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FAA AD on McDonnell Douglas Corporation model MD-90/30 airplanes (2010-05-04)

Washington, Usa - To detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 8465-8467] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0783; Directorate Identifier 2009-NM-081-AD; Amendment 39-16213; AD 2010-05-04] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Corporation Model MD- 90-30...

fra/pec - 1115542

AVIONEWS - World Aeronautical Press Agency
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