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FAA AD on Fokker model F.28 Mark 0070 and 0100 airplanes (2007-04-23)
Washington, Usa - To detect and correct fatigue cracking of the sliding member, which could result in possible separation of the MLG from the airplane and consequent reduced controllability of the airplane upon landing
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Airworthiness Directive Federal Register Information [Federal Register: February 27, 2007 (Volume 72, Number 38)] [Page 8615-8617] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25391; Directorate Identifier 2006-NM-097-AD; Amendment 39-14956; AD 2007-04-23] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 74576
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency