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FAA AD on Boeing model 727 series airplanes (2004-09-36)
Usa - To prevent undetected cracking of the H-11 bolts or excessive wear of the cadmium-plated bolts, which would compromise the primary load path of the engine support and could result in separation of the engine from the airplane
Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26015-26017] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-273-AD; Amendment 39-13627; AD 2004-09-36] RIN 2120-AA64 Airworthiness...
fra/pec - 63165
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency