AD 2004-22-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric Company | CF6-80C2A1 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2A2 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2A3 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2A5 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2A5F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2A8 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B1 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B1F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B2 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B2F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B4 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B4F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B5F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B6 | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B6F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B6FA | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B7F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2B8F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
| engine | General Electric Company | CF6-80C2D1F | Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines |
Unsafe Condition
This document makes a correction to Airworthiness Directive (AD) 2004-22-07. That AD applies to GE CF6-80C2 turbofan engines with certain part number (P/N) high pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed. That AD was published in the Federal Register on October 27, 2004 (69 FR 62571). The phrase "5.0 or more cycles per flight leg" in the Compliance section is incorrect. This document corrects that phrase. In all other respects, the original document remains the same.
Compliance Time
section is incorrect
Affected Aircraft
GE CF6-80C2 turbofan engines with certain part number (P/N) high pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed.
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) 2004-22-07. That AD applies to GE CF6-80C2 turbofan engines with certain part number (P/N) high pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed. That AD was published in the Federal Register on October 27, 2004 (69 FR 62571). The phrase "5.0 or more cycles per flight leg" in the Compliance section is incorrect. This document corrects that phrase. 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 42 (Friday, March 4, 2005)]
[Rules and Regulations]
[Page 10485]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 05-4072]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.
========================================================================
Federal Register / Vol. 70, No. 42 / Friday, March 4, 2005 / Rules
and Regulations
[[Page 10485]]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NE-43-AD; Amendment 39-13835; AD 2004-22-07]
RIN 2120-AA64
Airworthiness Directives; General Electric Company (GE) CF6-80C2
Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2004-22-07. That AD applies to GE CF6-80C2 turbofan engines with
certain part number (P/N) high pressure turbine stage 2 nozzle guide
vanes (HPT S2 NGVs) installed. That AD was published in the Federal
Register on October 27, 2004 (69 FR 62571). The phrase ``5.0 or more
cycles per flight leg'' in the Compliance section is incorrect. This
document corrects that phrase. In all other respects, the original
document remains the same.
EFFECTIVE DATE: Effective March 4, 2005.
FOR FURTHER INFORMATION CONTACT: Eugene Triozzi, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA; telephone (781) 238-7148;
fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-23929 that
applies to GE CF6-80C2 turbofan engines with certain P/N HPT S2 NGVs
installed, was published in the Federal Register on October 27, 2004
(69 FR 62571). The following correction is needed:
PART 39--[CORRECTED]
Sec. 39.13 [Corrected]
0
On page 62574, in the first column, in paragraph (h)(1), in the second
line, ``more cycles per flight leg,'' is corrected to read ``more hours
per flight leg,''
Issued in Burlington, MA, on February 24, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 05-4072 Filed 3-3-05; 8:45 am]
BILLING CODE 4910-13-U
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.