AD 2004-22-07

final rule

Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines; Correction

AD Number
2004-22-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NE-43-AD
FR Citation
70 FR 10485
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
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]]


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

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.

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

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

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