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FAA AD on McDonnell Douglas model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes (2004-07-05)
Usa - To detect and correct fatigue cracking, which could result in major damage to the adjacent structure of the pylon aft spar upper cap, and consequent reduced structural integrity of the airplane
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NM-255-AD; Amendment 39-13549; AD 2004-07-05] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes PDF Copy (If Available): Preamble...
fra/pec - 61134
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency