airworthiness · Rule · Final rule; request for comments. · Published 1998-09-15 · Effective 1998-09-30 · 63 FR 49278
Document
Document number
98-24403
Federal Register citation
63 FR 49278
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-09-15
Effective date
1998-09-30
FAA docket
Docket No. 98-ANE-07-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Rolls-Royce Limited, Aero Division-Bristol/ S.N.E.C.M.A. Olympus 593 series turbojet engines. This action requires initial and repetitive X-ray and ultrasonic inspections of exhaust diffuser vanes for corrosion and cracks, and, if necessary, removal from service of cracked exhaust diffusers and replacement with serviceable parts. This amendment is prompted by reports of 17 turbine exhaust diffuser modules with one or more exhaust diffuser vanes cracked. The actions specified in this AD are intended to prevent exhaust diffuser vane failure, which could result in an adverse effect on the engine oil and reheat systems, possibly causing an inflight engine shutdown or damage to the aircraft.