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Airworthiness Directives; General Electric Company CJ610 Series Turbojet and CF700 Series Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 1997-12-08 · Effective 1998-01-02 · 62 FR 64513

Document

Document number
97-31862
Federal Register citation
62 FR 64513
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CJ610 Series Turbojet and CF700 Series Turbofan
Publication date
1997-12-08
Effective date
1998-01-02
FAA docket
Docket No. 97-ANE-21-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CJ610 series turbojet and CF700 series turbofan engines. This action requires removal from service of possibly defective turbine torque rings and compressor drive shafts which may have been manufactured from contaminated material; and replacement with serviceable parts. This amendment is prompted by a report of a cooling plate removed from a GE CT58 series engine that was found to have an iron-rich inclusion that came from a contaminated heat lot. Parts on GE CJ610 series and CF700 series engines which were manufactured from the same and similar heat lots may also be contaminated. The actions specified in this AD are intended to prevent turbine torque ring or compressor drive shaft failure due to a manufacturing defect, which could result in an uncontained engine failure.

Source

Authoritative
Federal Register document
Machine
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