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Form No: AWF‐AMO‐009

UAE GCAA – CAR 145

Maintenance Organization Exposition Supplement

DERICHEBOURG Atis Aeronautique GCAA CAR145 Approval No.

AMO/144/04

Supplement Reference No.

MOE.SUP.01

Revision No./Date

Issue 7 of 21/09/2011

‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐ For GCAA Use:

Approval certificate/letter of 05 January 2012

Ref: 21529/55791/DXB/AW/11 HANAN M. BAHAJRI INSPECTION OFFICER

Approval and Date

General Civil Aviation Authority

UAE GCAA – CAR 145 MAINTENANCE ORGANIZATION EXPOSITION SUPPLEMENT Form No: AWF‐AMO‐009

Supplement Ref. № MOE.SUP.01 Rev. № 7 Rev. Date 21/09/2011

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INTRODUCTION This supplement in conjunction with the latest revision of the organization approved DGAC/OSAC Maintenance Organization Exposition (MOE) defines the organization and procedures upon which compliance with the Civil Aviation Regulations (CARs) of the United Arab Emirates is based and shall form the basis of acceptance by the UAE General Civil Aviation Authority (GCAA) to perform and certify maintenance on aircraft registered in the UAE or on components, or on engines, or on APUs or propellers installed on aircraft registered in the UAE under the regulatory control of the UAE GCAA. Whenever there is an amendment to the organization approved DGAC/OSAC MOE, the Quality department shall send a copy of the revised and approved EASA MOE in the form of a CD to the UAE GCAA. The Same copy of the CD shall contain the latest approved UAE GCAA MOE supplement. The supplement shall be amended as necessary to remain in compliance with the requirements of the UAE GCAA Civil Aviation Regulations. To maintain GCAA CAR 145 approval, this supplement and any subsequent amendment shall be approved by the GCAA.



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LIST OF EFFECTIVE PAGES Applicable pages: All the pages in this supplement of MOE are at the latest applicable issue (see below).

LISTE OF UPDATES

Issue Revision date Pages affected and Nature of the modification

1 20/07/06 All pages : MOE.SUP.01 creation

2 09/02/07 Logo and company name change (from ATIS Aviation to Penauille Aeronautics/ATIS Aviation). “During flight” defect report procedure deleted (line maintenance not concerned). Minor changes

3 18/10/07 Logo and company name change (from Penauille Aeronautics/ATIS Aviation to DERICHEBOURG ATIS Aéronautique/ATIS Aviation) Page 13 § 21: light wording modifications

4 01/10/08

Add A330 in the rating Company name change (from DERICHEBOURG ATIS Aéronautique/ATIS Aviation to DERICHEBOURG ATIS Aéronautique)

5 27/10/09 §19 Add Ethiad in the list of UAE Customer §20 Add B777 (GE90-115) in the rating

6 20/09/10 Addition Prague line station §20 Add A340-300 (CFM56)

7 21/09/2011 All pages: MOE SUP 01 modification in accordance with requirement with form AWF-AMO-009 §1.3 Add B777-200/300 ER/LR RR Trent 800 and GE-110/115 at PRG station.



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SUPPLEMENT REQUIREMENTS AND COMPLIANCE REFERENCE MATRIX The “Supplement Requirements and Compliance reference Matrix” provides reference on procedures documented on the Organization approved EASA/NAA MOE and also outlines the additional requirements of UAE GCAA Civil Aviation Regulations (CARs). EASA/NAA MOE Compliance Ref. REQUIREMENT UAE GCAA

Supplement Ref PART 1 – MANAGEMENT DOC MOE 02 Organization address and contact details 1.0

§1.1 Corporate Commitment by the Accountable Manager 1.1 §1.2 Safety and Quality Policy §1.3 Management Personnel 1.2 §1.4 Duties and Responsibilities of Management Personnel §1.5 Management Organization Chart §1.6 List of Certifying Staff §1.7 Manpower Resources §1.8 Facilities

DOC MOE 15 / §1.9

Scope of Work and Line Maintenance Locations 1.3

MOE SUP 01 Notification Procedure to the GCAA regarding Changes to the Organization’s Activities/Approval/Location/ Personnel

1.4

§1.11 Exposition Amendment Procedures MOE SUP 01 Supplement Amendment Procedures 1.5 MOE SUP 01 Continued Validity of Approval 1.6 MOE SUP 01 Audit by UAE GCAA 1.7

PART 2 – MAINTENANCE PROCEDURES §2.1 Supplier Evaluation and Subcontract Control Procedure §2.2 Acceptance/Inspection of Aircraft Components and Material

from outside contractors

§2.3 Storage, Tagging and release of aircraft components and material to aircraft maintenance

§2.4 Acceptance of tools and Equipment §2.5 Calibration of tools and Equipment §2.6 Use of Tooling and Equipment by staff (including

alternate tools)

§2.7 Cleanliness standards of Maintenance Facilities §2.8 Maintenance instructions and relationship to aircraft/aircraft

component manufacturer’s instructions including updating and availability to staff

§2.9 Repair procedure §2.10 Aircraft Maintenance Programme Compliance §2.11 Airworthiness Directive procedure



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EASA/NAA MOE Compliance Ref. REQUIREMENT UAE GCAA

Supplement Ref §2.12 Optional Modification Procedure §2.13 Maintenance Documentation in use and its completion §2.14 Technical Record control §2.15 Rectification of defects arising during base maintenance §2.16 Release to service procedure 2.1 §2.17 Records for the operator §2.18

DOC MOE 16 Reporting of defects to the GCAA/Operator/Manufacturer

2.2

§2.19 Return of defective aircraft components to store §2.20 Defective components to outside contractors §2.21 Control of Computer Maintenance Records Systems §2.22 Control of Manual planning Versus Scheduled Maintenance

Work

§2.23 Control of critical tasks §2.24 Specific Maintenance procedures §2.25 Procedures to defect and rectify maintenance errors §2.26 Shift/task handover procedures §2.27 Notification of Maintenance Data Inaccuracies and

Ambiguities

§2.28 Production Planning Procedures Not applicable Certificate of Maintenance Review (CMR) Procedures 2.3 Not applicable Certificate of Fitness for Flight (CFF) procedures 2.4 §2.23 Duplicate Inspection Procedures 2.5 PART L2 – ADDITIONAL LINE MAINTENANCE PROCEDURES

L2.1 Line Maintenance Control of Aircraft Components, Tools, Equipment etc…

L2.2 Line Maintenance Procedures Related To Servicing/Fuelling/Deicing etc…

L2.3 Line Maintenance Control of Defects and Repetitive Defects L2.4 Line Procedure for completion of Technical Log L2.5 Line Procedure for Pooled Parts and Loan Parts

L2.6 Line Procedure For Return of Defective Parts Removed From Aircraft

L2.7 Line Procedure For Control of Critical Tasks PART 3 – QUALITY SYSTEM PROCEDURES

§3.1 Quality Audit of Organization Procedures §3.2 Quality Audit of Aircraft §3.3 Quality Audit Remedial Action Procedure §3.4 §3.4

Certifying Staff and Category B1 and B2 Support Staff Qualification and Training Procedures

§3.5 Certifying Staff and Category B1 and B2 support staff Records



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EASA/NAA MOE Compliance Ref. REQUIREMENT UAE GCAA

Supplement Ref §3.6 Quality Audit Personnel §3.7 Qualifying Inspectors §3.8 Qualifying Mechanics

§3.9 Aircraft or Aircraft Component Maintenance Tasks Exemption Process Control

§3.10 Concession Control For Deviation from the Organization’s Procedures

§3.11 Qualification Procedure for Specialized Activities such as NDT, Welding, etc…

§3.12 Control of Manufacturers’ and other Maintenance Working Teams

§3.13 Human Factors Training Procedures §3.14 Competence Assessment of Personnel

PART 4 – CONTRACTED OPERATORS §4.1

MOE SUP 01 Contracted Operators

4.1

§4.2 MOE SUP 01

Operators Procedures and Paperwork 4.2

§4.3 Operator Records Completion PART 5 – APPENDICES

MOE SUP 01 Sample of Documents 5.1 §5.2 List of Subcontractors §5.3

DOC MOE 02 List of Line maintenance Locations

§5.4 List of Contracted Organizations



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1.0 ORGANIZATION ADDRESS AND CONTACT DETAILS Main Facility: Headquarter Head of Quality Address: DERICHEBOURG Atis Aeronautique Immeuble Thales – Parc Algorithmes 17 avenue Didier Daurat 31700 BLAGNAC FRANCE Accountable Manager Pascal LANNETTE Telephone: +33 (0)5 34 60 61 45 Fax: +33 (0)5 34 60 61 50 E‐mail: [email protected] Quality Manager Pascal PARISIS Telephone: +33 (0)5 34 60 44 32 Fax: +33 (0)5 34 60 61 50 E‐mail: [email protected]



