military aircraft maintenance licences

1 Revision: 4.0

Military Aircraft Maintenance Licences

Exclusions, Inclusions and Endorsements

Defence Aviation Safety Authority

"Capability First, Safety Always"

DASR 66 Exclusions, Inclusions and Endorsements

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Document Version History Date Version Comments

26 FEB 2018 1.0 Initial Release

AUG 2018 2.0 Alignment with MEA Aeroskills Training Package Release 2.0

JUN 2019 3.0 Alignment with MEA Aeroskills Training Package Release 3.0

JAN 2020 4.0 Alignment with MEA Aeroskills Training Package Release 4.0

Sponsor

Directorate of Continuing Airworthiness (DCA-DASA) Deputy Director Maintenance Licencing and Training

Effective Date 21 February 2020

Review Date 30 June 2020

Obective id BP7460667


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Table of Contents

Preliminary ............................................................................................................................................... 4 Summary of Changes .............................................................................................................................. 4

Regulatory Requirements ........................................................................................................................ 4

Licences................................................................................................................................................... 4

Application for a MAML ........................................................................................................................... 5

Core Units of Competence ...................................................................................................................... 5

Pathways to a Military Aircraft Maintenance Licence .............................................................................. 5 Military-specific Units of Competency ..................................................................................................... 5

Specialist Services .................................................................................................................................. 6

Excluded systems & exclusions on type categories ............................................................................... 7

Included systems, specialist & military maintenance endorsements ...................................................... 8

All Categories - Core Units of Competency............................................................................................. 9 A Category or Sub-category Licence Exclusions .................................................................................. 10

A Category or Subcategory Licence Inclusions..................................................................................... 11

B Category or Subcategory Licence Exclusions ................................................................................... 12

Specialised and Military Maintenance Extension for a Category or Subcategory of Licence ............... 37

DASR 66 Consolidated list of Exclusions applicable to MAML categories ........................................... 55

Type rated aircraft and type rating endorsements for Category B1, B2 or C licences .......................... 59 List of Superseded UOC Codes in MEA Aeroskills Package Revision 4.0 ........................................... 60

List of Approved Alternate UOC Codes ................................................................................................. 62

S1000D: Standard Numbering System – Air Vehicle, Engines and Equipment ................................... 64


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Preliminary This document was prepared in December 2019 taking into account the latest amendments to the MEA Aeroskills Training Package Release 4.0 and the CASA Part 66 Manual of Standards version released 12/11/2019. A detailed breakdown of each MEA Qualification and Unit of Competency (UOC) may be obtained at https://training.gov.au/Training/Details/MEA. Summary of Changes The following changes have been made in the November 2019 release of this document: A number of MEA UOC Codes are superseded in release 4.0 of the MEA Aeroskills

Training Package released on 30 September 2019. A list of the codes can be found in Appendix C.

Acceptable Alternate MEAs updated throughout the document. A quick reference table is located in Appendix D.

Guidance on E62 exclusion removal updated. Addition of I2 Oxygen System inclusion. Inclusion of S1000D numbering system

Regulatory Requirements ADF aviation maintenance is regulated by the Defence Aviation Safety Authority (DASA). Regulatory requirements associated with aviation maintenance are detailed in the Defence Aviation Safety Regulations (DASR) which are generally aligned with those of the European Military Airworthiness Requirements (EMAR). The latest version of the DASR may be referenced at: www.defence.gov.au/DASP/DASR-Regulations/. Licences DASA is responsible for the control, issue, oversight and enforcement of Military Aircraft Maintenance Licences (MAML) required under the DASR. The licence categories are: Category A with sub-categories A1 and A3 for certification of minor scheduled and unscheduled mechanical and avionics maintenance performed, respectively, on gas turbine fixed wing aircraft and gas turbine engine helicopters. Category B1 with sub-categories B1.1 and B1.3 for certification of scheduled and unscheduled mechanical and minor avionics maintenance performed, respectively, on gas turbine fixed wing aircraft and gas turbine engine helicopters. Category B2 for certification of complex avionic maintenance on aircraft. Category C for certification of maintenance following Base maintenance.

https://training.gov.au/Training/Details/MEA

http://www.defence.gov.au/DASP/DASR-Regulations/

http://www.defence.gov.au/DASP/DASR-Regulations/


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Application for a MAML Individuals seeking the award of a MAML, or applying for a variation to an existing MAML, must apply to DASA using the latest DASR Form 19, available from the DASA website. All applications must be submitted to DASA 66 Licencing via the group mailbox ‘[email protected]’ along with all relevant supporting documentation. ADF members are obligated to ensure that their PMKeyS data is up to date prior to submitting their licence application. Core Units of Competence Personnel involved in the operation and maintenance of Defence aircraft need to meet standardised and robust Qualification Training and Education (QTE) requirements to effectively operate within the regulatory framework. The mandatory core UOC required for the issuance of all DASR 66 MAML are: MEA107, MEA118, MEA154, MEA155, MEA156, MEA157, MEA158, MEA301. Superseded UOC considered approved alternatives are listed in Appendix C. Pathways to a Military Aircraft Maintenance Licence DASR 66 Military Aircraft Licencing establishes the requirements for eligibility, application, issue, and validity of a MAML. Detailed information on the MAML process may be accessed at the following website: https://www.defence.gov.au/DASP/Docs/Manuals/DefenceAviationSafetyRegulation/DASRWeb/index.htm#10508.htm#o10509 Military-specific Units of Competency Military-specific units of competency are achieved through military delivered training courses or in conjunction with a type course against the DASR 66 Syllabus as follows:

SG3 Skill Grade 3 - Service specific supervisory training

SG3ATT Skill Grade 3 - Service specific Advanced Technical Training

W&B Weight and Balance syllabus incorporated in type training

NDT Non Destructive Testing (Dye Penetrant only)

CAMERA Camera system theory and practical training and assessment to satisfy DASR 66 Appendix I Module 53.2 (System 97)

SONAR Sonar system theory and practical training and assessment to satisfy DASR 66 Appendix I Module 53.1 (System 93)

DEFEXO001 Work safely with Explosive Ordnance. Theory and practical training and assessment to satisfy elements of DASR 66 Appendix 1 Module 50

https://www.defence.gov.au/DASP/Docs/DASR-Documents/DASR-Forms/DASR-Form-19-Application%20for%20issue-Amendment-of-DASR-66-Military-Aircraft-Maintenance-Licence.pdf

mailto:[email protected]

https://www.defence.gov.au/DASP/Docs/Manuals/DefenceAviationSafetyRegulation/DASRWeb/index.htm%2310508.htm%23o10509

https://www.defence.gov.au/DASP/Docs/Manuals/DefenceAviationSafetyRegulation/DASRWeb/index.htm%2310508.htm%23o10509


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Specialist Services Specialised services staff having specific trade knowledge and skills and deemed competent and authorised by the relevant DASR 145 Quality Manager (QM). These Specialised services staff carry out specialised maintenance tasks to the standard specified in the Instructions for Continuing Airworthiness (ICA) or defined standards acceptable to the DASA and therefore, do not require a MAML. For further information, refer to the DASR GM 145.A.50 (a) Certification of maintenance (AUS). Note to Readers Please note that whilst every effort has been made to enhance the readability of the information in this document, some details listed against Exclusions/Inclusions in the A Licence, B Licence, and Specialised tables presented may extend across multiple pages.


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Excluded systems & exclusions on type categories E1 Excluding Electrical systems E2.1 Excluding Mechanical systems E2.2 Excluding Mechanical systems advanced troubleshooting E2.3 Excluding Structural components -Pressurised aircraft E2.4 Excluding Structural components -Unpressurised aircraft E2.5 Excluding Minor structural repairs -Pressurised aircraft E2.6 Excluding Minor structural repairs -Unpressurised aircraft E2.7 Excluding Weight and balance assessment E2.8 Excluding liquid penetrant NDT process E3.1 Excluding Powerplant systems E3.2 Excluding Powerplant advanced troubleshooting E6.1 Excluding Instrument/Avionic/Radio subsystems and LRU’s E6.2 Excluding Avionics advanced troubleshooting E12 Excluding Propellers E14 Excluding Vapour cycle air-conditioning E18 Excluding ADF systems E19 Excluding VOR systems E20 Excluding ILS systems E21 Excluding Weather radar systems E22 Excluding ATC transponder, Radio altimeter, DME & Doppler systems E26 Excluding Satellite navigation systems E28.1 Excluding Multi-axis autopilots - Fixed wing E28.2 Excluding Multi-axis autopilots - Rotary wing E29 Excluding Remote indicating compass systems E30 Excluding Inertial navigation and reference systems E31 Excluding Cabin pressurisation instrument and control systems E34 Excluding Digital systems E41 Excluding Oxygen systems E42 Excluding landing gear retraction systems E44 Excluding Wiring repairs E60 Excluding Pitot static systems E61 Excluding Refuelling tanker systems E62 Excluding Supervision of maintenance


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Included systems, specialist & military maintenance endorsements I2 Oxygen Systems S1 Including Electroplating processes S2 Including Brazing processes S3 Including Gas welding processes (OXY) S4 Including Gas tungsten arc welding processes (TIG) S5 Including Gas metal arc welding processes (MIG) S6 Including Manual metal arc welding processes (STICK) S7 Including Plasma welding processes S8 Including Major structural repairs - Pressurised aircraft S9 Including Major structural repairs - Unpressurised aircraft S10 Including Fibre optic maintenance M1 Including Armed aircraft maintenance M2 Including Weapon suspension systems B1 M2.1 Including Weapon suspension systems B2 M3 Including Weapons and gunnery B1 M3.1 Including Weapons and gunnery B2 M4 Including Attack & self-protection management systems B1 M4.1 Including Attack & self-protection management systems B2 M5 Including Surveillance Systems B1 M5.1 Including Surveillance Systems B2 M6 Including Sonar systems B1 M6.1 Including Sonar systems B2 M7 Including Image recording and Optical systems B1 M7.1 Including Image recording and Optical systems B2 M8 Including Electronic warfare systems B1 M8.1 Including Electronic warfare systems B2 M9 Including Ejection seat systems


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All Categories - Core Units of Competency

Competency Unit(s) required

CASA MAML Core Requirements & Flight servicing A1 A3 B1.1 B1.3 B2

Unit of competency from Aeroskills Training Package (Release V 4.0)

This section outlines core competency details and provides general guidance that reflects DASR 66.A.20 Privileges

The S1000D system of standard numbering is used in this table where necessary to specify particular Systems and Sub-systems. Appendix E of this document provides more detail.

Applicability to MAML Category will be marked with an X

Where equivalent units of competency exist this section highlights replacement units or packaged units of competence that meet syllabus requirements.e.g:

MEA317 Remove and install pressurised aircraft structural and non-structural components:

Is higher and Incorporates

MEA304 Remove and install non-pressurised aircraft structural and non-structural components

MEA107 MEA118 MEA154 MEA155 MEA156 MEA157 MEA158 MEA301

MEA107 MEA154 MEA155 MEA156 MEA157 MEA158 MEA3XX#

A category licenses may select the appropriate competency in place of MEA 301 As follows: A1 to complete MEA345 Perform scheduled line maintenance activities on gas turbine engine fixed wing aircraft. A3 to complete MEA346 Perform scheduled line maintenance activities on gas turbine engine rotary wing aircraft B2 to complete MEA301 Perform aircraft flight servicing to be granted an A license #Note 1- CASA requires different flight servicing competencies depending on which category is requested, however all licenses require a competency be achieved.

X X X X X




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A Category or Sub-category Licence Exclusions Competency Unit(s) required CASA A License Exclusions A1 A3

MEA201 MEA203 MEA295

MEA265 MEA295

E1 Excluding Electrical systems Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of electrical systems.

X X

MEA303 MEA305 MEA307 MEA398

MEA344

E2.1 Excluding Mechanical systems Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of Fixed wing mechanical systems.

(MEA307 may be omitted where a propeller is not fitted)

X


MEA344

E2.1 Excluding Mechanical systems Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of Rotary wing mechanical structural & power plant systems.

X

MEA317 MEA344

E2.3 Excluding Structural components Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of structural systems.

X X

MEA304 MEA344

E2.3 Excluding Structural components Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of structural systems.

X


MEA418 E2.5 Excluding repairs of aircraft internal fittings. Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for repairs of aircraft internal fittings.

X X

MEA306 MEA344 E3.1 Excluding Powerplant systems Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of structural systems.

X X

MEA343 MEA264

E6.1 Excluding Avionic systems Upon completion of these competencies, a Pt 145 with task training privileges may provide task training for minor scheduled line maintenance and simple defect rectification of avionic systems.

X X


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A Category or Subcategory Licence Inclusions

Competency Unit(s) required CASA A License Inclusions A1 A3

DEFEX001 Not Covered

M1 Including Armed aircraft maintenance Can perform maintenance on an aircraft that has explosive ordnance installed (‘Ordnance’ does not include cartridges used to activate a fire suppression system or used in a cargo hook or rescue hoist system)Cannot Remove or Install explosive ordnance on an aircraft.

X X

MEA304 or MEA317

Not Covered

M2 Including Weapon suspension systems Weapons systems (94-00, -30)

X X


Not Covered

M2.1 Including Weapon suspension systems Weapons systems (94-00, -10, -30)

X X

MEA294 Inspect, test and troubleshoot advanced aircraft electrical systems and components:



Is equivalent to

MEA317 Remove and install pressurised aircraft structural and non-structural components

Is higher and incorporates

MEA223 Inspect aircraft electrical systems and components plus

MEA227 Test and troubleshoot aircraft electrical systems and components

MEA603 Remove and install aircraft stores suspension system components plus

MEA605 Inspect, test and troubleshoot aircraft stores suspension systems and components


MEA601 Not Covered

M9 Including Ejection Seats Crew escape and safety (95-10,20,30,70)

X X


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B Category or Subcategory Licence Exclusions DASA Competency Unit(s) required

CASA Competency Unit(s) required

B Licence Exclusions B1.1 B1.3 B2

Unit of competency from Aeroskills Training Package (Revision 4.0)

Exclusion or Extension Code

This section should be read in conjunction with S1000D Air vehicle, Engines and Equipment numbering system located in Appendix E.

Aircraft systems that are excluded from license privileges are presented with the name of the system/sub system, and the assigned code/sub code listed in brackets, e.g.:

• Lighting (33-00 thru -90) indicates that all sub systems are included.

• Crew escape and safety (95-10,20,30,70) includes a set of specific subsystems.

Applicability to MAML Category

Where equivalent units of competency exist this section highlights replacement units or packaged units of competence that meet syllabus requirements.e.g:

MEA317 Remove and install pressurised aircraft structural and non-structural components:



MEA201 MEA203 MEA246 MEA294 MEA296

MEA201 MEA203 MEA223 MEA227 MEA246 MEA296

E1 Excluding Electrical systems Interface with Mechanical systems/LRU’s

Interface with Structural systems/LRU’s

Interface with Powerplant systems/LRU’s

Electrical Power (24-00 thru -90)

Lighting (33-10 thru -50)

Fire Protection (26-10 thru -30)

Air vehicle wiring (91)

X



13

DASA Competency Unit(s) required












X










X



MEA223 Inspect aircraft electrical systems and components, plus



14




MEA303 MEA305 MEA318 MEA320 MEA321 MEA328 MEA398

MEA303 MEA305 MEA317 MEA318 MEA320 MEA321 MEA323 MEA325 MEA328 MEA339 MEA365 MEA398

E2.1 Excluding Mechanical systems Environmental control (21-10 thru -90)

Equipment/furnishings (25-10 thru -80)


Flight controls (27-10 thru -90)

Fuel (28-10 thru -60)

Hydraulic power (29-10 thru -30)

Ice and rain protection (30-10, -20, -40 thru -80)

Landing gear (32-10 thru -90)

Pneumatic (36-10, -20)

Vacuum (37-10, -20)

Water/Waste (38-10 thru -40)

Nitrogen (47-10 thru -40)

Cargo and accessory compartment (50-10 thru -60)

X

MEA312 Inspect, test and troubleshoot aircraft fixed wing flight control systems and components


MEA323 Perform advanced troubleshooting in aircraft mechanical maintenance

Is equivalent to

MEA321 Test and troubleshoot aircraft fixed wing flight control systems and components

SG3ATT Advanced Technician course


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MEA303 MEA304 MEA308 MEA309 MEA310# MEA316 MEA328 MEA398

MEA303 MEA304 MEA308 MEA309 MEA310 MEA316 MEA323 MEA325 MEA328 MEA339 MEA365 MEA398

E2.1 Excluding Mechanical systems Environmental control (21-10 thru -90)




Fuel (28-10 thru -60)

Hydraulic power (29-10 thru -30)

Ice and rain protection (30-10, -20, -40 thru -80)

Landing gear (32-10 thru -90)

Pneumatic (36-10, -20)

Vacuum (37-10, -20)

Water/Waste (38-10 thru -40)

Cargo and accessory compartments (50-10 thru -60)

Main Rotor (62-10 thru -40)

Main Rotor drives (63-10 thru -40)

Tail rotor (64-10 thru -40)

Tail rotor drive (65-10 thru -40)

Folding blades/pylon (66-10 thru -30)

Rotors flight control (67-10 thru -30)

X

#Note: MEA310 Inspect, Test and Troubleshoot Aircraft Pneumatic Systems and Components can be achieved by submission of a completed log of industrial experience for Defence trained personnel as underpinning knowledge was provided as part of MEA303 Remove and Install Aircraft Pneumatic System Components at RAAFSTT. This activity must be undertaken in accordance with service specific training policy and submitted to DASA accompanied by a Form 19.


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MEA309 - Inspect, test and troubleshoot aircraft hydro-mechanical and landing gear systems and components

Is equivalent to

MEA310 Inspect, test and troubleshoot aircraft pneumatic systems and components

Is incorporated in


Is equivalent to

MEA318 - Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components Plus

MEA320 Test and troubleshoot aircraft hydro-mechanical, gaseous and landing gear systems and components,

MEA318 Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components plus

MEA320 Tett and troubleshoot aircraft hydro-mechanical, gaseous and landing gear systems and components


SG3ATT MEA323 E2.2 Excluding Mechanical systems advanced troubleshooting Troubleshooting outside of the scope of that which can be achieved using all available Instructions for Continuing Airworthiness

X X


Is equivalent to



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MEA317 MEA339

E2.3 Excluding Structural Components - Pressurised aircraft* All Structural Components - Unpressurised aircraft detailed in E2.4 &;

Standard Practices - Structures (51-00, -10)

Doors (52-10 thru -80)

Fuselage (53-10 thru -90)

Nacelles/pylons (54-10 thru -90)

Stabilisers (55-10 thru -50)

Windows and canopies (56-10 thru -40)

Wings (57-10 thru -80)

Crew escape and safety (95-50, -60)

X

Note* Applicants who meet the requirements for exclusion removal of E2.3 will also be granted exclusion removal of E2.4 as MEA317 is considered to be higher and inclusive of the elements required in MEA304

MEA339 Inspect, repair and maintain aircraft structures


MEA401Maintain aircraft structure/components plus

MEA410 Inspect aircraft structures


MEA304 MEA339

E2.4 Excluding Structural components - Unpressurised aircraft Standard Practices - Structures (51-00, -10)







Crew escape and safety (95-50, -60)

X X



18






MEA401Maintain aircraft structure/components &


MEA317 MEA339

MEA317 MEA339

E2.5 Excluding Minor Structural Repairs - Pressurised aircraft* • Remove corrosion by chemical and mechanical methods. • Restore protective coatings. • Apply sealants and jointing compounds. • Freehand precision hole generation. • Remove and install structural hardware and fastening devices. • Remove and replace bushes, bearings and bearing surfaces. • Metal scab patch, flush, splice, lap and formed section repair. • Composite external patch, scarf, stepped and bolted repairs.

Standard Practices - Structures (51-00 thru -80)







X



19




MEA401Maintain aircraft structure/components

MEA405 Repair/modify aircraft composite material structure/components


MEA420 Fabricate basic structural components for aircraft

MEA422 Repair/modify aircraft metal structure

In combination are higher and incorporate


MEA311 Inspect and repair/modify aircraft structures

Is equivalent to

MEA402 Fabricate aircraft structural components

Is equivalent to

MEA403 Repair/modify aircraft structure

Is equivalent to



MEA422 - Repair/modify aircraft metal structure


20




MEA304 MEA339

MEA304 MEA339

E2.6 Excluding Minor Structural Repairs - Unpressurised aircraft • Remove corrosion by chemical and mechanical methods. • Restore protective coatings. • Apply sealants and jointing compounds. • Freehand precision hole generation. • Remove and install structural hardware and fastening devices. • Remove and replace bushes, bearings and bearing surfaces. • Metal scab patch, flush, splice, lap and formed section repair. • Composite external patch, scarf, stepped and bolted repairs.

Standard Practices - Structures (51-00 thru -80)







X X


MEA401Maintain aircraft structure/components

MEA405 Repair/modify aircraft composite material structure/components




In combination are higher and incorporate



21




MEA311 Inspect and repair/modify aircraft structures

Is equivalent to

MEA403 Repair/modify aircraft structure

Is equivalent to


Is equivalent to




SG3 W&B

MEA325 E2.7 Excluding Weight and balance assessment

DASR 66 Syllabus 7.16 Aircraft Weight and Balance

X X

SG3 W&B

MEA241 E2.7 Excluding Weight and balance assessment

DASR 66 Syllabus 7.16 Aircraft Weight and Balance

X

SG3 NDT *

MEA365 E2.8 Excluding liquid penetrant NDT process

X X

* Appendix 1 to DASR 66 Module 7.18 (c) Non-destructive Inspection stipulates that the applicant must have achieved a minimum of Level 2 knowledge base requirement. Note this exclusion only applies to the performance of Non-destructive Inspection Dye Penetrant processes.


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MEA306 MEA314

MEA306 MEA307# MEA315# MEA319 MEA322 MEA323

E3.1 Excluding Powerplant systems Electrical power (24-10, -20, -30)

Ice and rain protection systems (30-20)

Airborne auxiliary power APU (49-10 thru -90)

Standard practices Engine (70-00, -70, -80)

Power plant (71-00 thru -80)

Engine turbine/turboprop Ducted fan/inducted fan (72-00 thru -90)

Engine fuel and control (73-10 thru -30)

Ignition (74-10 thru -30)

Air (75-10 thru -50)

Engine controls (76-10, -20)

Engine indicating (77-10 thru -40)

Exhaust (78-10 thru -60)

Oil (79-10 thru -30)

Starting (80-10)

Water Injection (82-10 thru -40)

Accessory Gearboxes (83-10, -20)

X X

# Note 1

MEA307 Remove and Install Propeller Systems and Components & MEA315 Inspect, Test and Troubleshoot Propeller Systems and Components are covered by E12 exclusions

MEA314 Inspect, test and troubleshoot gas turbine engine systems and components

Is equivalent to

MEA319 Inspect gas turbine engine systems and components plus

MEA322 Test and troubleshoot gas turbine engine systems and components


23




SG3ATT

MEA323 E3.2 Excluding Powerplant systems advanced troubleshooting Troubleshooting outside of the scope of that which can be achieved using all available Instructions for Continuing Airworthiness

X X


Is equivalent to




E6.1

Excluding Instrument/Avionic/Radio subsystems and LRU’s Autopilot (22-10 thru -50)

Communications (23-10 thru -80)



Indicating and recording systems (31-10 thru -70)

Navigation (34-10 thru -70)

Integrated modular avionics (42-20, -30)

Cabin systems (44-10 thru -60)

Tactical Communications (43-10 thru -90)

Cabin Systems(44-10 thru -60)

Central maintenance system (45-04 thru -99)

Systems integration and display (46-10 thru -79)

Information systems (46-10 thru -50)

In Flight Refuelling Tanker (48-10 thru -60)

Airborne Auxiliary Power (49-10 thru -90)

Cargo and Accessory Compartment (50-10 thru -50)

Propellers (61-10 thru -50)

X X


24




Main Rotors (62-10 thru -40)

Main Rotor Drives(63-10 thru -40)

Tail Rotor(64-10 thru -40)

Tail Rotor Drives (65-10 thru -40)

Folding Blades/Pylon (66-10 thru -30)

Rotors Flight Control (67-10 thru -30)

Engine Fuel and Control (73-20)

Air indicating (75-40)

Engine indicating system (77-40)

Oil indicating (79-30)

Radar (92-10 thru -80)

Note – Limited to maintenance that requires ‘simple’ tests to prove their serviceability as defined in DASR 66.A.20 Privileges (a), 2.


25





MEA206 MEA224 MEA225# MEA226 MEA228 MEA229 MEA230# MEA231# MEA232* MEA235 MEA292 MEA293

E6.1

Excluding Instrument/Avionic/Radio subsystems and LRU’s

Communications (23-10 thru -80)


Ice and rain protection systems (30-80)


Navigation (34-10 thru -70)

Integrated modular avionics (42-20, 30)

Tactical Communications (43-10 thru -90)

Cabin Systems(44-10 thru -60)


Systems integration and display (46-10 thru -79)


In Flight Refuelling Tanker (48-10 thru -60)

Airborne Auxiliary Power (49-10 thru -90)

Cargo and Accessory Compartment (50-10 thru -50)

Propellers (61-10 thru -50)

Main Rotors (62-10 thru -40)

Main Rotor Drives (63-10 thru -40)

Tail Rotor (64-10 thru -40)

Tail Rotor Drives (65-10 thru -40)

Folding Blades/Pylon (66-10 thru -30)

Rotors Flight Control (67-10 thru -30)

Engine Fuel and Control (73-20)

Air indicating (75-40)

Engine indicating system (77-40)

X


26




Oil indicating (79-30)


#Note 1

MEA225 Inspect fixed wing aircraft automatic flight control systems and components, MEA230 Test and troubleshoot fixed wing aircraft automatic flight control systems and components, MEA231 Inspect, test and troubleshoot rotary wing aircraft automatic flight control systems and components are covered by E28 Exclusions

*Note 2

MEA216 Inspect, test and troubleshoot instrument landing systems and components required for exclusion(E20)

MEA220 Inspect, test and troubleshoot aircraft primary radar systems and components required for exclusion (E21)

MEA221 Inspect, test and troubleshoot aircraft secondary radar systems and components required for exclusion (E22)

Are used for Defence Aircraft systems therefore negating the requirement for MEA232 Test and troubleshoot aircraft pulse systems and components

MEA213 Inspect, test and troubleshoot advanced aircraft instrument systems and components


MEA224 Inspect aircraft instrument systems and components plus

MEA228 Test and troubleshoot aircraft instrument systems and components

MEA214 Inspect, test and troubleshoot aircraft basic communication and radio navigation systems and components


MEA215 Inspect, test and troubleshoot advanced aircraft communications systems and components




MEA226 Inspect aircraft electronic systems and components plus

MEA229 Test and troubleshoot aircraft radio frequency navigation and communications systems and components


MEA229 Test and troubleshoot aircraft radio frequency navigation and communications systems and components




27




SG3ATT MEA235 E6.2 Excluding Avionics advanced troubleshooting Troubleshooting outside of the scope of that which can be achieved using all available Instructions for Continuing Airworthiness

X

MEA307 MEA315

MEA307 MEA315

E12 Excluding Propellers Propeller/rotor (60-10 thru -90)

Propeller/propulsion (61-10 thru -50)

X

MEA362 MEA201# MEA246# MEA296 MEA362

E14 Excluding vapour cycle air-conditioning Environmental control (21-10 thru -90)

X X

#Note 1

MEA201, MEA246 are electrical aspects covered in E1 Exclusion.

MEA362 Maintain aircraft vapour cycle air conditioning systems

Is equivalent to

AURETU004 - Diagnose and repair air conditioning and HVAC systems or

AURETU3004 - Diagnose and repair air conditioning and HVAC systems


28




MEA206 MEA214

MEA206 MEA214

E18

Excluding ADF systems Navigation system ADF functions (34-50, -60)

X


MEA229 Test and troubleshoot aircraft radio frequency navigation and communications systems and components,

Is equivalent to


MEA206 MEA214


E19

Excluding VOR systems Navigation system VOR functions (34-50, -60)

X



Is equivalent to



29






E20 Excluding ILS systems Navigation system ILS functions (34-30, -60)

X



Is equivalent to

MEA216 Inspect, test and troubleshoot instrument landing systems and components

MEA220 MEA293

MEA220 MEA293

E21 Excluding radar systems Navigation system radar functions (34-40, -60)


X

MEA226 - Inspect aircraft electronic systems and components plus

MEA232 Test and troubleshoot aircraft pulse systems and components

Is equivalent to

MEA220 Inspect, test and troubleshoot aircraft primary radar systems and components


30




MEA221 MEA293

MEA221 MEA293

E22 Excluding ATC, Radio altimeter, transponder, DME & Doppler systems Navigation systems ATC, Radio altimeter, transponder DME and Doppler functions (34-50, -60)

Note - Incorporates CASA E23, E24 & E25 exclusions due to same competence requirements

X


MEA232 Test and troubleshoot aircraft pulse systems and components,

Is equivalent to

MEA221 Inspect, test and troubleshoot aircraft secondary radar systems and components



E26 Excluding Satellite navigation systems Navigation systems Satellite navigation functions (34-50, -60)

X

MEA217 MEA293

MEA217 MEA293

E28.1 Excluding Multi-axis autopilots Fixed Wing Autopilot (22-10 thru -50)

X

MEA217 Inspect, test and troubleshoot fixed wing autopilot systems and components

Is equivalent to

MEA225 Inspect fixed wing aircraft automatic flight control systems and components plus

MEA230 Test and troubleshoot fixed wing aircraft automatic flight control systems and components

MEA231 MEA293

MEA218 MEA293

E28.2 Excluding Multi-axis autopilots Rotary Wing Autopilot (22-10 thru -50)

X


31




MEA213 MEA292

MEA213 MEA292

E29 Excluding remote indicating compass systems Autopilot (22-10)

X


MEA228 Test and troubleshoot aircraft instrument systems and components.

Is equivalent to

MEA213 - Inspect, test and troubleshoot advanced aircraft instrument systems

MEA233 MEA293

MEA233 MEA293

E30 Excluding Inertial navigation and reference systems Navigation systems Inertial navigation and reference system functions (34-40, -60)

X

MEA208 MEA219

MEA208 MEA219

E31 Excluding Cabin pressurisation instrument and control systems Environmental control (21-30)

X



Is equivalent to

MEA219 Inspect, test and troubleshoot aircraft pressurisation control systems and components


32




MEA278 MEA279# MEA293

MEA293; and any one of the following: MEA227 MEA228 MEA229 MEA230 MEA231 MEA232 MEA278

E34 Excluding Digital systems Communications (23-10 thru -80)

Flight controls fly-by-wire functions (27-10 thru -90)

Equipment/furnishings (25-60)


Integrated modular avionics (42-20, -30)

Cabin systems (44-10 thru -60)


Systems integration and display (46-10, -20, -30)


Engine fuel and control (73-20, -30)

Engine indicating system (77-10 thru 40)

Note: MEA279 is required by DASA as it specifically addresses the syllabus requirements of DASR 66 Appendix I Module 14.1 Full Authority Digital Engine (or Electronics) Control (FADEC).

X

MEA209 MEA222

MEA209 MEA222

E41 Excluding Oxygen systems Oxygen (35-10 thru -40)

X X


33





MEA201# MEA201# MEA202# MEA210# MEA246# MEA296 MEA309 MEA398

E42 Excluding landing gear retraction systems Landing gear (32-10 thru -90)

X X

# Note 1

MEA201,MEA202, MEA210, MEA246 & MEA260 are electrical aspects covered in E1 Exclusion.


Is equivalent to

MEA318 - Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components Plus

MEA320 Test and troubleshoot aircraft hydro-mechanical, gaseous and landing gear systems and components,



E44 Excluding Wiring Repairs Continuity, insulation and bonding techniques and testing;

Crimping and testing of crimped joints;

Connector pin removal and insertion;

Wiring protection techniques

X X


34




MEA343 or MEA213 MEA292 MEA303 MEA310

Not Covered E60 Excluding Pitot static systems Ice and Rain protection (30-30)

Navigation (34-10)

X X

#Note 1

MEA310 Inspect, Test and Troubleshoot Aircraft Pneumatic Systems and Components can be achieved by submission of a completed log of industrial experience for Defence trained personnel as underpinning knowledge was provided as part of MEA303 Remove and Install Aircraft Pneumatic System Components at RAAFSTT. This activity must be undertaken in accordance with service specific training policy and submitted to DASA accompanied by a Form 19.

MEA310 Inspect, test and troubleshoot aircraft pneumatic systems and components

Is incorporated in


MEA320 Test and troubleshoot aircraft hydro-mechanical, gaseous and landing gear systems and components


35





Not Covered E61 Excluding Refuelling tanker systems In-flight refuelling tanker (System 48-10 thru -60)

X


Is incorporated in

MEA318 Inspect aircraft hydro-mechanical, mechanical, gaseous and landing gear systems and components,


MEA312 Inspect, test and troubleshoot aircraft fixed wing flight control systems and components




Is equivalent to

MEA 321 Test and troubleshoot aircraft fixed wing flight control systems and components

Is equivalent to

MEA321 Test and troubleshoot aircraft fixed wing flight control systems and components

MEA309 Inspect, test and troubleshoot aircraft hydro-mechanical and landing gear systems and components

MEA312 Inspect, test and troubleshoot aircraft fixed wing flight control systems and components Note: MEA321 is only a satisfactory alternative to MEA312 if accompanied with any of MEA309, MEA315, MEA316, or MEA318.


36




SG3

MEA111 MEA112 MEA113 MEA116 MEA142 MSMENV472

E62 Excluding Supervision of maintenance The MAML holder can only perform maintenance certifications where they have personally performed the maintenance, and cannot be utilised to supervise A or B MAML holders.

DASA 66 Syllabus 7.20 Maintenance Procedures (Appendix I)

Note: MSMENV472 is a mandatory packaging requirement however does not fit any DASR 66 Syllabus requirements

Note: DASR syllabus MOD 10 is a mandatory requirement in addition to the above requirements until 147 organisations incorporate syllabus requirements into training programs.

X X X


37

Specialised and Military Maintenance Extension for a Category or Subcategory of Licence DASA Competency Unit(s) required


Title of Extension for specialised and military maintenance Exclusion removal military specific systems can be achieved through completion of all required MEA competencies & a type course that incorporates S1000D Air-vehicle system basic knowledge requirements into the type syllabus.

B1.1

B1.3

B2

MEA209 MEA222

MEA209 MEA222

I2 Including Oxygen Systems DASA 66 Syllabus 11.15 Oxygen (System 35-10 thru -40)

X

MEM08003 Specialised Service

S1 Including Electroplating Processes DASA 66 Syllabus 7.18 Disassembly, Inspection, Repair and Assembly Techniques ( Reprotection)

11.2 Airframe Structures — General Concepts

12.5 Airframe Structures

X X

MEA431 or MEM05006

Specialised Service

S2 Including Brazing Processes *Ongoing certification against relevant standards and materials required*

DASA 66 Syllabus 7.15 Welding, Brazing, Soldering and Bonding

X X

MEA430 or MEM05004

Specialised Service

S3 Including Gas welding processes (OXY) *Ongoing certification against relevant standards and materials required*


X X

MEA432 or MEM05049

Specialised Service

S4 Including Gas tungsten arc welding processes (TIG) *Ongoing certification against relevant standards and materials required*


X X


38




B1.1

B1.3

B2

MEA433 or MEM05050

Specialised Service

S5 Including Gas metal arc welding processes (MIG) *Ongoing certification against relevant standards and materials required*


X X

MEA435 or MEM05012

Specialised Service

S6 Including Manual metal arc welding processes (STICK) *Ongoing certification against relevant standards and materials required*


X X

MEA434 Specialised Service

S7 Including Plasma welding processes *Ongoing certification against relevant standards and materials required*


X X


Specialised Service

S8 Including Major structural repairs - Pressurised aircraft Includes all structural repairs listed in E2.5 and E2.6 and;

• Composite Repairs and modifications beyond minor external patch, scarf, stepped and bolted repairs.

• Bending, cutting, rolling, shrinking and stretching. • Assembly of aircraft sub-assemblies or end items from detailed parts using jigs and fixtures

Disassembly and reassembly of aircraft structure, such as wings, tailplanes or fuselage sections, using trestling, jigs and fixtures

• Replacement of major structural load carrying members, for example, skins, longerons, spars, frames and bulkheads

All other repairs or modifications to aircraft structures that are not covered in aircraft maintenance program documentation and are provided using methods prescribed by a recognised standard.

X X


39




B1.1

B1.3

B2

Structures — General (51-00 thru -80)



Nacelles and pylons (54-10 thru -90)


Windows (A56-10 thru -40)


MEA420: Fabricate basic structural components for aircraft plus

MEA421: Fabricate advanced structural components for aircraft

Is equivalent to

MEA403 – Repair/modify aircraft structure.

Is equivalent to

MEA404 - Disassemble and reassemble aircraft structure for major repair or modification.

Is a satisfactory alternative to


MEA422 Repair/modify aircraft metal structure.

MEA423 - Aircraft structure major disassembly and reassembly


40




B1.1

B1.3

B2


Specialised Service

S9 Including Major structural repairs -Unpressurised aircraft Including all Minor structural repairs - Unpressurised aircraft detailed in E2.6 &

• Composite Repairs and modifications beyond minor external patch, scarf, stepped and bolted repairs.

• Bending, cutting, rolling, shrinking and stretching. • Assembly of aircraft sub-assemblies or end items from detailed parts using jigs and fixtures

Disassembly and reassembly of aircraft structure, such as wings, tailplanes or fuselage sections, using trestling, jigs and fixtures

• Replacement of major structural load carrying members, for example, skins, longerons, spars, frames and bulkheads

All other repairs or modifications to aircraft structures that are not covered in aircraft maintenance program documentation and are provided using methods prescribed by a recognised standard.

Structures — General (51-00 thru -80)



Nacelles and pylons (54-10 thru -90)


Windows (A56-10 thru -40)


X X

MEA420: Fabricate basic structural components for aircraft plus

MEA421: Fabricate advanced structural components for aircraft

Is equivalent to

MEA403 – Repair/modify aircraft structure.

Is equivalent to


MEA422 Repair/modify aircraft metal structure.


41




B1.1

B1.3

B2

MEA404 - Disassemble and reassemble aircraft structure for major repair or modification.

