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FAA AD on Bombardier model DHC-8-311 airplanes (2004-18-05)

Usa - To prevent disbonding of the subject skin panels, which could reduce the load-carrying capacity of the skin panels and result in reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 7, 2004 (Volume 69, Number 172)] [Page 53999-54000] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18563; Directorate Identifier 2002-NM-98-AD; Amendment 39-13783; AD 2004-18-05] RIN...

fra/pec - 102926
Rome, Italy, 09/08/2004 15:09
AVIONEWS - World Aeronautical Press Agency

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