| Number |
US-2003-24-12R1 |
| Issued by |
 United States of America |
| Issue date |
2003-12-31 |
| Effective date |
2003-12-18 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
PRATT & WHITNEY
-
JT9D
-
JT9D-3A
-
JT9D-7
-
JT9D-7A
-
JT9D-7AH
-
JT9D-7F
-
JT9D-7H
-
JT9D-7J
|
| Revision |
This AD revises FAA AD 2003-24-12, dated December 3, 2003, to correct errors in the depicted clamping configuration (Figure 1 of the AD), which must be correct to ensure that AD compliance can be achieved. Also, an optional method to avoid having to disconnect the tube from the engine has been added to this revised AD.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Service information related to this AD, if any, may be obtained from Pratt & Whitney, 400 Main St., East Hartford, CT 06108; telephone (860) 565-7750; fax (860) 565-1605. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
