| Number |
2009-0259 |
| Issued by |
 Europe |
| Issue date |
2009-12-10 |
| Effective date |
2009-12-24 |
| EASA approval number |
|
| ATA Chapter |
29 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-231
-
A320-232
-
A320-233
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus AOT A320-29A1150 at original issue.
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD.
Hamilton Sundstrand SB ERPS08M-29-8. |
| PAD number |
09-121 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 October 2009 as PAD 09-121 for consultation
until 04 November. No comments were received during the consultation
period.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research 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 – EAS Fax +33 5
61 93 44 51, E-mail: account.airworth-eas@airbus.com.
|
