AD 2005-06-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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]
=======================================================================
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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
-----------------------------------------------------------------------
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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