Is equivalent to

MEA423 - Aircraft structure major disassembly and reassembly

MEA266 Specialised Service

S10 Including Termination or repair of optical fibre cable DASA 66 Syllabus Module 5.10

X

DEFEXO001 Not Covered M1 Including Armed aircraft maintenance Can perform maintenance on an aircraft that has explosive ordnance installed (‘Ordnance’ does not include cartridges used to activate a fire suppression system or used in a cargo hook or rescue hoist system)

Removal and Installation of explosive ordnance and associated pre-flight inspections are to meet DASR M.A.301 (a) 1

X X X

MEA304

Not Covered M2 Including Weapon suspension systems B1 Weapons systems (94-00, -10, -30)

Note – Only maintenance requiring simple tests to prove serviceability and not requiring troubleshooting IAW DASR 66.A.20 Privileges (a), 2

X X

MEA 317 Remove and install pressurised aircraft structural and non-structural components



MEA 304 Remove and install non-pressurised aircraft structural and non-structural components,

Is equivalent to

MEA603 Remove and install aircraft stores suspension system components &



42




B1.1

B1.3

B2


Not Covered M2.1 Including Weapon suspension systems B2 Weapons systems (94-00, -10, -30, -70)

X



Is equivalent to



Is equivalent to

MEA294 Inspect, test and troubleshoot advanced aircraft electrical systems and components

MEA213 Inspect, test and troubleshoot advanced aircraft instrument systems

MEA603 MEA605

Not Covered M3 Including Weapons and gunnery B1 Weapons systems (94-00, -10, -50)

Note – Only maintenance requiring simple tests to prove serviceability and not requiring troubleshooting IAW DASR 66.A.20 Privileges (a), 2.

X X

MEA603 Remove and install aircraft stores suspension system components &


Is equivalent to

MEA304 Remove and install non-pressurised aircraft structural and non-structural components & a type course that incorporates S1000D Air-vehicle system 94 basic knowledge requirements into the type syllabus.


43




B1.1

B1.3

B2


Not Covered M3.1 Including Weapons and gunnery B2 Weapons systems (94-00, -10, -50, -70)

X



Is equivalent to



Is equivalent to



MEA602 MEA604

Not Covered M4 Including Attack & self-protection management systems B1 Attack System Management (39-00, -70)

Operational Attack Functions (40-00, -30, -60, -70)


X X


44




B1.1

B1.3

B2


Not Covered M4.1 Including Attack & self-protection management systems B2 Attack System Management (39-10 thru -90)

Operational Attack Functions (40-10 thru -70)

Cross Technical Attack Functions (42-10 thru -70)

X



Is equivalent to



Not Covered M5 Including Surveillance Systems B1 Surveillance (93-10 thru -80)


X X


45




B1.1

B1.3

B2

MEA213

MEA214

MEA215

MEA216

MEA220

MEA221

MEA233

MEA234

MEA278

MEA280

MEA294

Not Covered M5.1 Including Surveillance Systems B2 Surveillance (93-10 thru -80)

X



Is equivalent to



Is equivalent to

MEA226 - Inspect aircraft electronic systems and components plus MEA229 Test and troubleshoot aircraft radio frequency navigation and communications systems and components.

Is equivalent to





46




B1.1

B1.3

B2


MEA229 Test and troubleshoot aircraft radio frequency navigation and communications systems and components.

Is equivalent to



Is equivalent to



Is equivalent to


MEA232 Test and troubleshoot aircraft pulse systems and components.

Is equivalent to






Not Covered M6 Including Sonar Systems B1 Surveillance (93-90)


X X


47




B1.1

B1.3

B2

MEA213 MEA214 MEA215 MEA216 MEA220 MEA221 MEA233 MEA234 MEA278 MEA280 MEA294 SONAR

Not Covered M6.1 Including Sonar Systems B2

Surveillance (93-90)

X



Is equivalent to



Is equivalent to




48




B1.1

B1.3

B2



Is equivalent to



Is equivalent to



Is equivalent to



Is equivalent to



Is equivalent to







49




B1.1

B1.3

B2


Not Covered M7 Including Image recording and optical systems B1 Image recording (97-10 thru -70)


X X

MEA213

MEA215

MEA220

MEA221

MEA233

MEA234

MEA278

MEA294 CAMERA*

Not Covered M7.1 Including Image recording and optical systems B2 Image recording (97-10 thru -70)

X

*Note – Theory and practical training on specific aircraft type camera systems must address the knowledge level requirements of DASR Appendix I Module 53.2 (System 97)


50




B1.1

B1.3

B2



Is equivalent to



Is equivalent to


MEA232 Test and troubleshoot aircraft pulse systems and components,

Is equivalent to

MEA224 - Inspect aircraft instrument systems and components plus MEA228 - Test and troubleshoot aircraft instrument systems and components Test and troubleshoot aircraft instrument systems and components.

Is equivalent to



Is equivalent to


MEA220 Inspect, test and troubleshoot aircraft primary radar systems and components.



MEA215 Inspect, test and troubleshoot advanced aircraft communications systems and components.


51




B1.1

B1.3

B2


Not Covered M8 Including Electronic warfare systems B1 Electronic Warfare (99-10 thru -80)


X X

MEA213 MEA214 MEA215 MEA216 MEA220 MEA221 MEA233 MEA234 MEA278 MEA280 MEA294

Not Covered M8.1 Including Electronic warfare systems B2 Electronic Warfare (99-10 thru -80)

X



Is equivalent to



52




B1.1

B1.3

B2



Is equivalent to



Is equivalent to



Is equivalent to



Is equivalent to



Is equivalent to

MEA232 Test and Troubleshoot aircraft secondary radar systems and components plus



MEA226 Inspect aircraft electronic systems and components.

Is equivalent to

MEA215 Inspect, test and troubleshoot advanced aircraft communications systems and components.





MEA221 Inspect, Test and Troubleshoot aircraft secondary radar systems and components


53




B1.1

B1.3

B2

MEA601 Not Covered M9 Including Ejection Seats Crew escape and safety (95-10 thru -70)

X X X


54

Appendix A

55

DASR 66 Consolidated list of Exclusions applicable to MAML categories

Consolidated list of Exclusions applicable to MAML categories

A1

E1 Excluding Electrical Systems

E2.1 Excluding Mechanical systems

E2.3 Excluding Structural components -Pressurised aircraft

E2.5 Excluding Minor Structural repairs -Pressurised aircraft

E3.1 Excluding Powerplant systems

E6.1 Excluding Instrument/Avionic/Radio subsystems and LRU's

M1 Including Armed aircraft maintenance

M2 Including Weapon suspension systems

M2.1 Including Weapon suspension systems

M9 Including Ejection Seats

A3

E1 Excluding Electrical Systems


E2.4 Excluding Structural components -Unpressurised aircraft

E2.6 Excluding Minor Structural repairs -Unpressurised aircraft


E6.1 Excluding Instrument/Avionic/Radio subsystems and LRU's





B1.1

E1 Excluding Electrical systems


E2.2 Excluding Mechanical systems advanced troubleshooting

E2.3 Excluding Structural Components -Pressurised aircraft

E2.5 Excluding Minor structural repairs -Pressurised aircraft

E2.7 Excluding Weight and balance assessment

E2.8 Excluding NDT assessment of structural repairs


56

E3.2 Excluding Powerplant systems advanced troubleshooting

E6.1 Excluding Instrument/Avionic/Radio subsystems and LRU’s

E12 Excluding Propellers

E14 Excluding vapour cycle air-conditioning

E41 Excluding Gaseous systems

E42 Excluding landing gear retraction systems

E44 Excluding Wiring Repairs

E60 Excluding Pitot static systems

E61 Excluding Refuelling tanker systems

E62 Excluding Supervision of maintenance

S1 Including Electroplating Processes

S2 Including Brazing Processes

S3 Including Gas welding processes (OXY)

S4 Including Gas tungsten arc welding processes (TIG)

S5 Including Gas metal arc welding processes (MIG)

S6 Including Manual metal arc welding processes (STICK)

S7 Including Plasma welding processes

S8 Including Major structural repairs -Pressurised aircraft

S9 Including Major structural repairs -Unpressurised aircraft



M3 Including Weapons and gunnery B1

M4 Including Attack & self-protection management systems B1

M5 Including Surveillance Systems B1

M6 Including Sonar Systems B1

M7 Including Image recording and optical systems B1

M8 Including Electronic warfare systems B1


B1.3



E2.2 Excluding Mechanical systems advanced troubleshooting

E2.4 Excluding Structural components -Unpressurised aircraft

E2.6 Excluding Minor structural repairs -Unpressurised aircraft


57

E2.8 Excluding NDT assessment of structural repairs


E3.2 Excluding Powerplant systems advanced troubleshooting


E14 Excluding vapour cycle air-conditioning

E41 Excluding Gaseous systems

E42 Excluding landing gear retraction systems

E44 Excluding Wiring Repairs

E60 Excluding Pitot static systems


S1 Including Electroplating Processes

S2 Including Brazing Processes

S3 Including Gas welding processes (OXY)

S4 Including Gas tungsten arc welding processes (TIG)

S5 Including Gas metal arc welding processes (MIG)

S6 Including Manual metal arc welding processes (STICK)

S7 Including Plasma welding processes

S8 Including Major structural repairs -Pressurised aircraft

S9 Including Major structural repairs -Unpressurised aircraft



M3 Including Weapons and gunnery B1

M4 Including Attack & self-protection management systems B1

M5 Including Surveillance Systems B1

M6 Including Sonar Systems B1

M7 Including Image recording and optical systems B1

M8 Including Electronic warfare systems B1


B2




E6.2 Excluding Avionics advanced troubleshooting

E18 Excluding ADF systems

E19 Excluding VOR systems

58

E20 Excluding ILS systems

E21 Excluding radar systems

E22 Excluding ATC, Radio altimeter, transponder, DME & Doppler systems

E26 Excluding Satellite navigation systems

E28.1 Excluding Multi-axis autopilots Fixed Wing

E28.2 Excluding Multi-axis autopilots Rotary Wing

E29 Excluding remote indicating compass systems

E30 Excluding Inertial navigation and reference systems

E31 Excluding Cabin pressurisation instrument and control systems

E34 Excluding Digital systems


S10 Including Termination or repair of optical fibre cable



M3.1 Including Weapons and gunnery B2

M4.1 Including Attack & self-protection management systems B2

M5.1 Including Surveillance Systems B2

M6.1 Including Sonar Systems B2

M7.1 Including Image recording and optical systems B2

M8.1 Including Electronic warfare systems B2


Appendix B

59

Type rated aircraft and type rating endorsements for Category B1, B2 or C licences

