# Airworthiness Directives; Rolls-Royce Limited, Aero Division- Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines
> **Rule** · Final rule; request for comments. · Published 1998-09-15 · Effective 1998-09-30 · 63 FR 49278
## Document
- **Document number:** 98-24403
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 63 FR 49278
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/09/15/98-24403/airworthiness-directives-rolls-royce-limited-aero-division--bristolsnecma-olympus-593-series)
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