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FAA AD on Bombardier model DHC-7-100 series airplanes

Usa - To detect and correct fatigue cracking in the baggage door fittings and the support structure, which could result in structural failure, and consequent rapid decompression of the airplane during flight

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26025-26027] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-153-AD; Amendment 39-13612; AD 2000-02-07 R1] RIN 2120-AA64 Airworthiness...

fra/pec - 63185
Rome, Italy, 05/12/2004 17:48
AVIONEWS - World Aeronautical Press Agency

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