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FAA (Correction) AD on Rockwell International models AT-6, AT-6A, AT- 6B, AT-6C, AT-6D, AT-6F, BC-1A, SNJ-7, and T-6G airplanes; and Autair Ltd. model Harvard airplanes
Washington, Usa - To detect and correct any fatigue crack in the inboard and outboard, upper and lower wing attach angles (except for the nose angles) of either wing, which could result in failure of the wing
Airworthiness Directive Federal Register Information [Federal Register: July 11, 2005 (Volume 70, Number 131)] [Page 39651-39652] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21463; Directorate Identifier 2005-CE-30-AD; Amendment 39-14144; AD 2005-12-51] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 123650
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency