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FAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes (2004-05-21)

Usa - To prevent the mechanical disconnection of a flap actuator, which, if followed by failure of the flap panel's second actuator due to increased loading, could result in flap asymmetry and consequent loss of controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-258-AD; Amendment 39-13516; AD 2004-05-21] RIN 2120-AA64 Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes PDF Copy (If Available): Preamble...

fra/pec - 60009
Rome, Italy, 03/12/2004 18:17
AVIONEWS - World Aeronautical Press Agency

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