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

Washington, 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 Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-154-AD; Amendment 39-13458; AD 2004-03-14] RIN 2120-AA64 Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Series Airplanes PDF Copy (If Available): Preamble...

fra/pec - 58206
Rome, Italy, 02/12/2004 14:10
AVIONEWS - World Aeronautical Press Agency

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