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FAA AD on Air Tractor, Inc. models AT-400; AT- 401, AT-401B, AT-402, AT-402A, and AT-402B airplanes (2006-08-08)

Washington, Usa - To prevent fatigue cracks from occurring in the wing lower spar cap before the originally established safe life is reached which if not detected and corrected, could result in wing separation and loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2006 (Volume 71, Number 75)] [Page 19986-19994] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23646; Directorate Identifier 2006-CE-05-AD; Amendment 39-14563; AD 2006-08-08] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 139513
Rome, Italy, 04/20/2006 15:30
AVIONEWS - World Aeronautical Press Agency

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