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FAA AD on McDonnell Douglas model DC-9-14, DC-9- 15, and DC-9-15F airplanes; and model DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes
Washington, Usa - To prevent failure of the outboard idler hinge fitting of the left and right wing flap at station Xw=333.148 due to fatigue cracking, which could result in a deflected flap that may cause asymmetric lift and consequent reduced controlla
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Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8, 2004 (Volume 69, Number 173) [Page 54201-54204] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-345-AD; Amendment 39-13789; AD 2004-18-11] RIN 2120-AA64 Airworthiness...
fra/pec - 103006
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency