| Number |
2004-0009R3 |
| Issued by |
 Europe |
| Issue date |
2016-03-23 |
| Effective date |
2016-03-30 |
| EASA approval number |
|
| Contributor |
EASA Propulsion Section |
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE CORPORATION (USA)
-
250 Series II
-
250-C18
-
250-C18A
-
250-C20
-
250-C20B
-
250-C20F
-
250-C20J
-
250-C20R
-
250-C20R/1
-
250-C20R/2
-
250-C20R/4
-
250-C20S
-
250-C20W
-
250-C28/-C30/-C47
-
250-C28B
-
250-C28C
-
250-C30
-
250-C30G
-
250-C30G/2
-
250-C30M
-
250-C30P
-
250-C30S
|
| Revision |
This AD revises EASA AD 2004-0009R2 dated 25 November 2005. The original issue of this AD superseded United Kingdom (UK) Civil Aviation Authority (CAA) AD 010-12-92 Revision 2, effective date 03 March 1995.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Corporation Alert CSL A-169, A-1166, A-2113, A-3117 and A-4036 (single document), original issue dated 15 November 1990, or Revision 1 dated 5 February 2007. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
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 AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
