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FAA AD on McDonnell Douglas several models aircraft
Washington, Usa - To detect and correct cracking of the lower inboard auxiliary spar cap, which could cause excessive loads to the structure attaching the support fitting of the main landing gear (MLG) to the wing, and result in loss of the MLG
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-184-AD; Amendment 39-13336; AD 2003-21-02] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes;...
fra/pec - 53793
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency