Published 2004-05-07 · Federal Register document 04-10429

Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2004-07-13. That AD applies to General Electric Company (GE) CF6- 80C2 series turbofan engines. That AD was published in the Federal Register on April 1, 2004 (69 FR 17033). The amendatory text in the Applicability section is incorrect. This document corrects the aircraft models that these engines are installed on. In all other respects, the original document remains the same.

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Source revision: federal_register_ad_metadata_2004-cb1e1f18d61cac01
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Raw source SHA-256: cb1e1f18d61cac01616802134d899b0c8ce1a9f79716b5ee037f78e4cb53a00a

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2004-07-13
Effective date printed in this edition: Unknown

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 0f84fd4cd61a50fd874c60cb9bb7d02113cae2a0659f60a55bac2a7a36a63b0c. Source manifest: df33eaf0b68ca1c18a68b8d6486cf715bc13fde7c17fdd98b8412bf0d4481260.

Official source · 2004-05-07

Publication text

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[Federal Register Volume 69, Number 89 (Friday, May 7, 2004)]
[Rules and Regulations]
[Page 25488]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-10429]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-46-AD; Amendment 39-13557; AD 2004-07-13]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF6-80C2 
Series Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2004-07-13. That AD applies to General Electric Company (GE) CF6-
80C2 series turbofan engines. That AD was published in the Federal 
Register on April 1, 2004 (69 FR 17033). The amendatory text in the 
Applicability section is incorrect. This document corrects the aircraft 
models that these engines are installed on. In all other respects, the 
original document remains the same.

DATES: Effective Date: Effective April 1, 2004.

FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, 
Aircraft Certification Office, FAA, Engine and Propeller Directorate, 
12 New England Executive Park, Burlington, MA 01803; telephone (781) 
238-7192; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-7235, that 
applies to General Electric Company (GE) CF6-80C2 series turbofan 
engines was published in the Federal Register on April 1, 2004 (69 FR 
17033). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 17034, in the first column, in the Amendatory Section, 
Applicability paragraph (c), in the eighth line, ``A300 and A330'' is 
corrected to read ``A300 and A310''.

    Issued in Burlington, MA, on May 3, 2004.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 04-10429 Filed 5-6-04; 8:45 am]
BILLING CODE 4910-13-P

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