Airworthiness Directives; Allison Engine Company AE 3007A and AE 3007C Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2000-06-08 · Effective 2000-08-07 · 65 FR 36317
Document
Document number
00-14441
Federal Register citation
65 FR 36317
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Allison
Publication date
2000-06-08
Effective date
2000-08-07
FAA docket
Docket No. 99-NE-07-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to Allison Engine Company AE 3007A and AE 3007C series turbofan engines. This AD requires revisions to the Airworthiness Limitations Section of the Allison Engine Company AE 3007A and AE 3007C Engine Manuals to include required enhanced inspection of selected critical life-limited parts at each piece-part exposure. This AD also requires an air carrier's approved continuous airworthiness maintenance program to incorporate these inspection procedures. Air carriers with an approved continuous airworthiness maintenance program will be allowed to either maintain the records showing the current status of the inspections using the record keeping system specified in the air carrier's maintenance manual or establish an acceptable alternate method of record keeping. This amendment is prompted by an 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 that, 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.