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FAA AD on Pratt & Whitney Canada PT6B-36A and PT6B-36B turboshaft engines (2004-20-04)

Washington, Usa - To prevent uncontained failure of the compressor rear hub and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 1, 2004 (Volume 69, Number 190)] [Page 58824-58826] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19170; Directorate Identifier 2004-NE-18-AD; Amendment 39-13809; AD 2004-20-04] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 104522
Rome, Italy, 10/04/2004 16:15
AVIONEWS - World Aeronautical Press Agency

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