S-58 BT to JT Sikorsky S-58
(PWC PT6T) Note 1, Note 3SIKORSKY AIRCRAFT S-70A GE T700(CT7) Sikorsky S-70A
(T700-GE-701)
S-92A Sikorsky S-92A (GE CT7-8) Note 7 NA 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 3
Note 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 TRACTOR 400
500
800
Air Tractor Small/non-rated aircraft
(PWC PT6) Note 1DE HAVILLAND CANADA DHC-4 Caribou Small/non rated aircraft
(PWC PT6) Note 1(DORNIER) RUAG AEROSPACE 228-100 Series
228-200 Series
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 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 5
Note 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)
AGUSTA AS61N
AS61NI
Agusta AS61N/Sikorsky
S-61N
(GE CT58)AGUSTAWESTLAND
AGUSTAWESTLAND
A109E
A109N
A109S
AW109SP
Agusta A109 Series
(PWC PW206/207)A109
A109A
A109AII
A109C
Agusta A109 Series
(RR Corp 250)A109K2 Agusta A109
(Turbomeca Arriel 1)A109E
A109LUH
Agusta A109 Series
(Turbomeca Arrius 2)AB139
AW139
Agusta AB139/
AW139 (PWC PT6)AW169 AW169
(PWC 210)AW189 AW189
(GE CT7)AB 212 Bell 212/
Agusta AB212
(PWC PT6)BELL HELICOPTER TEXTRON, INC 212 214ST Bell 214ST (GE CT7) 412
412EP
412CF
Bell 412/
Agusta AB412
(PWC PT6)AGUSTA AB412
AB412 EP
BELL HELICOPTER CANADA 222SP Bell 222 (RR Corp 250) 222
222B
222UBell 222 (Honeywell LTS 101) 230 Executive/
Utility/EMSBell 230
(RR Corp 250)
427 Bell 427
(PWC PW207D)
429 Bell 429
(PWC PW207D)
430 Bell 430
(RR Corp 250)AIRBUS HELICOPTERS
AIRBUS HELICOPTERS
SA330 J Eurocopter SA 330
(Turbomeca Turmo)AS332 C
AS332 L
AS332 C1
AS332 L1
Eurocopter AS 332
(Turbomeca Makila 1A/1A1)AS355 E
AS355 F
AS355 F1
AS355 F2
Eurocopter AS 355
(RR Corp 250)AS355 N
AS355 NP
Eurocopter AS 355
(Turbomeca Arrius 1)SA 365 N
SA 365 N1
AS 365 N2
Dauphin Eurocopter 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)AIRBUS HELICOPTERS
DEUTSCHLAND
GmbHAIRBUS HELICOPTERS
DEUTSCHLAND
GmbHBO 105 A
BO 105 C/CBS-4/-5
BO 105 D/DB
BO 105 DB‑4
BO 105 DBS Series
BO 105 LS
A-1/A-3BO 105 S
BO 105 series
(RR Corp 250)EC 135 P1 Series
EC 135 P2 Series
EC 635 P2+
Eurocopter EC 135
(PWC PW206)EC 135 T1 Series
EC 135 T2 Series
EC 635 T1
EC 635 T2 Series
Eurocopter EC 135 (Turbomeca Arrius 2B) MBB-BK 117 A Series
MBB-BK 117 B Series
Eurocopter MBB-BK 117 A/B
(Honeywell LTS 101)MBB-BK 117 C1 Eurocopter MBB‑BK 117 C1
(Turbomeca Arriel 1) Note 2MBB-BK 117 C2 EC145 Eurocopter MBB‑BK 117 C2
(Turbomeca Arriel 1) Note 2
MBB-BK 117 D2 EC145 T2
H145Eurocopter MBB‑BK 117 D2 (Turbomeca Arriel 2) Note 2 MD HELICOPTERS INC MD900 MD Helicopters MD900
(PWC PW206/207)SIKORSKY AIRCRAFT
SIKORSKY AIRCRAFT
S-58 BT to JT Sikorsky S-58
(PWC PT6T)S-61N
S-61NM
Agusta AS61N/Sikorsky
S-61N
(GE CT58)S-70A GE T700(CT7) Sikorsky S-70A
(T700-GE-701)
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.
