Published 2004-01-14 · Federal Register document 04-760

Airworthiness Directives; General Electric Company (GE) CF6-80E1A2 and -80E1A4 Turbofan Engines; Correction

Publication 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.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:13.905821+00:00. The title, summary and date are source facts.

Source revision: federal_register_ad_metadata_2004-cb1e1f18d61cac01
Source row: results[23]
Raw source SHA-256: cb1e1f18d61cac01616802134d899b0c8ce1a9f79716b5ee037f78e4cb53a00a

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2003-26-11
Effective date printed in this edition: Unknown

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: e2649881e27b57948afd922aa3877fb300312d240ca712740fc9d946c14caf29. Source manifest: 574a7611141ddec1d1f325bdf38dbc3abcd7d67f77f8096664fbff73ed74d697.

Official source · 2004-01-14

Publication text

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[Federal Register Volume 69, Number 9 (Wednesday, January 14, 2004)]
[Rules and Regulations]
[Page 2062]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-760]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-26-AD; Amendment 39-13409; AD 2003-26-11]
RIN 2120-AA64


Airworthiness Directives; General Electric Company (GE) CF6-
80E1A2 and -80E1A4 Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments correction.

-----------------------------------------------------------------------

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.

EFFECTIVE DATE: Effective January 14, 2004.

FOR FURTHER INFORMATION CONTACT: 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 INFORMATION: 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:


Sec.  39.13  [Corrected]

0
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''.

    Issued in Burlington, MA on January 8, 2004.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 04-760 Filed 1-13-04; 8:45 am]
BILLING CODE 4910-13-P

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