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FAA AD on Pratt & Whitney JT8D-200 series turbofan engines
Washington, Usa - To prevent fracture of the 7th and 9th through 12th stage high pressure compressor (HPC) disks and 8th stage HPC hub, resulting in uncontained engine failure and damage to the airplane
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-41-AD; Amendment 39-13258; AD 2003-16-05] RIN 2120-AA64 Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines PDF Copy (If Available): Preamble Information AGENCY: Federal...
fra/pec - 51926
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency