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FAA AD on Boeing model 737-300, -400, and -500 series airplanes

Washington, USA - To prevent fatigue cracking of the rod ends of the actuators of the leading edge slats, which could result in failure of the rod ends, uncommanded deployment of the wing leading edge slat, and consequent reduced controllability of plane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-274-AD; Amendment 39-13029; AD 2003-03-05] RIN 2120-AA64 Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes PDF Copy (If Available): Preamble Information Regulatory Information 2003-03-05 Boeing: Amendment...

AVIONEWS - World Aeronautical Press Agency - 39664

AVIONEWS - World Aeronautical Press Agency