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FAA AD on McDonnell Douglas model MD-90-30 airplanes (2009-13-08)

Washington, Usa - To detect and correct cracks in the fail-safe structure that may not be able to sustain limit load, which could result in the loss of overall structural integrity of the horizontal stabilizer

Airworthiness Directive Federal Register Information Federal Register: [Page 30922-30924] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0160; Directorate Identifier 2008-NM-176-AD; Amendment 39-15947; AD 2009-13-08] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes PDF...

fra/pec - 1106559
Rome, Italy, 07/01/2009 16:01
AVIONEWS - World Aeronautical Press Agency

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