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FAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes

Usa - To find and fix damage and prevent subsequent failure of the rear spar fittings between the flex shaft of the flap secondary drive and the wing-to-fuselage structure, which could result in loss of the wing

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26010-26012] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-38-AD; Amendment 39-13623; AD 2004-03-14 R1] RIN 2120-AA64 Airworthiness...

fra/pec - 63311
Rome, Italy, 05/14/2004 14:21
AVIONEWS - World Aeronautical Press Agency

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