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FAA AD on Rolls-Royce Limited, Aero Division-Bristol, Snecma Olympus 593 Mk. 610-14-28 turbojet engines (2002-23-12)
Washington, USA - To prevent failure of the HPC stage 5 disk due to cracking, which could result in an uncontained engine failure and damage to the airplane
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-28-AD; Amendment 39-12956; AD 2002-23-12] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce Limited, Aero Division-Bristol, S.N.E.C.M.A. Olympus 593 Mk. 610-14-28 Turbojet Engines PDF Copy (If Available): Preamble Information Regulatory...
AVIONEWS - World Aeronautical Press Agency - 38072
AVIONEWS - World Aeronautical Press Agency
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AVIONEWS - World Aeronautical Press Agency