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FAA AD on Fokker model F-28 Mark 0070 and 0100 airplanes

Washington, Usa - To detect and correct corrosion of the wing rear spar lower girder, which could result in reduced structural integrity of the wing rear spar

Airworthiness Directive Federal Register Information [Federal Register: August 25, 2006 (Volume 71, Number 165)] [Page 50333-50335] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24959; Directorate Identifier 2005-NM-258-AD; Amendment 39-14737; AD 2006-17-16] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 147782
Rome, Italy, 08/29/2006 18:06
AVIONEWS - World Aeronautical Press Agency

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