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

Washington, Usa - To prevent incorrect altitude information transmitted by the Mode S transponder and simultaneous loss of the Traffic Alert and Collision Avoidance System (TCAS), and increasing the possibility of an air traffic conflict

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-391-AD; Amendment 39-13241; AD 2003-14-22 ] 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 - 48095
Rome, Italy, 07/21/2003 14:35
AVIONEWS - World Aeronautical Press Agency

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