| Number |
2009-0073R1 |
| Issued by |
Europe |
| Issue date |
2010-08-16 |
| Effective date |
2009-04-14 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 500
-
RB211 Trent 553-61
-
RB211 Trent 553A2-61
-
RB211 Trent 556-61
-
RB211 Trent 556A2-61
-
RB211 Trent 560A2-61
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
-
RB211-524
-
G2-T-19
-
G3-T-19
-
H-T-36
-
H2-T-19
|
| Revision |
This AD revises AD 2009-0073 dated 30 March 2009.
|
| Correction |
This AD has been republished in order to correct a typographical error in a Part
Number designation included in the Applicability section.
|
| Supersedure |
This AD replaces AD 2009-0073 dated 30 March 2009.
|
| Publication(s) and related information |
Rolls-Royce RB211 Propulsion System NMSB 72-AF964 Revision 1.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
09-039 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD
2. This AD was published on 17 February 2009 as PAD 09-039 for
consultation until 10 March 2009. The Comment Response Document can
be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|