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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

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
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