← FAA Federal Register actions

Airworthiness Directives; General Electric Company CF6-50, -80A1/ A3, and -80C2A Series Turbofan Engines

airworthiness · Rule · Final rule. · Published 1999-09-03 · Effective 1999-11-02 · 64 FR 48286

Document

Document number
99-22967
Federal Register citation
64 FR 48286
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-09-03
Effective date
1999-11-02
FAA docket
Docket No. 98-ANE-54-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to General Electric Company (GE) CF6-50, -80A1/A3, and - 80C2A series turbofan engines installed on Airbus A300 and A310 series airplanes, that requires initial and repetitive thrust reverser inspections and checks, and allows extended repetitive inspection intervals if an optional double p-seal configuration is installed. This amendment is prompted by the report of a higher than anticipated center drive unit (CDU) cone brake failure rate which reduces the overall thrust reverser system protection against inadvertent deployment. The actions specified by this AD are intended to prevent inadvertent in- flight thrust reverser deployment, which can result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown