| Number |
2012-0121 |
| Issued by |
 Europe |
| Issue date |
2012-07-06 |
| Effective date |
2012-07-20 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
LEARJET, INC.
-
45
-
45 (Learjet 40)
-
45 (Learjet 45)
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None. This AD deviates from, and thereby replaces, State of Design FAA AD 2012-08-08 for the affected aeroplanes registered in an EU Member State or associated country.
|
| Publication(s) and related information |
Bombardier Learjet 45 Maintenance Manual MM-104, Revision 53, dated January 10, 2011, or Bombardier Learjet 40 Maintenance Manual MM-105, Revision 21, dated January 10, 2011.
Learjet Inc. Model 45 Maintenance Manual JAA Supplement MM-104-JAA, revision 9, dated 05 September 2011, or Model 45 (commercial designation Learjet 40) Maintenance Manual EASA Supplement MM-105-EASA, revision 5, dated 05 September 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-062 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 06 June 2012 as PAD 12-062 for consultation until 04 July 2012. 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[dot]eu.
|
