Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction
airworthiness · Rule · Final rule; correction. · Published 2009-12-14 · Effective 2009-12-14 · 74 FR 66042
Document
Document number
E9-29483
Federal Register citation
74 FR 66042
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
General Electric Company CF6-80C2 Series Turbofan
Publication date
2009-12-14
Effective date
2009-12-14
FAA docket
Docket No. FAA-2009-0018
Abstract
The FAA is correcting airworthiness directive (AD) 2009-21-07, which published in the Federal Register. That AD applies to General Electric Company (GE) CF6-80C2 series turbofan engines with certain thrust reverser ballscrew gearbox assembly adjustable-length end actuators installed. The unsafe condition statement of "We are issuing this AD to prevent loss of asymmetric thrust and thrust control", and rod-end part number "MS2124S06" in paragraph (j) are incorrect. This document corrects the unsafe condition statement and the part number. In all other respects, the original document remains the same.