| Number |
US-2008-10-09R1 |
| Issued by |
 United States of America |
| Issue date |
2010-01-07 |
| Effective date |
2010-01-15 |
| EASA approval number |
|
| ATA Chapter |
28 |
Approval Holder
/ Type Designation |
-
BOEING
-
737
-
737-100
-
737-200
-
737-200C
-
737-300
-
737-400
-
737-500
|
| Revision |
This AD clarifies the intended effect of the AD on spare and on-airplane fuel tank system components, with new information concerning explanation of CDCCL requirements.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6-38278-CMR, Revision March 2008; or Boeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6-38278-CMR, Revision May 2009 |
| Remarks |
For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; e-mail me.boecom@boeing.com;
Internet https://www.myboeingfleet.com.
|
