E ASA AD No.: 2013

- 0196

TE. CAP.0011 0

- 00 3 © European Aviation Safety Agency. All rights reserved. 1 / 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 

## EASA AIRWORTHINESS DIRECTIVE

AD No

. : 20 13 - 0 196

Date: 28 August 2013

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation

. This AD is issued in accordance with EU 748/2012, Part 21A.3B. In accordanc e with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may ope rate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [EC 2042/2003 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption]

. 

### Design Approval Holder’s Name: AIRBUS Type/Model designation(s): A330 and A340

- 200/300 aeroplanes

TCDS Number: EASA.A.004, EASA.A.015

F oreign AD: Not applicable Supersedure: None



### ATA 92 

### E lectri c and Electronic Common I nstallation

– 

### Harness at

D oor 3 A rea – Modification
Manufacturer(s): Airbus (formerly Airbus Industries) Applicability: Airbus A330

- 201, A330

- 202, A330

- 203, A330

- 223, A330

- 243, A330

- 301, A330

- 302, A330

- 303, A330

- 321, A330

- 322, A330

- 323, A330

- 341, A330

- 342 and A330

- 343 aeroplanes, all manufacturer serial numbers (MSN) on which Airbus Modification (M od) No 48825 is embodied in production , except those on which Mod No 52485 or Mod No 40161 or Mod No 201669 are embodied

. Airbus A340

- 211, A340

- 212, A340

- 213, A340

- 311, A340

- 312 and A340

- 313 aeroplanes, all MSN on which Airbus Mod No 48825D42865 is embodied in production , except those on which Mod No 55606 or Mod No 40161 are embodied

. Reason: On the production line , electrical harnesses 1523VB and 1524VB have been found in contact with hatrack rod at Frame (FR) 53.7 between stringers (STR) 14 and 15. It was conclud ed that there is a risk of chaffing between these harnesses and the surrounding structure , which could lead to a short circuit on two oxygen chemical generator containers in different wiring routes. Consequently, the electrical opening of all the containers connected to these routes would not be possible, resulting in a malfunction of up to two thirds of the affected containers. This condition, if not corrected, could lead , in case of a sudden depressurisation event, to lack of oxygen supply, possibly resulting in injuries to aeroplane occupants

. To address this potential unsafe condition, Airbus developed two modification s of the routing of the affected harness es

.E ASA AD No.: 2013

- 0196

TE. CAP.0011 0

- 00 3 © European Aviation Safety Agency. All rights reserved. 2 / 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. For the reasons described above , this AD requires modification of the routing of harnesses 1523VB and 1524VB

. Effective Date: 11 September 2013 Required A ction(s) and Compliance Time(s) : Required as indicated, unless accomplished previously: Within 24 months after the effective date of this AD, modify the routing of the harnesses 1523VB and 1524VB at the level of the door 3 area at Left Hand and Right Hand s ide s in accordance with the instructions of Airbus SB A330

- 92

- 3098 or Airbus SB A340

- 92

- 4084 , as applicable to aeroplane model.
Ref. Public ations: Airbus SB A330

- 92

- 3098 original issue dated 11 January 2013

. Airbus SB A340

- 92

- 4084 original issue dated 11 January 2013

. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Remarks: 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD

. 2. This AD was posted on 18 June 2013 as PAD 13

- 0 80 for consultation until 16 July 2013 . The Comment Response Document can be found at http://ad.easa.europa.eu

. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Executive Directorate, EASA. E

- mail: ADs@easa.europa.eu

. 4. For any question concerning the technical content of the requirements in t his AD, please contact: Airbus

– Airworthiness Office

– EIAL; E

- mail: airworthiness.A330

- A340@airbus.com

.