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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 failure of the engine rear mount struts on the left and right engine nacelles, which could result in reduced structural integrity of the nacelle and engine support structure

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-266-AD; Amendment 39-13388; AD 2003-25-05] 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 - 56475
Rome, Italy, 12/19/2003 20:10
AVIONEWS - World Aeronautical Press Agency

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