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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.

Source

Authoritative
Federal Register document
Machine
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