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FAA AD on Boeing 737 (2002-19-51)
Washington, Usa - To prevent operation with one failed flight control module (FCM), which could result in reduced controllability of the airplane, or with two failed FCMs, which could result in loss of control of the airplane
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-NM-248-AD; AD 2002-19-51 R1 Boeing Model 737 Series Airplanes PDF Copy (If Available): Regulatory Information 2002-19-51 R1 BOEING: Docket No. 2002-NM-248-AD. Revises AD 2002-19-51. Applicability: All Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C,...
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