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FAA AD on Bombardier model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes
Washington, Usa - To detect and correct fatigue cracking of the longitudinal skin joints in the fuselage pressure shell, which could affect the structural integrity of the airplane, and result in loss of cabin pressurization during flight
Airworthiness Directive Federal Register Information [Federal Register: July 5, 2005 (Volume 70, Number 127)] [Page 38575-38578] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20852; Directorate Identifier 2004-NM-240-AD; Amendment 39-14175; AD 2005-13-38] RIN 2120-AA64 Airworthiness Directives; Bombardier...
fra/pec - 123313
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency