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FAA AD on Gulfstream Aerospace Corporation, model G-1159, G-1159A, and G-1159B airplanes (2012-11-06)
Washington, Usa - To detect and correct excessive gaps in the wing-to-fuselage attachment fittings, which could result in reduced structural integrity at the wing-to-fuselage attachment and separation of the wing from the plane
[Federal Register Volume 77, Number 103] [Rules and Regulations] [Pages 31483-31486] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2012-13034] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2012-0494; Directorate Identifier 2012-NM-088-AD; Amendment 39-17069; AD 2012-11-06] RIN 2120-AA64 Airworthiness...
fra/pec - 1141492
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency