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FAA AD on BAE Systems (Operations) Limited model ATP airplanes (2006-18-09)

Washington, Usa - To detect and correct fatigue cracking of certain structural elements, which could result in reduced structural integrity of the airplane and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 6, 2006 (Volume 71, Number 172)] [Page 52418-52421] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25721; Directorate Identifier 2006-NM-132-AD; Amendment 39-14748; AD 2006-18-09] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 148656
Rome, Italy, 09/11/2006 18:22
AVIONEWS - World Aeronautical Press Agency

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