| Number |
2010-0202R2 |
| Issued by |
 Europe |
| Issue date |
2012-02-07 |
| Effective date |
2012-02-21 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplane Section |
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
BAE SYSTEMS (OPERATIONS) LTD
|
| Revision |
Revision 2 of EASA AD 2010-0202 is issued to delay the threshold for the
initial inspection of the upper part of the NLG main fitting.
|
| Correction |
Not applicable
|
| Supersedure |
This AD revises EASA AD 2010-0202R1 dated 14 October 2010. The original
issue of EASA AD 2010-0202 dated 05 October 2010 superseded EASA
Emergency AD 2010-0001-E dated 4 January 2010 and EASA AD 2010-0072R1
dated 17 June 2010.
|
| Related information |
BAE Systems (Operations) Limited ISB.32-182 Revision 1 dated 02
November 2011.
Messier-Dowty Ltd SB 146-32-174 Revision 2 dated 16 August 2010.
Messier-Dowty Ltd SB 146-32-174 Appendix A Revision 1 dated 2
September 2009.
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. The required actions and the risk allowance have granted the issuance
of a Final AD with Request for Comments, postponing the public
consultation process after publication.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Executive Directorate, EASA. E-mail: ADs[@]easa.europa[dot]eu.
|
