| Number |
US-2002-03-05 |
| Issued by |
 United States of America |
| Issue date |
2002-02-12 |
| Effective date |
2002-03-19 |
| EASA approval number |
|
| ATA Chapter |
38 |
Approval Holder
/ Type Designation |
-
BOEING
-
DC-8
-
DC-8-11
-
DC-8-12
-
DC-8-21
-
DC-8-31
-
DC-8-32
-
DC-8-33
-
DC-8-41
-
DC-8-42
-
DC-8-43
-
DC-8-51
-
DC-8-52
-
DC-8-53
-
DC-8-55
-
DC-8-61
-
DC-8-61F
-
DC-8-62
-
DC-8-62F
-
DC-8-63
-
DC-8-63F
-
DC-8-71
-
DC-8-71F
-
DC-8-72
-
DC-8-72F
-
DC-8-73
-
DC-8-73F
-
DC-8F-54
-
DC-8F-55
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Shaw Aero SB 10101000B-38-1 and SB 10101000C-38-2, both dated October 7, 1994, are related to the requirements of this AD. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
