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FAA AD on Boeing model 727, 727C, 727-100, 727- 100C, 727-200, and 727-200F series airplanes (2005-14-07)
Washington, Usa - To detect and correct fatigue cracking of the attach fittings of the foreflap carriage of the wings, which could result in partial or complete loss of the foreflap and consequent loss of controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: July 11, 2005 (Volume 70, Number 131)] [Page 39647-39651] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-19679; Directorate Identifier 2003-NM-132-AD; Amendment 39-14184; AD 2005-14-07] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 123648
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency