Summary
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.
Directive Details
AD Number
FAA-2009-0018
Document Number
E9-29483
Type
Rule
Publication Date
December 14, 2009
Effective Date
December 14, 2009
Affected Manufacturer
General Electric Company CF6-80C2 Series Turbofan
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2009-0018
Official Documents
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