| Number |
US-89-25-10 |
| Issued by |
 United States of America |
| Issue date |
1989-12-01 |
| Effective date |
1990-01-04 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
TEXTRON AVIATION INC.
-
100 (King Air)
-
65 (Queen Air)
-
65-90
-
65-A90-1
-
65-A90-2
-
65-A90-3
-
65-A90-4
-
90 (King Air)
|
| Revision |
Not applicable
|
| Correction |
The FAA has approved an AMOC for this AD, which has been accepted by EASA. See attached SAIB CE-10-34, which has been revised to correct the contact information
|
| Supersedure |
This AD supersedes FAA AD 87-23-09 and FAA AD 70-25-04.
|
| Publication(s) and related information |
Beech Structural Inspection and Repair Manual (SIRM), Part Number 98-39006, Revision A4, dated May 1, 1987, or other FAA approved instructions provided by Beech Aircraft Corporation. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
