- Effective
- February 5, 2004
- Published
- January 6, 2004 · 69 FR 494–495
- Issued
- December 23, 2003
- Models
- CF6-80E1A2, CF6-80E1A4
- Data sheet
- TCDSE41NE
- Registered aircraft
- 10 matched by model
- Product
- Engine
- Amendment
- 39-13409
- Docket
- 2003-NE-26-AD
- Issued as
- Final rule; request for comments
Unofficial copy from the Federal Register XML, document 04-144. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 136 KB | 0dc33b2b…d75e887 | 04-144.pdf on govinfo.gov |
| Official PDF | 128 KB | 63a42282…e39531a | 04-760.pdf on govinfo.gov |
| Federal Register XML | 17 KB | 17207efe…831fc70 | 04-144.xml on federalregister.gov |
| Federal Register XML | 4 KB | d0f3ee5f…4daee48 | 04-760.xml on federalregister.gov |
| FAA DRS HTML attachment | 55 KB | dfc7e4ac…a30f4ce | FAA DRS (API key needed) |
| FAA DRS PDF | 44 KB | 29ce6a94…79b1210 | FAA DRS (API key needed) |
On this page
Summary
This document makes a correction to Airworthiness Directive (AD) 2003-26-11 applicable to GE CF6-80E1A2 and -80E1A4 turbofan engines with left vertical link bolts part number (P/N) 1304M26P02 installed, and pylon attachment bolts originally torqued to 450-500 lb ft. That AD was published in the Federal Register on January 6, 2004 (69 FR 494). The SUPPLEMENTARY INFORMATION paragraph title, first sentence, and first three words of the second sentence of that paragraph were inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.
The airworthiness directive
On page 494, in the second column, under FOR FURTHER INFORMATION CONTACT: after the seventh line, add “ SUPPLEMENTARY INFORMATION: GE has notified the FAA that an unsafe condition may exist on GE CF6-80E1A2 and -80E1A4 turbofan engines. GE advises that”.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
Effective datePage 1
Effective January 14, 2004.
For further information contactPage 1
Karen Curtis, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7192; fax (781) 238-7199.
Supplementary informationPage 1
A final rule; request for comments AD, FR Doc. 04-144 applicable to GE CF6-80E1A2 and -80E1A4 turbofan engines with left vertical link bolts part number (P/N) 1304M26P02 installed, and pylon attachment bolts originally torqued to 450-500 lb ft, was published in the Federal Register on January 6, 2004 (69 FR 494). The following correction is needed:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 10
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 2015 | 4 |
|---|---|
| 2016 | 4 |
| 2017 | 2 |