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SecurityFAA (Revision) AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2008-13-12R1)

Washington, Usa - To detect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap joint

Airworthiness Directive Federal Register Information Federal Register: [Page 67383-67385] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more