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FAA AD on Boeing model 707-300B, -300C, and -400 series airplanes

Washington, Usa - To detect and correct fatigue cracking of the hinge fitting assembly of the inboard leading edge slats

Airworthiness Directive Federal Register Information [Federal Register: July 12, 2005 (Volume 70, Number 132)] [Page 39912-39914] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20725; Directorate Identifier 2003-NM-250-AD; Amendment 39-14183; AD 2005-14-06] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 123688
Rome, Italy, 07/13/2005 12:04
AVIONEWS - World Aeronautical Press Agency

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