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FAA AD on Bombardier model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes (2007-12-01)

Washington, Usa - To prevent loss in shock absorption during touchdown and failure of the shock strut housing, which could result in a subsequent loss of directional control

Airworthiness Directive Federal Register Information [Federal Register: June 5, 2007 (Volume 72, Number 107)] [Page 30959-30961] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27713; Directorate Identifier 2006-NM-240-AD; Amendment 39-15079; AD 2007-12-01] RIN 2120-AA64 Airworthiness Directives; Bombardier...

fra/pec - 1074956
Rome, Italy, 06/06/2007 13:30
AVIONEWS - World Aeronautical Press Agency

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