Note to Part 66 Manual of Standards (MOS)
The Part 66 Manual of Standards (MOS) (in force under the Civil Aviation Safety Regulations 1998) as shown in this compilation comprises Part 66 Manual of Standards amended as indicated in the Tables below.
Table of Manual of Standards and Amendments
Year and
numberDate of registration on FRLI
Date of
commencementApplication, saving or
transitional 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 —
Table of Amendments
ad. = added or inserted am. = amended rep. = repealed rs. = repealed and substituted
Provision affected How affected Power to make...................... am. MOS 66 2011 No. 1 s. 1...........................................
(Now numbered 66.1A)rs. MOS 66 2011 No. 2 s. 2
Renumbered s. 66.1B .....
MOS 66 2011 No. 2s. 3 .......................................... rep. MOS 66 2011 No. 2 Schedule heading ............... rep. MOS 66 2011 No. 2 Part 1 heading ..................... ad. MOS 66 2016 No. 5 MOS title................................. rep. MOS 66 2011 No. 2 Part 2 heading ..................... ad. MOS 66 2016 No. 5 s. 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 s. 66.A.1................................. am. MOS 66 2014 No. 1, MOS 66 2016 No. 1 s. 66.A.4................................. MOS 66 2016 No. 5 s. 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 s. 66.A.21............................... ad. MOS 66 2014 No. 1, MOS 66 2016 No. 1, MOS 66 2016 No. 5 s. 66.A.23............................... am. MOS 66 2014 No. 1, MOS 66 2016 No. 1 s. 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 s. 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 s. 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 s. 66.A.50............................... am. MOS 66 2012 No. 2, MOS 66 2013 No. 1 s. 66.A.55............................... am. MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2016 No. 5 s. 66.A.56............................... ad. MOS 66 2015 No. 1 s. 66.A.57............................... ad. MOS 66 2015 No. 1 s. 66.A.58............................... ad. MOS 66 2015 No. 1 am. MOS 66 2017 No. 1 s. 66.A.70............................... am. MOS 66 2016 No. 1 Appendix I.............................. am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2016 No. 1 Appendix II............................. am. MOS 66 2011 No. 2, MOS 66 2012 No. 2 Appendix III............................ am. MOS 66 2011 No. 2, MOS 66 2012 No. 2, MOS 66 2013 No. 1, MOS 66 2016 No. 1 Appendix IV........................... am. MOS 66 2012 No. 1, MOS 66 2013 No. 1, MOS 66 2014 No. 1, MOS 66 2016 No. 1
rs. MOS 66 2016 No. 5
Appendix V............................ rs. MOS 66 2011 No. 2 Appendix VI........................... rs. MOS 66 2011 No. 2 Appendix VII.......................... am. MOS 66 2011 No. 2, MOS 66 2016 No. 1, MOS 66 2016 No. 5 Appendix VIII......................... ad. MOS 66 2013 No. 1
am. MOS 66 2016 No. 1
rs. MOS 66 2016 No. 5
Appendix IX........................... ad. MOS 66 2014 No. 1
am. 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
Table A Application, saving or transitional provisions
Part 66 Manual of Standards Amendment Instrument 2013 (No. 1)
4 Interpretation
A reference in Schedule 1 to Appendix IV, followed by a reference to a unit of competency, is a reference to the row in Appendix IV that refers to that unit in the first column (Competency units required).
Example: Appendix IV (MEA211C).
5 Transitional
(1) If an applicant to whom paragraph 66.A.25 (a) or 66.A.30 (b) of the MOS refers was entitled to the issue of a unit of competency (the unit) immediately before the commencement day, and the unit is replaced on the commencement day by a subsequent version of that unit of competency, the applicant is entitled to the new unit of competency.
(2) In subsection (1):
commencement day means the day on which this instrument comes into effect.
Part 66 Manual of Standards Amendment Instrument 2015 (No. 5)
3 Transitional
If:
(a) immediately before the commencement day, a person was entitled to a unit of competency mentioned in Appendix IV or VIII of the Part 66 Manual of Standards; and
(b) on the commencement day this instrument replaces the unit with a new version of the unit;
then the applicant is entitled to the new unit.
0
0
0