Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2000-02-07 · Effective 2000-03-13 · 65 FR 5759
Document
Document number
00-2687
Federal Register citation
65 FR 5759
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company CF34 Series Turbofan
Publication date
2000-02-07
Effective date
2000-03-13
FAA docket
Docket No. 99-NE-49-AD
Abstract
This amendment adopts a new airworthiness directive (AD), that requires revisions to the Engine Maintenance Program specified in the manufacturer's Instructions for Continued Airworthiness (ICA) for General Electric Company (GE) CF34 series turbofan engines to include required enhanced inspection of selected critical life-limited parts at each piece-part exposure. This AD also requires that an air carrier's approved continuous airworthiness maintenance program incorporate these inspection procedures. This amendment is prompted by a Federal Aviation Administration (FAA) study of in-service events involving uncontained failures of critical rotating engine parts that indicated the need for improved inspections. The improved inspections are needed to identify those critical rotating parts with conditions, which if allowed to continue in service, could result in uncontained failures. The actions specified by this AD are intended to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.