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FAA AD on Boeing model 757-200 and -200PF series airplanes
Washington, Usa - To prevent delamination of the leading edge slats, possible loss of pieces of the trailing edge wedge assembly during flight, reduction of the reduced maneuver and stall margins, and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: March 31, 2005 (Volume 70, Number 61)] [Page 16403-16406] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18876; Directorate Identifier 2003-NM-254-AD; Amendment 39-14032; AD 2005-07-08] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 117685
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency