Airworthiness Directive · Amendment 39-10753 · Rolls-Royce Limited, Aero Division- Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines
Rolls-Royce Limited, Aero Division- Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines
Rolls-Royce Limited, (R-R) Aero Division-Bristol/ S.N.E.C.M.A. Olympus 593 Mk. 610-14-28 turbojet engines, installed on but not limited to British Aerospace/Aerospatiale Concorde series aircraft.
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.