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1.1 CORPORATE COMMITMENT BY THE ACCOUNTABLE MANAGER This supplement and the latest DGAC/OSAC approved MOE define the organization and procedures upon which the UAE GCAA CAR 145 approval is based as required by CAR 145.70. These procedures are approved by the undersigned and shall be complied with, as applicable when work/orders are being processed under the terms of GCAA CAR 145 approval. It is accepted that these procedures do not override the necessity of complying with any new or amended regulation published by the UAE GCAA from time to time where these new or amended regulations are in conflict with these procedures. It is understood that the UAE GCAA shall approve this organizations whilst the UAE GCAA is satisfied that the procedures are being followed and work standards maintained. It is further understood that the UAE GCAA reserves the right to suspend, limit or revoke the CAR 145 approval of the organization if the UAE GCAA has evidence that procedures are not followed or standards not upheld. Signed: _________________________________________ Accountable Manager

for and on Behalf of (DERICHEBOURG Atis Aeronautique)

Date: 08/11/2011



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1.2 MANAGEMENT PERSONNEL

The Senior Managers shown below are nominated by the organization and have been accepted by DGAC/OSAC and recognized by the United Arab Emirates General Civil Aviation Authority (GCAA).

These nominated persons are responsible for ensuring that the Company is in compliance with the GCAA approval requirements.

• Accountable Manager Pascal LANNETTE • Maintenance Manager Jean‐Marie LUSSAMAKI • Quality Manager Pascal PARISIS

In case, there is any change or transfer to the management personnel, letter of acceptance from DGAC/OSAC shall be forward to the GCAA If the Accountable Manager changes, the corporate commitment statement within this supplement shall be signed immediately by who supersedes the title. The statement, together letter of acceptance from DGAC/OSAC shall be forwarded to the GCAA. 1.3 SCOPE OF WORK AND LINE MAINTENANCE LOCATIONS

Scope of work Base

maintenanceLine maintenance Aircraft (Engine) UAE

OperatorB L4 L3 L2 L1 Station

B777‐200/300 RR Trent 800 Emirates X NICE A330‐200 RR Trent 700 Emirates X PRAGUE

NICE A340‐300 CFM 56 Emirates X NICE

A330‐200 RR Trent 700 Ethiad X DUBLIN B777‐200/300 GE90‐115 Ethiad X DUBLIN A340‐300 CFM 56 Emirates X PRAGUE B777‐200/300 ER/LR

RR Trent 800 and GE‐110/115Emirates X PRAGUE

SCOPE OF WORK DEFINITION: B Base Maintenance L1 Preflight, Transit check, including minor defects rectification L2 L1 checks up to and including Daily Check L3 L2 checks up to and including Weekly/Service check L4 All line maintenance checks up to and including A check



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1.4 NOTIFICATION PROCEDURE TO THE GCAA REGARDING CHANGES TO THE ORGANIZATION’S ACTIVITIES/APPROVAL/LOCATION/PERSONNEL

In accordance with UAE GCAA requirements, the Quality Assurance Manager or in his absence, his deputy, is responsible for notifying the UAE GCAA as soon as practicable of any of the changes listed below:

The name of the Organization; The location of the Organization; Additional locations of the Organization; The Accountable Manager; Any of the senior persons specified in UAE MOE Supplement/Maintenance Management

Personnel; The facilities, equipment, tools, material, procedures, certifying staff and scope of work that

could affect the GCAA approval. The purpose of this notification is to enable the GCAA to determine continued compliance and amend, if necessary, GCAA CAR 145 approval certificate.

1.5 SUPPLEMENT AMENDMENT PROCEDURES The Quality Manager is responsible for the issuance and administration of this supplement including the submission of proposed amendments to the GCAA for approval. Whenever the DGAC/OSAC MOE is amended, the Quality Manager shall ensure that the changes affecting UAE GCAA supplement are also addressed simultaneously for GCAA approval. The GCAA approval of the supplement shall be made by stamping the cover page of the supplement. 1.6 CONTINUED VALIDITY OF APPROVAL

The UAE GCAA approval certificate is valid for 1 year from the date of issue, or as stated in the certificate. The approved Organization shall forward a request for renewal to the UAE GCAA 60 days prior to the expiry date. The renewal shall be applied using GCAA form AWF‐AMO‐001 Application for CAR 145 Approval. The approval shall be renewed upon satisfying the following: a) The approved organization remains in compliance with GCAA requirements. b) Payment of any charges as prescribed by the GCAA. 1.7 AUDITS BY UAE GCAA



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The GCAA reserves the right to audit the organization’s facility and station(s) at any time during the validity period of the GCAA CAR 145 approval for which prior notice shall be served. The organization shall provide the GCAA with the necessary arrangements to access the facility and station(s) in order to determine continued compliance with GCAA requirements.

2.1 Release to Service Procedure The UAE GCAA requires that the performance of maintenance of UAE registered aircraft are carried out by UAE GCAA approved Aircraft Maintenance Organizations and certified in accordance with UAE GCAA Civil Aviation Regulations (CAR) and the organization’s release to service procedures. A certificate of release to service (CRS) shall be issued by an appropriately authorized certifying staff when satisfied that all required maintenance had been properly carried out in accordance With UAE Civil Aviation Regulations and DERICHEBOURG Atis Aeronautique (DAA) release to services procedures specified in MOE §2.16 Additionally, DERICHEBOURG Atis Aeronautique (DAA) being identified as a UAE GCAA approved maintenance organization shall annotate the UAE GCAA approval number on the aircraft Certificate of Release to Service. The Certificate of Release to service shall contain the statement laid down in CAR AMC 145.50(b) “Certifies that the work specified except as otherwise indicated was carried out in accordance with CAR 145 and in respect to that work the aircraft/aircraft component is considered fit for release to service”. AW Form 1 or EASA Form 1 with GCAA dual release shall be used, when releasing to service aircraft components, engines, or APUs. 2.2 Reporting Defects to the GGCAA/Operator/Manufacturer . Refer to CAAP 22 and ROSI online

form.

Any un‐airworthy condition or defect on UAE registered aircraft, aircraft engine or aircraft component as defined in GCAA Civil Aviation Advisory Publication CAAP 22, Appendix C shall be reported to Quality Department and Line Maintenance Manager of DERICHEBOURG Atis Aeronautique (DAA) within 24 hours from identification of the condition, using the “Reporting of Safety Incident (ROSI)” or “Occurrence Reporting Detected in Maintenance (DOC MOE 16) of (DAA)” by Station Manager (DAA). Any un‐airworthy condition or defect on UAE registered aircraft shall be reported to the GCAA within 72 hours from identification of the condition, using the “Reporting Of Safety Incident (ROSI) form, on line or print hard copies, and submit after filling in thought the GCAA FAX +971 4 2820847 by Quality Department (DAA). http://www.gcaa.ae/en/rosi/pages/reportform.aspx



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2.3 Certificate of Maintenance Review Procedures Not applicable 2.4 Certificate of Fitness for Flight Procedures Not applicable 2.5 Duplicate Inspection Procedures Reference GCAA CAR Part V, Chapter 2, Section 9, and §2.23 of MOE DERICHEBOURG Atis Aeronautique (DAA). All vital points or control systems must be identified in the Aircraft Maintenance Manuel. Whether vital points or control systems were not identified, the customer must be informed. Where vital point have been identified in the maintenance documents for the aircraft, such points shall be subject to duplicate inspection following initial assembly or following any disturbance to them or to any control system. 1. A duplicate inspection of all vital points/control systems (as indicated/provided by the UAE operator)

in an aircraft shall be made after initial assembly and before the first flight after overhaul, repair, replacement, modification or adjustment.

2. Vital points/control systems subject to duplicate inspection shall not be disturbed or readjusted after the first certified inspection and the second part of the duplicate inspection shall, as nearly as possible, follow immediately after the first part.

3. If a vital point/control system is disturbed after completion of the duplicate inspection, that part

which has been disturbed shall again be inspected in duplicate before the aircraft flies.

4. The duplicate inspection shall be the final operation to establish the integrity of the vital point/control system when all the work has been completed.

An additional inspection shall be made, when all covers and bearings are finally secured, to ensure that full, free and correct movement of the controls is obtained. 5. Persons holding valid customers approval letter with appropriate aircraft type and rating are qualified

to make first and/or second duplicate inspection. 3.1 RESERVED



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4.1 Contracted Operators

The following list contains all the UAE organizations DERICHEBOURG Atis Aéronautique provides with service: ‐Emirates ‐Ethiad

4.2 Operators Procedures and Paperwork This shall be done in accordance with approved operator procedure but in all cases it shall be specified within Maintenance Support Agreement with the operator. 5.1 SAMPLE OF DOCUMENTS

‐ Sample of ROSI form:



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‐ Samples of ETHIAD form:



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‐ Sample of EMIRATES form: