AD 2005-06-07

final rule

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

AD Number
2005-06-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NE-41-AD
FR Citation
70 FR 23783
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-80A1 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
engine General Electric Company CF6-80A3 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
engine General Electric Company CF6-80C2A1 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
engine General Electric Company CF6-80C2A2 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
engine General Electric Company CF6-80C2A3 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
engine General Electric Company CF6-80C2A5 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
engine General Electric Company CF6-80C2A5F 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
engine General Electric Company CF6-80C2A8 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

Unsafe Condition

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.

Compliance Time

section is incorrect

Affected Aircraft

General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A series turbofan engines installed on Airbus Industrie A300-600 and A310 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

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.

Document Text

Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 05-8883]


=======================================================================
-----------------------------------------------------------------------

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

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

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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