Type Certificate (TC) holder Aircraft type Military Designation EIAC

Army Sikorsky S-70A Blackhawk A25

Airbus - MRH90 Taipan A40

Airbus - ARH Tiger A38

Boeing CH47F Chinook A15

Navy Sikorsky MH-60R Seahawk N48

Airbus EC135 Eurocopter EC 135 (Turbomeca Arrius 2B) N52

SRG Boeing P-8A Poseidon A47

Lockheed Martin AP-3C Orion A09

Boeing E-7A Wedgetail A30

AMG Lockheed Martin C-130J Hercules A97

C-27J Spartan A34

Boeing C17 Globemaster A41

Airbus KC-30A MRTT A39

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

A36

Bombardier CL-600-2B16

Challenger

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

(GE CF34)

A37

Dassault Falcon 7X Falcon 7X A56

ACG Boeing F/A-18A Hornet A21

Boeing FA-18F Super Hornet A44

Boeing EA-18G Growler A46

BAE Hawk 127 Hawk A27

Lockheed F-35A JSF A35

AFTG Pilatus PC-9 A23

Pilatus PC-21 A54

Hawker Beechcraft King Air B300

Super King Air Beech 300 Series

(PWC PT6) A32

Appendix C

60

List of Superseded UOC Codes in MEA Aeroskills Package Revision 4.0

UOC Code Title Released Superseded by* Title Released

MEA101 Interpret work health and safety practices in aviation maintenance 11-Feb-15 MEA154 Apply work health and safety practices in

aviation maintenance 31-Aug-18

MEA103 Plan and organise aviation maintenance work activities 11-Feb-15 MEA155 Plan and organise aviation maintenance

work activities 31-Aug-18

MEA105 Apply quality standards applicable to aviation maintenance 11-Feb-15 MEA156 Apply quality standards during aviation

maintenance activities 31-Aug-18

MEA108 Complete aviation maintenance industry documentation 11-Feb-15 MEA157 Complete aviation maintenance industry

documentation 31-Aug-18

MEA109 Perform basic hand skills, standard trade practices and fundamentals in aviation maintenance

11-Feb-15 MEA158 Perform basic hand skills, standard trade practices and fundamentals in aviation maintenance

31-Aug-18

MEA205 Remove and install advanced aircraft instrument system components

11-Feb-15 MEA292 Remove and install advanced aircraft

instrument system components 31-Aug-18

MEA207 Remove and install aircraft electronic system components 12-Feb-15 MEA293 Remove and install aircraft electronic

system components 31-Aug-18

MEA211 Inspect, test and troubleshoot advanced aircraft electrical systems and components 12-Feb-15 MEA294

Inspect, test and troubleshoot advanced aircraft electrical systems and components

31-Aug-18

61

UOC Code Title Released Superseded by* Title Released

MEA240 Use electrical test equipment to perform basic electrical tests 11-Feb-15 MEA295

Use electrical test equipment to perform basic electrical tests on aircraft and components

31-Aug-18

MEA260 Use electrical test equipment 12-Feb-15 MEA296 Use electrical test equipment in aviation maintenance activities 31-Aug-18

MEA302 Remove and install aircraft hydro-mechanical and landing gear system components 11-Feb-15 MEA398

Remove and install aircraft hydro-mechanical and landing gear system components

31-Aug-18

MEA311 Inspect and repair/modify aircraft structures 30-Jul-04 MEA369 Inspect and maintain structures and related components of non-pressurised small aircraft

31-AUG-18

DEFEO101D Work safely with explosive ordnance 24-Jan-13 DEFEXO001 Work safely with explosive ordnance 22-Oct-15

MSAENV472 Implement and monitor environmentally sustainable work practices 01-Dec-05 MSMENV472 Implement and monitor environmentally

sustainable work practices 15-Dec-15

*Unless otherwise indicated, courses given new UOCs are considered to be equivalent to the previous versions.

Appendix D

62

List of Approved Alternate UOC Codes

Exclusion/Inclusion Required MEA Code

Approved Alternate against listed Exclusion/Inclusion

E6.1, E29, E60, M2, M3.1, M4.1, M5.1, M6.1, M7.1, M8.1 213 224 + 228

E6.1, E18, E19, M5.1, M6.1, M8.1 214 226 + 229

E6.1, M4.1, M5.1, M6.1, M7.1, M8.1 215 226 + 229

E20. M5.1, M6.1, M8.1 216 226 + 229

E28.1 217 225 + 230

E31 219 224 + 228

E21, M4.1, M5.1, M6.1, M7.1, M8.1 220 226 + 232

E22, M4.1, M5.1, M6.1, M7.1, M8.1 221 232 + 226

E1, E6.1, M2.1, M3.1, M4.1, M5, M5.1, M6, M6.1, M7, M7.1, M8,

M8.1 294* 223 + 227

E2.4, E2.6, S9 304 317*

M2 304 603 + 605

E2.1, E42, E61 309 318 + 320

E2.1, E60 310 318 + 320

E61 312 321 + [309 or 315 or 316 or 318]

E3.1 314 319 + 322

E2.1 321 312*

E2.1, E2.2, E3.1, E3.2 323 SG3ATT

E2.5, E2.6 339 311

E2.5, E2.6 339 401 + 405+ 410+ 420+ 422**

E14 362 AURETU004 or AURETU3004

63

Exclusion/Inclusion Required MEA Code

Approved Alternate against listed Exclusion/Inclusion

E2.3, E2.4 401 + 410 339*

S8, S9 420 + 421 402

S8, S9 422 403

S8, S9 423 404

M3 603 + 605 304 or 317 + suitable type course

*is higher and incorporates. ** in combination are higher and incorporate Example 1. An applicant applying for removal of exclusion E2.4 from their licence must have completed either MEA339 or a combination of MEA401 and MEA410. Example 2. An applicant applying for inclusion S9 must have completed either MEA403 or MEA422. Example 3. An applicant applying for inclusion M6.1 must have completed MEA221 or a combination of MEA232 and MEA226. Example 4. An applicant applying for removal of exclusion E2.6 must have completed either MEA339, or completed all of MEA401, MEA405, MEA410, MEA420 and MEA422.

Appendix E

64

S1000D: Standard Numbering System – Air Vehicle, Engines and Equipment The S1000D is a numerical technical classification of all the systems and sub systems on an aircraft, which is universally used in aircraft engineering and aircraft maintenance and helps to standardize data across aircraft manufacturers and programs to facilitate improved maintenance and logistics. A detailed breakdown of the numbering system can be found at the DASA 66 webpage: https://www.defence.gov.au/DASP/Docs/DASR-Documents/Part66/S1000DSNSCodes.pdf.

System Title Definition

0 Product General General information for the complete Product, procedures for the Product safety and general Product maintenance, use of the Product safety and protective devices, information on the technical publication required to support the Product.

1 N/A

2 N/A

3 N/A

4 Worthiness (fit for purpose) limitations

This System provides guidance for the calculation of lives for critical items/components and defines the operating parameters for such calculations.

5 Scheduled/ unscheduled maintenance Manufacturers’ recommendation for time limits inspection (both scheduled and unscheduled).

6 Dimensions and areas Those illustrations and text which show the principal dimensions of the Product and the zones, areas and reference lines used to locate sub-assemblies/components. It also includes all access and drainage provisions.

7 Lifting, shoring, recovering and transporting

Includes all necessary procedures to lift the Product with jacks or slings, and to recover it in any of the conditions to which it can be subjected, including maintenance and repair. It also includes information on recovering the Product from any condition to which it can be subjected (including emergency recovering) and how to transport it by air/road/rail, etc.

https://www.defence.gov.au/DASP/Docs/DASR-Documents/Part66/S1000DSNSCodes.pdf

65


8 Levelling and weighing

This System includes the necessary information to level the Product for any of the various maintenance, overhaul or major repairs which becomes necessary during the life of the Product. It also includes those on- Product sub-assemblies or components which are specifically dedicated to record, store or compute mass and balance data. Includes those maintenance practices necessary to prepare the Product for weighing and the weighing procedure. Mass and center of gravity (c.g.) data also to be included.

9 Handling and maneuvering Those instructions necessary to handle and taxi the Product. Illustrations showing the location of attachment points, turning radius, etc, are included. Includes those maintenance procedures necessary to prepare the Product for handling and taxiing.

10 Parking, mooring, storing and return to service

This System is to contain the necessary information to park, moor and/or store the Product in all conditions to which it can be subjected. Where appropriate, it is to include the procedures to prepare for parking, mooring and storing and any related return to service requirements. Illustrations, where appropriate, are to show, for example, locations of any fixing or mooring points and any controls used in the parking/mooring and storing procedure.

11 Placards and markings

All procurable placards, labels, etc, is included in the Illustrated Parts Catalog. They are illustrated, showing the part number, legend and location. The maintenance publications must provide the approximate location (eg, FWD UPPER RH) and illustrate each placard, label, marking, self-illuminating sign, etc, required for safety information, maintenance significant information or by government regulations. Those required by government regulations are so identified.

12 Servicing

Those instructions for the replenishment and depletion of fluids, scheduled and unscheduled servicing, applicable to the whole Product. The information is concise and preferably in tabular or chart form. Precautions to be observed in servicing a particular container (eg, tank, reservoir, bottle, LOX converter, tire) such as grounding and prevention of fire hazards, is clearly stated. A diagram showing the location of regular and emergency servicing points is included. "No-step" areas or walkways, with necessary precautions, are indicated.

13 N/A

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14 Product loading and offloading

This System contains those procedures and illustrations necessary to load and offload internal and external stores and munitions and cargo. The System also contains information on the support equipment and special tools required. Cross-references are made to applicable systems for information on the Product attachment points, pylons and carriers.

15 Crew information

This System provides all specific information given to crew for performing all the designed missions of the Product. Description and function of the Product systems, system controls and installed equipment are included only to the extent that the information is essential to crew/operators and is not covered in the relevant system (21 and up).

16 Change of role Those instructions necessary to change the Product from one role to another.

17 N/A

18 Vibration and noise analysis and attenuation

This System provides the necessary information to enable operators to monitor and diagnose vibration and noise levels in order to identify imbalance, damage or misalignment in the Product dynamic and structural components. It also includes those Product and components which furnish a means of automatically controlling and/or reducing the force and/or value of the levels of vibration and/or noise within the Product through the use of active or passive systems/equipment.

19 N/A

20 Standard practices - Airframe systems

This System contains those standard mechanical and electrical electric/engineering practices applicable to more than one airframe system task which are not covered in systems 21 thru 49. It excludes those practices which are recognized as standard trade practices and also those practices/processes which are only applicable to manufacture. Practices for a particular application must be included in the appropriate airframe system as part of the procedure.

21 Environmental control

Those units and components which furnish a means of pressurizing, heating, cooling, moisture controlling, filtering and treating the air used to ventilate the areas of the fuselage within the pressure seals. Includes cabin supercharger, equipment cooling, heater, heater fuel system, expansion turbine, valves, scoops, ducts, cabin seals, etc. Also includes such systems as canopy/door seals, anti-g, demisting, waveguide pressurization, etc.

22 Auto Flight Those units and components which furnish a means of automatically controlling the flight of the air vehicle. Includes those units and components which control direction, heading, attitude, altitude and speed.

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23 Communications Those units and components which furnish a means of communicating from one part of the air vehicle to another and between the air vehicle or ground stations. Includes voice, data C-W communicating components, PA system, intercom and tape reproducers-record player.

24 Electrical Power

Those electrical units and components which generate, control and supply AC and/or DC electrical power for other systems, including generators and relays, inverters, batteries etc., through the secondary busses. Also includes those units and components which provide for multiplexing of electrical power and common electrical items such as wiring, switches, connectors, etc.

25 Equipment/furnishings Those removable items of equipment and furnishings contained in the flight and passenger compartments. Includes emergency, buffet and lavatory equipment. Does not include structures of equipment assigned specifically to other systems.

26 Fire protection Those fixed and portable units and components which detect and indicate fire or smoke and store and distribute fire extinguishing agent to all protected areas of the air vehicle; including bottles, valves, tubing, etc.

27 Flight controls

Those units and components which furnish the means of controlling the flight attitude characteristics of the air vehicle. Also includes the functioning and maintenance of the primary and secondary flying control surfaces and lift augmenting systems but not the maintenance of the structure of control surfaces which is covered by the system structures. Includes items such as control stick grips, rudder pedals, gearboxes, control rods and cables, linkages, hydraulic valves, actuators, control units, controls and indicators, computers, transducers, transformers, sensor units, displays, gyros, accelerometers, servos, warning systems and control locking devices. This includes rotorcraft rotor controls which are covered in the rotor systems.

28 Fuel

Those units and components which store and deliver fuel to the engine. Includes engine driven fuel pumps for reciprocating engines, includes tanks (bladder), valves, boost pumps etc, and those components which furnish a means of dumping fuel overboard. Includes integral and tip fuel tank leak detection and sealing. Does not include the structure of integral or tip fuel tanks and the fuel cell backing boards which are covered by the system structures, and does not include fuel flow rate sensing, transmitting and/or indicating, which are covered in System 73.

29 Hydraulic Power Those units and components which furnish hydraulic fluid under pressure (includes pumps, regulators, lines, valves etc) to a common point (manifold) for redistribution to other defined systems.

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30 Ice and rain protection

Those units and components which provide a means of preventing or disposing of formation of ice and rain on various parts of the aircraft. Includes alcohol pump, valves, tanks, propeller/rotor anti-icing system, wing heaters, water line heaters, pitot heaters, scoop heaters, windshield wipers and the electrical and heated air portion of windshield ice control. Does not include the basic windshield panel

31 Indicating/recording systems

Pictorial coverage of all instruments, instrument panels and controls. Procedural coverage of those systems which give visual or aural warning of conditions in unrelated systems. Includes units which record, store or compute data from unrelated systems and those units/systems that integrate indicating instruments into a central display system and instruments not related to any specific system.

32 Landing gear

Those units and components which furnish a means of supporting and steering the air vehicle on the ground or water, and make it possible to retract and store the landing gear in flight. ncludes tail skid assembly, arresting hooks, landing assistance equipment, drag chutes, brakes, wheels, floats, skids, skis, doors, shock struts, tires, linkages, position indicating and warning systems. Also includes the functioning and maintenance aspects of the landing gear doors but does not include the structure which is covered in System 52.

33 Lights

Lights Those units and components (electrically powered) which provide for external and internal illumination such as landing lights, taxi lights, position lights, rotating lights, ice lights, master warning lights, passenger reading and cabin dome lights, etc. Includes light fixtures, switches and wiring. Does not include warning lights for individual systems or self illuminating signs. Does not include lamps/bulbs which are covered in System 25.

34 Navigation Those units and components which provide air vehicle navigational information. Includes VOR, pitot, static, ILS, flight director, compasses, indicators, etc.

35 Oxygen Those units and components which store, generate, regulate, indicate, deliver and control oxygen to the passengers and crew, including bottles, relief valves, shut-off valves, outlets, regulators, masks, walk-around bottles, etc.

36 Pneumatic Those units and components (ducts and valves) which deliver large volumes of compressed air from a power source to connecting points for such other systems as air conditioning, pressurization, de-icing, etc.

37 Vacuum Those units and components used to generate, deliver and regulate negative air pressure, including pumps, regulators, lines etc, through and including the manifold.

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38 Water/waste Those fixed units and components which store and deliver for use, fresh water, and those fixed components which store and furnish a means of removal of water and waste. Includes wash basins, toilet assemblies, tanks, valves, etc.

39 Attack system management Those functions and hardware used for attack system management. That includes digital information networking, crew-machine communication management (including knowledge-based help), stores management etc.

40 Operational attack functions Those functions and hardware used for attack system operational aim. Links of these functions with technical functions are included

41 Water Ballast Those units and components provided for the storage, balancing, control, filling, discharge and dumping of water ballast. Does not include units or components covered in System 38

42 Cross-technical attack functions

Those functions and hardware used for attacks execution. These technical functions considered in this System are common to many attack system operational functions, and therefore within the "crossroad" of the attack system

42 Integrated modular avionics

Generalize computing devices that can host software applications for system functions that had traditionally been implemented in dedicated hardware. The actual system functions are covered in their respective systems.

43 Tactical communications

Those units and components that furnish the crew with a means of communicating within the air vehicle, one air vehicle to another, and from the air vehicle to ground stations. Includes voice, C-W communicating components, PA system, intercom and recorder/record player.

44 Cabin systems

Those units and components which furnish a means of entertaining the passengers and providing communication within the aircraft and between the aircraft cabin and ground stations. Includes voice, data, music and video transmissions. Does not include SATCOM, HF, VHF, UHF, and all transmitting/receiving equipment, antennas, etc, which are covered in System 23 or System 46.

45 Central maintenance system (CMS)

Those units, components and associated system which interfaces with multiple air vehicle systems. Contains checkout and fault isolation procedures using a central computer complex and/or standard fault isolation procedures to locate a single system or component malfunction

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46 Information system

Those units and components, which furnish a means of storing, updating and retrieving digital information traditionally provided on paper, microfilm, or microfiche. Includes units that are dedicated to the information storage and retrieval function such as the Electronic Library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display.

47 Liquid nitrogen Those units and components used to generate, store, deliver and regulate liquid nitrogen to 2 or more using systems. Includes regulators, lines, manifolds, etc. Does not include liquid nitrogen handling components of the using system (ie, System 21-80).

48 In-flight refuelling tanker

Those units and components which store, and deliver fuel to a receiver vehicle while in flight. Includes fuel storage units, distribution system, controls, sensors, etc, specifically used for in-flight refuelling supply. Includes interfaces with other systems but does not include any dual purpose item that is identified with another system.

49 Airborne auxiliary power

Those airborne power plants (engines) which are installed on the air vehicle for the purpose of generating and supplying a single type or combination of auxiliary electric, hydraulic, pneumatic or other power. Includes power and drive section, fuel, ignition and control systems; also wiring, indicators, plumbing, valves and ducts up to the power unit. Does not include generators, alternators, hydraulic pumps etc, or their connecting systems which supply and deliver power to their respective air vehicle systems.

50 Cargo and accessory Compartment

Those compartments for storage of cargo and various components and accessories. Includes those systems used to load/unload cargo and other cargo related systems. Does not include aircraft structure which is in System 53.

51 Standard practices - Structures

This System contains those standard practices, general procedures and typical repairs applicable to more than one structural task which are not specifically covered in Systems 52 thru 57. This excludes those standard practices which are recognized as standard trade practices, also those practices/processes which are only applicable to manufacture. Practices for a particular application are included in the appropriate structural system as part of the procedure.

52 Doors Removable units used for entrance or exit and for enclosing other structure contained within the fuselage. Includes passenger and crew doors, cargo doors, emergency exits, etc. Electrical and hydraulic systems associated with door control are included as appropriate

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53 Fuselage

Structural units and associated components and members which make up the compartments for equipment, passengers, crew, cargo, plus the structure of the envelope and gondola of airships. Includes skins, belt frames, stringers, floor beams, floor, pressure dome, scuppers, tail cone, fuselage-to-wing and- empennage fillets, attach/attached fittings, load curtains, cables, ballonets, etc. Also includes structural and removable pylons used for the carriage of external stores. Does not cover those pylons used for weapons which are covered in System 94-30.

