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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
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