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

Usa - To prevent contact between the lockwire pigtail of the fitting and the stiffener located on the inside surface of the fuel access covers of the wings, which could serve as a potential ignition source within the fuel tank if a cover is struck by lig

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8,2004 (Volume 69, Number 173) [Page 54213-54215] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-338-AD; Amendment 39-13788; AD 2004-18-10] RIN 2120-AA64 Airworthiness...

fra/pec - 103009
Rome, Italy, 09/09/2004 13:42
AVIONEWS - World Aeronautical Press Agency

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