Published 2005-05-05 · Federal Register document 05-8883

Airworthiness Directives; General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines. We published AD 2005-06-07 in the Federal Register on March 21, 2005, (70 FR 13365). A service bulletin number in the compliance section is incorrect. This document corrects that service bulletin number. In all other respects, the original document remains the same.

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Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2005-06-07
Effective date printed in this edition: Unknown

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Official source · 2005-05-05

Publication text

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[Federal Register Volume 70, Number 86 (Thursday, May 5, 2005)]
[Rules and Regulations]
[Pages 23783-23784]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-8883]


=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NE-41-AD; Amendment 39-14015; AD 2005-06-07]
RIN 2120-AA64


Airworthiness Directives; General Electric Company (GE) CF6-80A1/
A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie 
A300-600 and A310 Series Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series 
turbofan engines. We published AD 2005-06-07 in the Federal Register on 
March 21, 2005, (70 FR 13365). A service bulletin number in the 
compliance section is incorrect. This document corrects that service 
bulletin number. In all other respects, the original document remains 
the same.

EFFECTIVE DATE: Effective May 5, 2005.

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 AD, FR Doc. 05-5299, that 
applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines, was 
published in the Federal Register on March 21, 2005, (70 FR 13365). The 
following correction is needed:

PART 39--[CORRECTED]


Sec.  39.13  [Corrected]

0
On page 13368, in the first column, in compliance section paragraph 
(i)(2), in the sixth line, ``No. CF6-80C2A SB 78A4022, Revision 2,'' is 
corrected to read ``No. CF6-80C2A SB 78A1081, Revision 2''.


[[Page 23784]]


    Issued in Burlington, MA, on April 26, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 05-8883 Filed 5-4-05; 8:45 am]
BILLING CODE 4910-13-P

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