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FAA AD on Pratt & Whitney JT8D-1, -1A, -1B, -7, - 7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, and -17AR turbofan engines
Washington, Usa - To prevent first and second stage fan section separation from the low pressure compressor (LPC), resulting in turbine rotor overspeed, uncontained engine failure, and damage to the airplane
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Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-27-AD; Amendment 39-13083; AD 2003-05-07] RIN 2120-AA64 Airworthiness Directives; Pratt & Whitney JT8D-1, -1A, -1B, -7, - 7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, and -17AR Turbofan Engines PDF Copy (If Available): Preamble...
AVIONEWS - World Aeronautical Press Agency - 42142
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency