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FAA AD on McDonnell Douglas DC-9-10, -20, -30, -40, and -50 series airplanes
Washington, USA - To detect and correct cracking in the fuselage skin or doubler at the corner of the forward lower cargo doorjamb, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-78-AD; Amendment 39-12998; AD 2002-26-10] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas DC-9-10, -20, -30, -40, and -50 Series Airplanes PDF Copy (If Available): Preamble Information Regulatory Information 2002-26-10...
AVIONEWS - World Aeronautical Press Agency - 38258
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency