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FAA AD on Boeing model 757-200, -200PF, and - 200CB series airplanes (2005-01-12)
Usa - To prevent a flap skew due to insufficient secondary load path of the ballscrew of the trailing edge flaps in the event that the primary load path fails, which could result in possible loss of a flap and reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: January 10, 2005 (Volume 70, Number 6)] [Page 1655-1659] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-166-AD; Amendment 39-13936; AD 2005-01-12] RIN 2120-AA64 Airworthiness Directives; Boeing Model 757-200, -200PF, and...
fra/pec - 111717
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency