Number |
2008-0226R1 |
Issued by |
Europe |
Issue date |
2012-11-16 |
Effective date |
2012-11-16 |
EASA approval number |
|
ATA Chapter |
78 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-620
-
A300F4-622R
-
A310
-
A310-221
-
A310-222
-
A310-322
-
A310-324
-
A310-325
|
Revision |
This AD revises EASA AD 2008-0226 dated 19 December 2008.
|
Correction |
N/A
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A310-78-2030 original issue
Airbus SB A300-78-6029 original issue
The use of later approved revisions of these documents is acceptable for compliance with requirements of this AD.
Pratt & Whitney SB PW4NAC 78-113 original issue
Pratt & Whitney SB PW4NAC 78-119 original issue
Pratt & Whitney SB PW7R4 78-182 original issue
Pratt & Whitney SB PW7R4 78-184 original issue
|
PAD number |
08-119 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 26 November 2008 as PAD 08-119 for consultation until 17 December 2008. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail ADs[at]easa.europa.eu.
|