Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2002-05-23 · Effective 2002-06-27 · 67 FR 36090
Document
Document number
02-12631
Federal Register citation
67 FR 36090
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF6-80E1 Series Turbofan
Publication date
2002-05-23
Effective date
2002-06-27
FAA docket
Docket No. 2002-NE-04-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-80E1 series turbofan engines installed on Airbus Industrie A330 series airplanes. This action requires initial and repetitive thrust reverser inspections and checks, and allows extended threshold and repetitive inspection intervals for certain inspections if an optional double p-seal configuration is installed. This amendment is prompted by reports of service-induced hardware deterioration that reduces the overall thrust reverser system protection against inadvertent deployment, which can result in loss of control of the airplane. The actions specified in this AD are intended to prevent inadvertent in-flight thrust reverser deployment, which can result in loss of control of the airplane.