54 Nacelles/pylons

Structural units and associated components and members which furnish a means of mounting and housing the power plant or rotor assembly. Includes skins, longerons, belt frames, stringers, clamshells, scuppers, doors, nacelle fillets, attach/attached fittings, etc. Also includes the structure of power plant cowling inclusive of the structural portion of the inlet whether or not integral with the air vehicle. Structural portions of the exhaust systems are excluded where they are not integral with the airframe.

55 Stabilizers Horizontal and vertical stabilizers. Includes the structure of the elevator, rudder, auxiliary stabilizers and strakes.

56 Windows and canopies Fuselage and crew compartment windows and canopies, inclusive of windshield; also those windows installed in doors. Associated electrical/hydraulic/pneumatic actuation systems are to be included

57 Wings

Center wing and outer wing structural units and associated components and members which support the air vehicle in flight. Includes spars, skins, ribs, stringers, clamshells, scuppers etc., and integral fuel tank structure of the flaps, slats, ailerons or elevons (complete with tabs) and spoilers. Also includes structural and removable pylons used for carriage of external stores. Does not cover those pylons used for weapons which are covered in System 94-30.

58 N/A

59 N/A

60 Standard practices, Propeller/rotor

This system contains those standard mechanical and electrical/electronic engineering practices applicable to more than one propeller/rotor which are not covered in Systems 61 thru 69. It excludes those practices which are recognized as standard trade practices, also those practices/processes which are only applicable to manufacture. Practices for a particular application are included in the appropriate propeller/rotor system as part of the procedure.

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61 Propellers/propulsors

The complete mechanical or electrical propeller, pumps, motors, governor, alternators and those units and components external to or integral with the engine used to control the propeller blade angle. Includes propeller spinner synchronizers. Also includes propulsor duct assemblies, including aerodynamic fairing of mechanical components, stators, vectoring systems, etc.

62 Main rotors Rotor head assemblies and rotor blades, including the swash plate assemblies and the rotor shaft units if not an integral part of the gearboxes. Does not include the rotor anti-icing system which is dealt with in System 30, Ice and Rain Protection.

63 Main rotor drives Includes all components transmitting power to the rotors: engine coupling components, drive shafts, clutch and free wheel units, gearboxes, it’s (their) components, systems and securing elements

64 Tail rotor Assembly that rotates in a plane nearly parallel to the symmetry plane and delivers a thrust opposing to the main rotor torque thus ensuring yaw control. Includes the rotor blades and rotor head. Does not include the rotor anti-icing system which is dealt with in System 30, Ice and Rain Protection.

65 Tail rotor drive Includes all the components transmitting power to the tail rotor: drive shafts, bearings, gearboxes.

66 Folding blades/pylon

The whole of the system which provides automatic or manual folding and spreading of the rotor blades and/or tail pylon. Note Procedures produced in accordance with this system can also affect the components described by other systems.

67 Rotors flight control The system which provides means of manually controlling the flight attitude of the helicopter. Includes items such as control linkage and control cables for collective pitch, cyclic pitch, directional control, servo-controls and corresponding system. The trim system and the indicating and monitoring system.

68 N/A

69 N/A

70 Standard practices, Engine

This system contains those standard mechanical, electrical, electronic etc., engineering practices applicable to more than one engine task which are not covered in Systems 71 thru 84. It excludes those practices which are recognized as standard trade practices, also those practices/processes which are only applicable to manufacture. Practices for a particular application are included in the appropriate engine system as part of the procedure.

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71 Power plant The overall power package including engine, air intake, mount, cowling, scoops, cowl flaps.

72 Engine

Those units and components which are used to induce and convert fuel-air mixture into power. Includes, for the basic turbine engine: - air inlet, compressor, diffuser, combustion chambers, turbine and exhaust; and for the reciprocating engine: - blower and clutch, clutch control valve, cylinders, cylinder baffles, intake pipes, crankshaft assembly, etc.

Engine turbine/turboprop Ducted fan/inducted fan

Engine reciprocating

73 Engine fuel and control

For turbine engines, those units and components and associated mechanical systems or electrical circuits which furnish or control fuel to the engine beyond the main fuel quick disconnect and thrust augmenter, fuel flow rate sensing, transmitting and/or indicating units whether the units are before or beyond the quick disconnect. It includes coordinator or equivalent, engine driven fuel pump and filter assembly, main and thrust augmenter fuel controls, electronic temperature datum control, temperature datum valve, fuel manifold, fuel nozzles, fuel enrichment system, speed sensitive switch, relay box assembly, solenoid drip valve, burner drain valve, etc. For reciprocating engines, those units and components which deliver metered fuel and air to the engine. The fuel portion includes the carburettor/master control from the inlet side to the discharge nozzle, injection pumps, carburettor, injection nozzles and fuel primer. The air portion includes units from the scoop inlet to the vapour vent return and the impeller chamber.

74 Ignition

Those units and components which generate, control, furnish, or distribute an electrical current to ignite the fuel air mixture in the cylinders of reciprocating engines or in the combustion chambers or thrust augmenters of turbine engines. Includes induction vibrators, magnetos, switches, lead filters, distributors, harnesses, plugs, ignition relays, exciters and the electrical portion of spark advance.

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75 Air

For turbine engines, those external units and components and integral basic engine parts which go together to conduct air to various portions of the engine and the extension shaft and torque-meter assembly, if any. Includes compressor bleed systems used to control flow of air through the engine, cooling air systems and heated air systems for engine anti-icing. Does not include aircraft anti-icing, engine starting systems, nor exhaust supplementary air systems.

76 Engine controls

Those controls which govern operation of the engine. Includes units and components which are interconnected for emergency shutdown. For turbo-prop engines, includes linkages and controls to the coordinator or equivalent and from the coordinator or equivalent to the propeller governor, fuel control unit or other units being controlled. For reciprocating engines, includes controls for blowers. Does not include units or components which are specifically included in other systems.

77 Engine indicating

Those units, components and associated systems which indicate engine operation. Includes indicators, transmitters, analysers, etc. For turbo-prop engines includes phase detectors. Does not include systems or items which are specifically included in other systems except when indication is accomplished as part of an integrated engine instrument system (System 77-40).

78 Exhaust Those units and components which direct the engine exhaust gases overboard. For turbine engines, includes units external to the basic engine such as thrust reverser and noise suppressor. For reciprocating engines, includes augmenters, stacks, clamps, etc. Excludes exhaust driven turbines

79 Oil Those units and components external to the engine concerned with storing and delivering lubricating oil to and from the engine. Covers all units and components from the lubricating oil engine outlet to the inlet, including the inlet and outlet fittings, tank, radiator, by-pass valve etc., and auxiliary oil systems.

80 Starting Those units, components and associated systems used for starting the engine. Includes electrical, inertia air or other starter systems. Does not include ignition systems which are covered in System 74.

81 Turbines For reciprocating engines only. Includes power recovery turbine assembly and turbo-supercharger unit when external to the engine.

82 Water injection Those units and components which furnish, meter and inject water or water mixtures into the induction system, includes tanks, pumps, regulators, etc.

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83 Accessory gearboxes Those units and components which are remotely installed and connected to the engine by a drive shaft and which drive multiple types of accessories. Does not include those accessory drives which are bolted to and are immediately adjacent to the engine. The latter item is covered under System 72

84 Propulsion augmentation Those units and components that, independent of the primary propulsion system, furnish additional thrust of short duration. Includes solid or liquid propellants, controls, indicators, etc.

85 Fuel cell system

Those units and components using an electrochemical conversion process to produce electricity from a fuel (on the anode side) and an oxidant (on the cathode side). This includes reactants and reaction products supply/exhaust devices, fuel cell stacks, electric power output devices, cooling and/or heating devices and a centralized control and monitoring subsystem.

86 Lift system Those units and components, which together with the primary propulsion system furnish vector able vertical thrust allowing the aircraft to achieve short take-off and vertical landing (STOVL). Also includes those units and components which provide the means for stabilizing the aircraft when in the STOVL mode.

87 N/A

88 N/A

89 N/A

90 Recovery Those systems, units and components used to recover air vehicles and equipment.

91 Air vehiclewiring

Miscellaneous charts, diagrams and/or lists applicable to more than one system, or to system interfaces, such as wiring charts, spare wire charts, junction boxes charts, disconnect plug charts, conduit and wire routing charts, rigid tube charts, flexible hose charts, system integration diagrams, reusable hose component lists, control cable lists, multi-system consumables lists etc.

92 Radar Those units and components which comprise multifunction radar systems used on fighters (generally nose-mounted), on maritime patrol air vehicles, on AWACS-type air vehicles, etc.

93 Surveillance Those units and components which furnish a means of sensing the surrounding environment, and then process, display and record the resulting information.

94 Weapons system Those units and components which furnish a means of acquiring a target and releasing stores.

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95 Crew escape and safety Those units and components which furnish a means of ejecting or jettisoning seats, hatches, canopies, capsules etc, from the airframe also includes safety and survival equipment.

96 Missiles, drones and telemetry

Those units and components which furnish a means of launching and controlling drones

97 Image recording Those units and components which furnish a means of recording events on film, video, disc or tape, etc. Does not cover recording systems which are part of any other system or Subsystem.

98 Meteorological and atmospheric research

Those units and components which furnish a means of providing and recording measurement of natural or man-made atmospheric, gravitation and magnetic phenomena.

99 Electronic warfare Those units and components which furnish a means of detecting, analysing, jamming, or nullifying the effectiveness of defensive detection devices and communication links (tactical or not).

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End of document