E ASA AD No. : 20 14

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TE. CAP.0011 0

- 00 4 © European Aviation Safety Agency. All rights reserved. 1 / 4 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 

## EASA AIRWORTHINESS DIRECTIVE

AD No

. : 20 14

- 0280

Date: 19 December 2014

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 21.A.3B. In accordan ce with EU 1321/2014 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an air craft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [ EU 1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption]. 

### Type Approval Holder’s Name :

AIRBUS Type/Model designation(s) :

A300

- 600 , A300

- 600ST and A310 a eroplanes

TCDS Number : EASA.A. 172 and EASA A.014

F oreign AD : Not applicable

Supersedure : None



### ATA 35 Oxygen

– Passenger Chemical O xygen Generators

– Replacement

Manufacturer(s): Airbus (formerly A irbus I ndustrie )

Applicability: A310, A300

- 600 and A300

- 600ST aeroplane s , all models, all manufacturer serial numbers

.

Reason: Reports have been received indicating premature ageing o f certain passenger chemical oxygen generator s, Part Number ( P / N ) 117042

- XX

, manufactured by B/E Aerospace. Some operators reported that when they tried to activate generators

, some older units failed to activate. Given the number of failed units reported, all the generators manufactured in 1999, 2000 and 2001 must be considered u nreliable.

Th is condition

, if not corrected, could lead to failure of the generator to activate and consequently not deliver oxygen during an emergency , possibly resulting in injury to passenger s

. To address this potential unsafe condition

, Airbus issued Alert O perators Transmission (AOT) A35W008

- 14, making reference to B/E Aerospace Service Information Letter (SIL) D1019

- 01 (currently at Revision 1) and B/E Aerospace Service Bulletin ( SB ) 117042

- 35

- 001

. For the reason described above, this AD require s i dentification and replace ment of the affected oxygen generators.
Pending the on

- going investigation, this AD is considered to be an interim action and further AD action may follow.

Effective Date: 24 December 2014E ASA AD No. : 20 14

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- 00 4 © European Aviation Safety Agency. All rights reserved. 2 / 4 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. Required A ction(s) and Compliance Time(s) : Required as indicated , unless accomplished previously : (1) Within 30 days after the effective dat e of this AD, identify the date of manufacture (see Appendix 1 of this AD where this is located ) of each passenger oxyge n generator

, having a P/N as listed in Ta ble 1 of this AD

, in accordance with the instructions of Airbus AOT A35W008

- 14

. A review of aeroplane maintenance records is acceptable to make this identification , provided those records can be relied upon for the purpose of this requirement. (2) Within the compliance time specified in Table 1 of this AD, as applicable,

remove and replace each affected passenger oxygen generator from service in accordance with the instructions of Airbus AOT A35W008

- 14 and/or

, for 15 min generators

, in accordance with the instructions of B/E Aerospace SB 117042

- 35

- 001. B/E Aerospace SIL D1019

- 01 Revision 1 provides instructions for the activation and the disposal of a removed passenger oxygen generator

. Airbus AOT A35 W 00 8

- 14 (Appendix 1) includes instructions for report ing the results of the activation (including no findings) of removed units

. The data gathered from those results will be analysed to determine further action (s), if any.

Table 1

– Replacement of Passenger Oxygen Generators

P/N Compliance Time

117042

- 02 (15 min

– 2 masks) 117042

- 03 (15 min

– 3 masks) 117042

- 04 (15 min

– 4 masks) 117042

- 22 (22 min

– 2 masks) 117042

- 23 (22 min

– 3 masks) 117042

- 24 (22 min

– 4 masks) For units manufactured in 1999, before exceeding 15 years since date of manufacture, or within 30 days after the effective date of this AD, whichever occurs later
For units manufactured in 2000, before exceeding 1 4,5 years since date of manufacture, or within 6 months after the effective date of this AD, whichever occurs later
For units manufactured in 2001, before exceeding 1 4 years since date of manufacture, or within 12 months after the effective date of this AD

, whichever occurs later

( 3 ) F rom the effective date of this AD, it is allowed to install on any aeroplane a passenger oxygen generator with a P/N as listed in Table 1 of this AD, provided that the passenger oxygen generator has a manufacturing date of 200 5 or later.

Ref. Publications: Airbus AOT A35W008

- 14 d ated 1 8 December 201 4

. B/E Aerospace SB 117042

- 35

- 001 orig inal issue dated 10 December 201 4

. The use of later approved revisions of th ese document s is acceptable for compliance with the requirements of this AD. B/E Aerospace SIL D1019

- 01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator.

Remarks : 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.E ASA AD No. : 20 14

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- 00 4 © European Aviation Safety Agency. All rights reserved. 3 / 4 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication

. 3. Enquiries regarding this A D should be referred to the Safety Information Section

, Certification Directorate, EASA. E

- mail ADs@easa.europa.eu

. 4. For any question concerning the technical content of the requirements in this AD, please contact: AIRBUS

– Airworthiness Office

– E I A W

, E

- mail: continued.airworthiness

- wb.external@airbus.com

.E ASA AD No. : 20 14

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TE. CAP.0011 0

- 00 4 © European Aviation Safety Agency. All rights reserved. 4 / 4 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet.



### Appendix 1

– Passenger Oxygen Generator Date of M anufacture

Figure 1

– location of date (MM

- YY)

Figure 2

– MFG.DATE (06

- 02 = June 2002) example