Paul Anthony Price CAR Part II Chapter 7 CAR 66 Issue 02 effective - - PowerPoint PPT Presentation

10th Airworthiness Consultative Committee (ACC) Workshop CAR Part II Chapter 7 – CAR 66

Presented by Paul Anthony Price

CAR Part II Chapter 7 – CAR 66

Issue 02 effective from 15 November 2013

Operators Technical & Training Group

Current Membership

• Emirates. Etihad. Fly Dubai. Air Arabia. Presidential Flight. Jet Aviation.

Emirates Aviation College. Aerogulf Services. Abu Dhabi Aviation. Helidubai. SR Technics. Fujairah Aviation Academy. Abu Dhabi Polytechnic. Execujet.

• ADAT. Falcon Aviation Services.

Operators Technical & Training Group

Technical Group Description

The Operators Technical Group was designed to incorporate members of the General Civil Aviation authority, specifically from the Licensing and Policy Departments as well as select representatives from the aviation industry whose operations have a significant involvement with the Engineering Licensing (AMEL) regulations and associated activities.

Operators Technical & Training Group

Technical Group Description

The Operators Technical Group was formed to foster a collaborative working group who will develop the future AMEL regulations for the United Arab Emirates, with final decision making authority resting with the Director General of the GCAA.

Operators Technical & Training Group

Business Objective The main objectives of the Operators Technical Group was to update the Engineering Licensing (AMEL) regulations in order to harmonize, the current GCAA Safety Affairs regulatory suite.

Operators Technical & Training Group

Business Objective Additionally, to write a forward focused set of regulations that closely mirror the EU Engineering Licensing regulations in order to meet the GCAA strategic objectives and to ensure greater synergy with other National Regulatory bodies for the betterment of the UAE Aviation Industry as a whole.

Operators Technical & Training Group

Business Objective Lastly, to foster a more open and collaborative working relationship with representatives of the UAE aviation industry, as well as members of international regulatory bodies and the international aviation industry as a whole. On completion of the amended regulation, the Technical group will continue to meet, to ensure the amended regulations meet the GCAA strategic objective, and address any ongoing issues with industry.

CAR 66.5 Aircraft Groups

The current system of 13 sections of aircraft grouping is re-arranged to THREE Groups. Group 1: complex motor-powered aircraft as well as multiple engine helicopters, aeroplanes with maximum certified operating altitude exceeding FL290, aircraft equipped with fly-by-wire systems and other aircraft requiring an aircraft type rating when defined so by the GCAA

CAR 66.5 Aircraft Groups

Group 2: aircraft other than those in Group 1 belonging to the following subgroups: sub-group 2a: single turbo-propeller engine aeroplanes sub-group 2b: single turbine engine helicopters sub-group 2c: single piston engine helicopters. Group 3: piston engine aeroplanes other than those in Group 1.

CAR 66.20 (a) Privileges

A Category B2 AMEL Shall Permit the Holder;

To issue Certificates of Release to Service and to act as B2 Support Staff for the following;

• maintenance performed on avionic and electrical systems, and
• Electrical and avionic tasks within powerplant and mechanical systems, requiring only

simple tests to prove their serviceability, and

• To issue certificates of release to service following minor scheduled line maintenance

and simple defect rectification within the limits of tasks specifically endorsed on the certification authorization referred to in point 145.35 of CAR-145

CAR 66.20 (a) Privileges

A Category B2 AMEL Shall Permit the Holder Cont;

• This certification privilege shall be restricted to work that the license holder has

personally performed in the maintenance organisation which issued the certification authorisation and limited to the ratings already endorsed in the B2 license.

• The category B2 license does not include any A subcategory

The holder of a category B2 aircraft maintenance licence may only exercise the certification privileges described in CAR 66.20(a)(3)(ii) following the satisfactory completion of (i) the relevant category A aircraft task training and (ii) 6 months of documented practical experience covering the scope of the authorisation that will be

• issued. The task training shall include practical hands on training and theoretical

training as appropriate for each task authorised. Satisfactory completion of training shall be demonstrated by an examination or by workplace assessment. Task training and examination/assessment shall be carried out by the maintenance organisation issuing the certifying staff authorisation. The practical experience shall be also

• btained within such maintenance organisation.

CAR 66.20 (b) Privileges The training courses and examinations shall be passed within 10 years prior to the application for an aircraft maintenance license or the addition of a category

• r subcategory to such aircraft maintenance license.

CAR 66.40 (a) Continued Validity of the AMEL

The aircraft maintenance licence becomes invalid eight years after its last issue or amendment, unless the holder submits his/her aircraft maintenance licence to the GCAA. The validity of the AMEL is not affected by recency of maintenance experience whereas the validity of the 66.20 privileges is affected by maintenance experience as specified in 66.20(a) GM 66.20 refers.

CAR 66.45 (a) Type/Task Training and Ratings In order to be entitled to exercise certification privileges on a specific Aircraft type the holder of an AMEL needs to have his/her license Endorsed with the relevant aircraft ratings.

