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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
![](https://avionews.it/resources/big/5f740d1c185c7f5ef2bba5bec28f84e1.jpg.webp)
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