Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines; Correction
airworthiness · Rule · Final rule; correction. · Published 2005-03-04 · Effective 2005-03-04 · 70 FR 10485
Document
Document number
05-4072
Federal Register citation
70 FR 10485
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
General Electric Company (GE) CF6-80C2 Turbofan
Publication date
2005-03-04
Effective date
2005-03-04
FAA docket
Docket No. 2003-NE-43-AD
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.