CAR 66.45 (a) Type/Task Training and Ratings

For category B1, B2 or C the relevant aircraft ratings are the following:

• For group 1 aircraft, the appropriate aircraft type rating.
• For group 2 aircraft, the appropriate aircraft type rating, manufacturer sub-group

rating or full sub-group rating.

• For group 3 aircraft, the appropriate aircraft type rating or full group rating.
• For category B3, the relevant rating is ‘piston-engine non-pressurised aeroplanes
• f 2 000 kg MTOM and below’.
• For category A, no rating is required, subject to compliance with the

requirements of point 145.35 of CAR-145.

CAR 66.45 (b) Type/Task Training and Ratings

The endorsement of aircraft type ratings requires the satisfactory completion of the relevant category B1, B2 or C aircraft type training.

CAR 66.45 (c) Type/Task Training and Ratings

In addition to the requirement of point (b), the endorsement of the first aircraft type rating within a given category/sub-category requires satisfactory completion of the corresponding On the Job Experience, as described in Appendix III to CAR 66.

CAR 66.45 (f) Type/Task Training and Ratings

Group 3 Aircraft; For category B1, unless the applicant provides evidence of appropriate experience, the group 3 rating shall be subject to the following limitations, which shall be endorsed on the licence:

• pressurised aeroplanes
• metal structure aeroplanes
• composite structure aeroplanes
• wooden structure aeroplanes
• aeroplanes with metal tubing structure covered with fabric.

CAR 66.50 (a) (b) (c) Limitations

Limitations introduced on an aircraft maintenance licence are exclusions from the certification privileges and affect the aircraft in its entirety. For limitations referred to in point 66.45, limitations shall be removed upon: demonstration of appropriate experience; or after a satisfactory practical Assessment performed by the GCAA. For limitations referred to in point 66.70, limitations shall be removed upon satisfactory completion of examination on those modules/subjects defined in the applicable conversion report.

CAR 66.70 (a) Conversion Provisions

The holder of a certifying staff qualification valid, prior to the date of entry into force

• f this CAR shall be issued an aircraft maintenance licence by the GCAA without

further examination subject to the conditions specified in the conversion report. Where necessary, the aircraft maintenance licence shall contain limitations in accordance with point 66.50 to reflect the differences between the scope of the certifying staff qualification valid before the entry into force of this Regulation and the basic knowledge requirements and the basic examination standards laid down in Appendix I and II to the CAR.

Subject Module A or B1 aeroplane with: A or B1 helicopter with: B2 B3 Turbine engine(s) Piston engine(s) Turbine engine(s) Piston engine(s) Avionics Piston-engine Non-pressurised Aeroplanes 2 000 kg MTOM And below

1 X X X X X X 2 X X X X X X 3 X X X X X X 4 X X X X X X 5 X X X X X X 6 X X X X X X 7A X X X X X 7B X 8 X X X X X X 9A X X X X X 9B X 10 X X X X X X 11A X 11B X 11C X 12 X X 13 X 14 X 15 X X 16 X X X 17A X X 17B X

Category Hours Aeroplanes with a maximum take-off mass above 30 000kg; B1.1 150 B1.2 120 B2 100 C 30 Aeroplanes with a maximum take-off mass equal or less than 30 000kg and above 5 700kg B1.1 120 B1.2 100 B2 100 C 25 Aeroplanes with a maximum take-off mass of 5 700kg and below (*) B1.1 80 B1.2 60 B2 60 C 15 Helicopters (**) B1.3 120 B1.4 100 B2 100 C 25 (*) For non pressurized piston engine aeroplanes below 2000kg MTOM the minimum duration can be reduced by 50% (**) For helicopters in group 2 (as defined in point 66.45) the minimum duration can be reduced by 30%

Aircraft rating requirements

Aircraft Groups B1/B3 licence B2 licence C licence Group 1

• Complex motor-

powered aircraft

• Multiple engine

helicopters.

• Aeroplanes certified

above FL290.

• Aircraft equipped with

fly-by-wire.

• Other aircraft when

defined by the GCAA. (For B1) Individual TYPE RATING Type training:  Theory + examination  Practical + assessment PLUS OJT (for first aircraft in license subcategory) Individual TYPE RATING Type training:  Theory + examination  Practical + assessment PLUS OJT (for first aircraft in license category) Individual TYPE RATING Type training:  Theory + examination

Group 2: Subgroups: 2a: single turboprop aeroplanes (*) 2b: single turbine engine helicopters (*) 2c: single piston-engine helicopters (*) (*) Except those classified in Group 1. (For B1.1, B1.3, B1.4) Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full SUBGROUP RATING (type training + OJT) or (type examination + practical experience) on at least 3 aircraft representative of that subgroup Manufacturer SUBGROUP RATING (type training + OJT) or (type examination + practical experience)

• n at least 2 aircraft

representative of that manufacturer subgroup Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full SUBGROUP RATING based on demonstration

• f practical experience

Manufacturer SUBGROUP RATING based on demonstration of practical experience Individual TYPE RATING type training or type examination Full SUBGROUP RATING type training or type examination on at least 3 aircraft representative of that subgroup Manufacturer SUBGROUP RATING type training or type examination on at least 2 aircraft representative of that manufacturer subgroup

Group 3 Piston-engine aeroplanes (except those classified in Group 1) (For B1.2) Individual TYPE RA TING (type training + OJT) or (type examination + practical experience) Full GROUP 3 RA TING based on demonstration of practical experience Limitations:  Pressurised aeroplanes  Metal aeroplanes  Composite aeroplanes  Wooden aeroplanes  Metal tubing & fabric aeroplanes Individual TYPE RA TING (type training + OJT) or (type examination + practical experience) Full GROUP 3 RA TING based on demonstration of practical experience Individual TYPE RA TING type training or type examination Full GROUP 3 RA TING based on demonstration of practical experience

Piston-engine non-pressurised Aeroplanes of 2 000 kg MTOM and below (For B3) FULL RA TING “Piston engine non-pressurised aeroplanes of 2 000 kg MTOM and below” based on demonstration of practical experience Limitations:  Metal aeroplanes  Composite aeroplanes  Wooden aeroplanes  Metal tubing & fabric aeroplanes Not Applicable Not Applicable

Basic training courses complying with the requirements applicable before this Regulation applies may be started until 1 year after date by which this Regulation applies. Basic knowledge examinations conducted as part of these courses may comply with the requirements applicable before this Regulation applies. Basic knowledge examinations complying with the requirements applicable before this Regulation applies and conducted by the GCAA or conducted by a maintenance training

• rganisation approved in accordance with CAR 147 while not being part of a basic training

course, may be conducted until 1 year after the date by which this Regulation applies. Type training courses and type examinations complying with the requirements applicable before this Regulation applies shall be started and finished not later than 1 year after the date by which this Regulation applies.

Questions ?

CAR M Presentation Airworthiness Consultative Committee 28 November2013

Yousuf Al Azizi – Senior Inspector - Air Operators & CAMO

General Civil Aviation Authority Contents of the presentation

• E- Services
• Documents approvals – Q pulse
• Deliveries
• SMS & Audits
• ROSI

CAR M Presentation

General Civil Aviation Authority

• The GCAA has launched phase II of E-services which has

introduced the following services :

• Renewal of ARC by the GCAA Form AWF-ARC-15A
• Renewal of ARC by the CAMO Form AWF-ARC-15B
• Issuance of CAMO approval
• Renewal of CAMO approval
• Amendment of CAMO approval
• Nominated Personnel Amendment
• Nominated Personnel Renewal
• Nominated Personnel Revocation
• Nominated Personnel Initial

E-Services

General Civil Aviation Authority

Features :

• E services can be delegated within the company for specific tasks &

personnel

• All existing CAMO can use the e services for the following applications :

1.Renewal 2. Initial 3.Amendments

• Stand alone CAMO’s need to apply for E services subscription which

will enable them applying for the nomination of Accountable Manager, QA PH, CAMO PH & ARC staff.

• Existing CAMO can now apply through e services to add new ARC staff
• r change any Nominated PH.
• New AOC need to obtain their e services subscription in order to apply

for CAMO approval & Nominated PH during certification process.

E-Services

General Civil Aviation Authority

E-Services

Practices:

• Importance of entering the correct ownership details during C of

R application & C of R amendments .

• Importance of entering the proper aircraft manufacturer’s

designation as indicated in the type certificate data sheet for all applications.

• Importance of properly selecting subpart G or Subpart G + I incase
• f Renewal or Initial application of CAMO.

Future:

• GCAA are working on the next phase of e services to include Flight

Permit application.

• Also, GCAA are continuously working to enhance the current

features and to introduce new features in next phases.

General Civil Aviation Authority

Direct Bulk payment by operators:

• Some of the operators have the provision of processing

their payments towards their all application such of C of R issuance or ARC issuance on Bulk Payment basis. Agreement have been made by GCAA finance & operator’s finance departments to collect these payments\fees on monthly basis. This provision have eased and accelerated The process of these applications .

E-Services

General Civil Aviation Authority

Documents Approvals – Q Pulse

• Control of Manuals and approvals through Document Module in Q Pulse:
• Ref : Q pulse User Manual ( available on GCAA Website ).
• Initial operator manuals can also be uploaded into Q pulse for review and

approval

• Some of the existing manuals with the operator can not be uploaded since

the previous revision does not exist. Contact PAI to ensure previous revision is available on Q pulse.

General Civil Aviation Authority

Aircraft Deliveries

• A used aircraft to be imported to the UAE must be

certified in accordance with the Type Certificate Data Sheet of the State of Design

• Operators are required to comply with these requirements

by providing evidences after consultation with the manufacturer and by implementing all applicable related Service Bulletins.

General Civil Aviation Authority

Deliveries & preparations of ac certificates

• Direct Deliveries with Boeing & Airbus will be subject to 3

to 5 audits this year as part of GCAA oversight on the process.

• Delivery forecast 2014 to be submitted during December

13 in order to assign inspector and properly manage our resources.

• Importance of maintaining 2 weeks minimum for

submitting e service applications of C of R, C of A , ARC’s , Noise, De Registration or Export C of A to GCAA in order to prepare the certificates & assign inspectors.

General Civil Aviation Authority

SMS & Audits

• Audit plans for 2014 will be published to operators prior end of this

year through the assigned PAI.

• ACAP product audit ( Aircraft Continuing Airworthiness Program )
• SMS audits
• Based on Risk Assessment by GCAA, the Airworthiness will conduct

several audits on several operators throughout the year.

General Civil Aviation Authority

ROSI

• Importance of referring to the exact requirement and criteria
• f reporting safety incidents as per CAAP 22.
• Analysis of Internal Safety Reports – ROSI’s

General Civil Aviation Authority

Questions ?

CAR M Presentation

CAR M Presentation Airworthiness Consultative Committee 28 November2013

Warren Storey – Senior Inspector - Air Operators & CAMO

General Civil Aviation Authority Contents of the presentation

• CAR M Amendment
• CAR M Guidance Material

CAR M Presentation

General Civil Aviation Authority

• CAR M 708(a)

All continuing airworthiness management shall be carried

• ut according to the prescriptions of Section A, Subpart C of this

Chapter (CAR M).

• CAR M 710(b)

The airworthiness review staff of the approved continuing airworthiness management organisation shall carry out a physical survey of the aircraft. For this survey, airworthiness review staff not appropriately qualified to issue a CAR M Subpart H or CAR 145 CRS as appropriate for the type, for any work that may be carried out, shall be assisted by such qualified personnel.

CAR M Amendment

General Civil Aviation Authority

• CAR M 716(a) and (b)

Level One (1): A significant non-compliance with CAR M regulations, which could jeopardize overall safety and require immediate corrective action. An organisation’s approval Certificate may be provisionally suspended in whole or in part depending upon the extent of the Level 1 finding until corrective action has been taken. Level Two (2): Non-compliance with CAR M regulations or continuing airworthiness management organisation procedures, which may lower the Organisation’s operation, maintenance and safety () standard, which require corrective action and compliance within a period not exceeding thirty (30) days of first notification (inspectors shall use their discretion in setting the time frame)

CAR M Amendment

General Civil Aviation Authority

• Appendix 1 to AMC to CAR M 302

1.1.21 Operators and continuing airworthiness management

• rganisations are required to develop procedures to comply with

maintenance requirements for cockpit voice recorders (CVR) and (digital) flight data recorders FDR(DFDR):

• CVR – Each 6 m, confirm proper recording of each audio channel

and bulk erase inhibit logic

• FDR/DFDR - Each 3,000 fh/12 m, download and analyse at least a

whole flight recording. Check all mandatory parameters are active and are of acceptable quality and

• FDR/DFDR - Pre-Flight: check for no-failure

CAR M Amendment

General Civil Aviation Authority

• Appendix 1 to AMC to CAR M 302

1.1.22 Annual inspections should be included as follows:

• FDR/DFDR – A complete flight from the FDR(DFDR) should be

examined in engineering units to evaluate the validity of all recorded parameters. Particular attention should be given to parameters from sensors dedicated to the FDR(DFDR)

• The read-out facility should have the necessary software to

accurately convert the recorded values to engineering units and to determine the status of discrete signals.

• An annual examination of the CVR recorded signals should be

carried out, preferably from in-flight recordings, to ensure intelligibility standards are met

CAR M Amendment

General Civil Aviation Authority

• Appendix 1 to AMC to CAR M 302

1.1.23 Calibration of the FDR(DFDR) system should be included in the AMP

• The FDR(DFDR) system should be re-calibrated at least every five

years to determine any discrepancies in the engineering conversion routines for the mandatory parameters ( CAR-OPS 1.715 or CAR-OPS 3.715 ), and to ensure that parameters are being recorded within the calibration tolerances 1.1.24 Continuing Airworthiness Management Exposition

• Procedures must include arrangements for rectifying defects

noted during readout checks and to control rectification in accordance with the MEL

CAR M Amendment

General Civil Aviation Authority

• Guidance Material for CAR M has been produced in line

with the earlier CAR 145 GM. The content is as follows:

• Issuance, renewal and change of a CAR M approval for
• rganisations located within the UAE
• Issuance, renewal and change of a CAR M approval for
• rganisations located outside the UAE
• Technical Log System Approval
• Aircraft Continuing Airworthiness Product Audit
• Operator Ramp Audit
• Guidance on dating the Airworthiness Review Certificate

CAR M Guidance Material

General Civil Aviation Authority

• Sections A to F: Issuance, renewal and change of a CAR M

approval for organisations located within/outside the UAE

• Includes a new Subpart G Approval Recommendation Report (AWF-ARC-003)
• This report will support any recommendation made by an Inspector and will

provide a robust record of the basis for any approval being granted, renewed

• r changed
• A separate recommendation will be made for each transaction

CAR M Guidance Material

General Civil Aviation Authority

CAR M Guidance Material

• Section H: Technical Log Approval Procedures
• Covers the 5 Sections of the Technical Log required by M.306
• Includes additional parameters that might need to be recorded

and tracked for certain aircraft or certain types of operation

• Procedures for approval of the technical log, including control of

the amendment status of each of the 5 Sections

• Also has some basic information on the approval of Electronic

Technical Logs

General Civil Aviation Authority

CAR M Guidance Material

• Section I: Aircraft Continuing Airworthiness Product Audit
• Product audit of the Subpart G process
• An ACAP audit is a “Deep Cut” sample of airworthiness
• It is a method of establishing fleet or individual aircraft condition
• As a product audit it also allows the GCAA to assess CAR M

airworthiness management and CAR 145 competence

• Can be used as credit towards the CAR M compliance audit

programme

General Civil Aviation Authority

CAR M Guidance Material

• Section I: Aircraft Continuing Airworthiness Product Audit
• 13 Key Risk Elements identified as being critical to the continuing

airworthiness of aircraft, split into 3 categories

• Each ACAP audit will include an aircraft verification survey

Aircraft Configuration

• Type design and changes
• Airworthiness Limitations
• Airworthiness Directives

Aircraft Operation

• Aircraft Documents
• Flight Manual
• Mass and Balance
• Markings and Placards
• Operational Equipment
• Defect Management

Aircraft Maintenance

• Aircraft Maintenance Programme
• Component Control
• Repairs
• Records

General Civil Aviation Authority

CAR M Guidance Material

• Section I: Aircraft Continuing Airworthiness Product Audit
• These KREs and their detailed components should be adapted to the complexity of the aircraft type

being surveyed by retaining only those items that are applicable and relevant for the particular aircraft type.

• The KREs define the scope of continuing airworthiness. The list of KREs is intended to provide the

basis for planning and control of the ACAP audit programme. It will ensure that the programme covers all aspects of continuing airworthiness. While it is not required to cover all KREs during a given inspection, the ACAP audit programme needs to ensure that there is no omission, i.e. that certain KRE are never inspected.

Title Description A. Aircraft Configuration A.1 Type design and changes to type design The type design is the part of the approved configuration of a product, as laid down in the TCDS, common to all products of that type. Any changes to type design shall be approved and, for those embodied, shall be recorded with the reference to the approval. A.2 Airworthiness limitations An airworthiness limitation is a boundary beyond which an aircraft or a component thereof must not be operated, unless the instruction(s) associated to this airworthiness limitation is (are) complied with. A.3 Airworthiness Directives An Airworthiness Directive means a document issued or adopted by the State of Design, which mandates actions to be performed on an aircraft to restore an acceptable level of safety, when evidence shows that the safety level of this aircraft may otherwise be

• compromised. (CAR 21.3B)

General Civil Aviation Authority

CAR M Guidance Material

• Section I: Aircraft Continuing Airworthiness Product Audit

A.2 Airworthiness Limitations

A.2 Airworthiness limitations An airworthiness limitation is a boundary beyond which an aircraft or a component thereof must not be operated, unless the instruction(s) associated with this airworthiness limitation is complied with. Supporting information Typical inspection items Airworthiness limitations are exclusively associated with instructions whose compliance is mandatory as part of the type design. They apply to some scheduled or unscheduled instructions that have been developed to prevent and/or to detect the most severe failure. … 1.Check that the Aircraft Maintenance Programme (AMP) reflects airworthiness limitations and associated instructions (standard or alternative) issued by the relevant design approval holders and are approved by the competent authority. 2.Check that the aircraft and the components thereof comply with the approved AMP.

General Civil Aviation Authority

CAR M Guidance Material

• Section I: Aircraft Continuing Airworthiness Product Audit

… They mainly apply to maintenance (mandatory modification, replacement, inspections, checks, etc., but can also apply to instructions to control critical design configurations (for example Critical Design Configuration Control Limitations (CDCCL) for the fuel tank safety). 3. Check the current status of life-limited parts. The current status of life-limited parts is to be maintained throughout the operating life of the part. Typical Airworthiness Limitation items: Safe Life ALI (SL ALI)/Life limited parts, Damage Tolerant ALI (DT ALI)/Structure, including ageing aircraft structure, Certification Maintenance Requirements (CMR), Ageing Systems Maintenance (ASM), including Airworthiness Limitations for Electrical Wiring Interconnection System (EWIS), Fuel Tank Ignition Prevention (FTIP)/Flammability Reduction Means (FRM), CDCCL, check wiring if any maintenance carried out in same area wiring separation, Ageing fleet inspections mandated through ALS or AD are included in the AMP. Reference documents:  CAR 21.31  CAR 21.61  EASA CS 22.1529  EASA CS 23.1529, Appendix G, para. G25.4

General Civil Aviation Authority

CAR M Guidance Material

• Section J: Operator Ramp Audit Programme
• The condition of an aircraft as sampled is to a standard acceptable for the Certificate of

Airworthiness/Airworthiness Review Certificate to remain in force,

• Required documents are on-board, including the technical log and minimum equipment list,
• Operational and emergency equipment fitted is correctly installed and serviceable or clearly

identified as unserviceable,

• The pre-flight check has been accomplished to the required standard,
• The aircraft is up to date with regard to scheduled maintenance due and deferred defects

remaining within the MEL time limits,

• Pre-flight preparation procedures are being carried out in a consistent manner to achieve the

required standards,

• Control and co-ordination of ground handling activities including aircraft loading, refuelling

and aircraft start/pushback procedures.

• Use of the technical log system is being properly carried out, especially with regard to the

reporting and control of defects, including defects noted in any cabin defects log

General Civil Aviation Authority

CAR M Guidance Material

• Section K: Dating The Airworthiness Review Certificate

General Civil Aviation Authority

CAR M Guidance Material

• Section K: Dating The Airworthiness Review Certificate

General Civil Aviation Authority

Any Questions?

CAR M PRESENTATION

General Civil Aviation Authority of UAE

10th ACC Meeting

28 Nov 2013 Zahid Munawar – Manager Engineering Safety

10th ACC Meeting 28 Nov 2012 61

• New regulation & industry guidelines
• Production organization approval
• Monetary penalty scheme
• GCAA website
• Questions / Answer

Breakdown of Presentation

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 62

New Regulations & Industry Guidelines

• Noise requirements
• Type certificate validation – updating of CAR 21 AMC & GM
• Design organization approval – Updating of CAR 21 AMC & GM

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 63

Proposed Regulation

Noise Restriction – Proposed Changes to Part V Chapter 1

• After 01 Jan 2015, no jet powered subsonic aircraft type certificated to ICAO

Annex 16 Chapter 2 or FAR Part 36 Stage 2 standards or worse, and with a Maximum Take-Off Mass (MTOM) of 75000 Pounds / 34020 Kilograms or more shall be registered in the UAE.

• After 01 Jan 2017 no jet-powered subsonic aircraft registered in the UAE,

type certificated with a Maximum Take-Off Mass (MTOM) of 75000 pounds / 34020 Kilogram or more shall be operated to and from a UAE airport, unless it is compliant with ICAO Annex 16 Chapter 3 or FAR Part 36 Stage 3 or better noise standards.

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 64

New Industry Guidelines

• Type certificate validation – updating of CAR 21 AMC & GM
• UAE Type Acceptance is need for issue of C of A & C of R
• The GCAA only validates Type Certificates Issued by:
• European Aviation Safety Agency
• US Federal Aviation Administration
• Transport Canada
• In case of Embraer or any other State of Design than the above EASA TC is validated
• CAR 21 Subpart B1, AMC/GM IB 6/2006 & IB 14/2006 provide more details
• List of validated models available on the GCAA website
• For any clarifications contact Manager Engineering Safety at zmunawar@gcaa.gov.ae

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 65

New Industry Guidelines

• Design organization approval – Updating of CAR 21 Subpart J AMC & GM
• Application process
• Fees and charges
• Design Organizations with existing EASA approval
• Requirement of data and assessment
• Investigation
• Audit
• Reports & returns
• Point of contact for queries

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 66

Production Organization Approval

• Production specialist recruited
• Mr. Khalid Al Humaidan
• By mid year 2014 the GCAA is likely to achieve capability for

issuing POA without existing EASA POA

• Regulations CAR 21 Subpart G already published
• At the moment there is no UAE POA fee

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 67

Department of Airworthiness

Engineering Safety Section

Monetary Penalty Scheme

• The GCAA plans to introduce Monetary Penalty Scheme
• Moderate enforcement action
• New CAL being drafted
• Public consultation for draft CAL is in progress
• CAR Offense Regulations draft finalized
• Proposed Fines
• Individuals
• Organizations
• Likely to be implemented by Dec 2014

10th ACC Meeting 28 Nov 2012 68

Department of Airworthiness

Engineering Safety Section

GCAA Website

• Regulations, AMC/GM and Industry Guidance material

available on the GCAA website

• List of UAE Approved Design Organization
• List of UAE Type Accepted models

10th ACC Meeting 28 Nov 2012 69

Questions / Answer

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 70

Thank You

Department of Airworthiness

Engineering Safety Section

10th ACC Meeting 28 Nov 2012 71

General Civil Aviation Authority

AIRWORTHINESS CONSULTATIVE COMMITTEE

MEETING

CAR 145 PRESENTATION

General Civil Aviation Authority 28 November 2013

Issa Al Rawahi – Senior Inspector MRO

Airworthiness Consultative Committee- 28 Nov 2013

General Civil Aviation Authority  Contents:

• CAR 145 Regulations – Rev 04 dated Aug 2013
• Certificate of Fitness for Flight (CFF)
• Application Process for CAR 145 Approval
• Term of Approval – Ratings
• Cat A LMCM & Cat C Base Certifying

Engineer.

TITLE - CAR 145 PRESENTATION

Airworthiness Consultative Committee- 28 Nov 2013

Airworthiness Consultative Committee- 28 Nov 2013

Contents:

• Examination Standard for NDT
• Component Certifying Staff Requirement
• Addition of Brazilian ANAC Airworthiness Release Certification
• Independent Inspection
• Categorization of Findings

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

TITLE - CAR 145 PRESENTATION

Airworthiness Consultative Committee- 28 Nov 2013

NPA 17 - CAR 145 Regulations changes:

• Approved & published by PRP
• Status – Rev 04 dated August 2013
• Effective – September 2013

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

 AMC 145.1 Certificate of Fitness for Flight Requirements

Requirements were extracted & revised from CAR V Chap 2 Sec 11 and inserted in CAR 145 Appendix II to AMC 145.1.

Applicability:

• If Flight Permit is required.
• If Test Flight is a post check required after

maintenance.

Requirements:

• CFF procedures must be defined in the MOE.
• Defined who are eligible to issue CFF.

TITLE - CAR 145 AMENDMENT

Airworthiness Consultative Committee- 28 Nov 2013

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

 Appendix II to GM 145.1 Certificate of Fitness for Flight Format:

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

TITLE - CAR 145 AMENDMENTS

Airworthiness Consultative Committee- 28 Nov 2013

 Maintenance Organization Approval Process

The detailed description on the application process of CAR145 is in

Appendix I to GM145.15.

There are two applicable processes:

• Part A – Applicable for Organization located in the UAE
• Part B – Applicable for Organization located outside in the

UAE

General Civil Aviation Authority

TITLE - CAR 145 PRESENTATION

Airworthiness Consultative Committee- 28 Nov 2013

TITLE - CAR 145 PRESENTATION

CAR 145 Current– E- Services:  CAR 145 Approval:

• Initial Issuance
• Renewal
• Extension

 Addition/ deletion of Line Stations  Addition/deletion of class/rating/limitation  Addition/deletion of Base Maintenance

• Amendment

 Change in ownership/name  Change in Location

Airworthiness Consultative Committee- 28 Nov 2013

 Post-Holder Approval:

• PH – Accountable Manager – Acceptance
• PH – Quality (approval)
• PH – Maintenance (approval)

 MOE Approval This service is available through Q Pulse for:

• Submission.
• Amendment.

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

 CAR 145.20 Terms of approval:

• Addition/Deletion of ATA Chapters on C5, C6 & C9
• C5 – Deletion of ATA 85 (Fuel Cell System)
• C6 – Addition of ATA 44 (Cabin System)
• ATA 45 (Central Maint System)
• ATA 50 (Cargo & Accessory Compartment)
• C9 – Addition of ATA 47 (N2 Generation System)

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

 CAR 145.30(g) – Cat A LMCM:

NOTE 1: The existing Authorized Certifying staff holding privileges to sign the Certificate of Release to Service for limited tasks defined in AMC 145.30(g) and do not hold Category “A” Line Maintenance Certifying Mechanic LMCM license issued under the provision of CAR 66, may continue to exercise the Authorization privileges as defined in the Approved MOE, as a Category “A” License, provided the following criteria are met:

• a. The Authorization was issued before July 2011,
• b. The holder is in compliance with the requirements defined in the approved MOE,
• c. No amendment to the scope of the Authorization is made, unless agreed by GCAA.

NOTE 2: The above privileges will be cancelled either upon conversion of existing AMEL into CAR 66, Company Authorization held is withdrawn or by 1 July 2015 which is the deadline set by GCAA for conversion of the license.

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

 CAR 145.30(h) – Base Certifying Engineer:

NOTE 1: The organization existing Authorized Certifying staff holding privileges to sign the Certificate Release to Service under the superseded GCAA AMEL regulation and who do not hold category “C” license issued under the provision of CAR66 may continue to exercise the certification privileges as a Category “C” license, provided the person meets the following criteria:

• a. has either full set of Mechanical (Airframe & Engine Categories) or full set of Avionics (X &

R Categories) with 3 years of type rating endorsement on the license.

• b. holds company Authorization that gives him CAR 66 Category “C” license privileges in

accordance with criteria established in the MOE. NOTE 2: The above privileges will be cancelled either upon conversion of existing AMEL into CAR 66, Company Authorization held is withdrawn or by 1 July 2015 which is the deadline set by GCAA for conversion of the license.

TITLE - CAR 145 PRESENTATION

Airworthiness Consultative Committee- 28 Nov 2013

NDT Examination Standard AMC 145.30 (f)

The acceptable standard of NDT examination by GCAA is by NDT standard controlled by a board acceptable to EASA.

Component Certifying Staff Requirements AMC 145.30(i) Clarifies the requirement of granting

authorization to Component Certifying Staff.

TITLE - CAR 145 PRESENTATION

Airworthiness Consultative Committee- 28 Nov 2013

Addition of Brazilian ANAC Airworthiness Release Certificate AMC 145.42(a) considers Brazilian AW release certificate (SEGVOO

003 Form) an equivalent document to GCAA form 1.

Deletion of Duplicate Inspection

CAR 145.65(b)(3) stipulates that organization shall establish procedures with regard to Independent Inspection in accordance with CAR M (CAR M 402).

Airworthiness Consultative Committee- 28 Nov 2013

 Findings Categorization

CAR 145.95 introduces re-definition of the finding and addition of Level 3. The major change in the current revision is that the non compliance is not limited to CAR 145 compliance only, but it has been widen to include non compliance to the Civil Aviation Law, GCAA’s regulations, the organisation’s certification requirements/conditions, terms of license or evidence of a system failure.

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

ANY QUESTIONS

TITLE - CAR 145 PRESENTATION

General Civil Aviation Authority

Airworthiness Consultative Committee- 28 Nov 2013

Thank You

TITLE - CAR 145 PRESENTATION

Maintenance Programme Optimisation Airworthiness Consultative Committee 28 November2013

Warren Storey – Senior Inspector - Air Operators & CAMO

General Civil Aviation Authority Contents of the presentation

• CAR M 302 Aircraft Maintenance Programme
• IP 44 IMRBPB Evolution/Optimisation Guidelines
• Operator Maintenance Programme Optimisation

Maintenance Programme Optimisation

General Civil Aviation Authority CAR M.302 Aircraft Maintenance programme

• CAR M 302(d)

The aircraft maintenance programme must establish compliance with: (iii) additional or alternative instructions proposed by the owner or the continuing airworthiness management organisation once approved in accordance with CAR M.302, except for intervals of safety related tasks referred in paragraph (e), which may be escalated, subject to sufficient reviews carried out in accordance with paragraph (g) and only when subject to direct approval in accordance with CAR M.302(b).

Maintenance Programme Optimisation

General Civil Aviation Authority

CAR M.302 Aircraft Maintenance programme

• AMC CAR M 302(d)3

Where an aircraft type has been subjected to the MRB report process, an operator should normally develop the initial operator’s aircraft maintenance programme based upon the MRB report.

• AMC CAR M 302(d)5

This does not prevent the approved aircraft maintenance programme from being developed in the light of service experience to beyond the MRB report recommendations but will show the relationship to such recommendations.

Maintenance Programme Optimisation

General Civil Aviation Authority

CAR M.302 Aircraft Maintenance programme

• Alternate and/or additional instructions to those defined in

paragraphs CAR M.302(d)(i) and (ii), proposed by the owner or the

• perator, may include but are not limited to the following:
• Escalation of the interval for certain tasks based on reliability data
• r other supporting information. Appendix I recommends that

the maintenance programme contains the corresponding escalation procedures. The escalation of these tasks is directly approved by the Authority, except in the case of ALIs (Airworthiness Limitations).

• More restrictive intervals than those proposed by the TC holder

as a result of the reliability data or because of a more stringent

• perational environment.

Maintenance Programme Optimisation

General Civil Aviation Authority

IP 44 IMRBPB Evolution/Optimisation Guidelines

• International Maintenance Review Board Policy Board
• Industry developed and agreed guidelines for manufacturers to

use when looking to escalate (typically) their MRB/MPD task intervals

• The OEM’s MRB Industry Steering Committee (ISC) use these

guidelines to develop the Policy and Procedures Handbook (PPH) used for each evolution process.

• The OEM will present an escalation target to the ISC who will

establish how data will be gathered and considered, how findings will be weighed, and what the minimum data size will be to be validate each task to be considered.

Maintenance Programme Optimisation

General Civil Aviation Authority

Operator Maintenance Programme Optimisation

• Operators need to demonstrate effective review of TC/STC Holder
• data. MPD / AMM Chapter 5 and ICA maintenance requirement

changes need to be reviewed by the operator to ensure that:

• ALI, CMR, Life Limited Item etc Interval reductions are adopted
• Other reductions must be adopted unless the operator’s

reliability data can support interval retention

• Task interval escalations are reviewed against reliability data to

ensure the operator’s operating experience supports the increase

• The operator should also assess the change for compatibility with

fleet utilisation and operating pattern to ensure that maintenance planning penalties will not be incurred

Maintenance Programme Optimisation

General Civil Aviation Authority

Operator Maintenance Programme Optimisation

• Operators must have a full and mature reliability programme in place
• Operators of large transport aircraft need to be active participants in

the OEM MRB process

• The OEM must be enlisted to support any operator escalation

activity

• The escalation process should be based upon the latest IP 44 IMRBPB

Evolution/Optimisation Guidelines

• The GCAA must be involved in the process from the earliest meetings

to ensure they have agreed the format and scope of the escalation process

Maintenance Programme Optimisation

General Civil Aviation Authority

Operator Maintenance Programme Optimisation

• The operator must be able to provide sufficient fleet reliability data

relating specifically to their own operations

• The maintenance programme amendment proposal must include

rules for transitioning the fleet onto the new programme intervals

• GCAA approval of any changes proposed as a result of the
• ptimisation process must be obtained
• Each task amended as part of the optimisation programme must be

properly identified within the maintenance programme

Maintenance Programme Optimisation

General Civil Aviation Authority

Any Questions?

CAR M PRESENTATION