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FAA AD on Brantly International, Inc. model B-2, B-2A, and B-2B helicopters
Washington, Usa - To prevent fatigue cracking of a shaft, failure of a shaft, and subsequent loss of control of the helicopter
Airworthiness Directive Federal Register Information [Federal Register: April 17, 2006 (Volume 71, Number 73)] [Page 19624-19626] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24447; Directorate Identifier 2005-SW-35-AD; Amendment 39-14562; AD 2006-08-07] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 139381
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency