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FAA AD on Bombardier model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Usa - To prevent reduced aerodynamic smoothness of the wing leading edge de-icer boots and possible reduced stall margin, which could result in a significant increase in stall speeds, leading to a possible stall prior to activation of the stall warning

Airworthiness Directive Federal Register Information [Federal Register: September 29, 2004 (Volume 69, Number 188)] [Page 58043-58047] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-126-AD; Amendment 39-13808; AD 2004-20-03] RIN 2120-AA64 Airworthiness Directives; Bombardier Model DHC-8-101,...

fra/pec - 104323
Rome, Italy, 09/30/2004 14:09
AVIONEWS - World Aeronautical Press Agency

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