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Security

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SecurityFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2007-11-07)

Washington, Usa - To prevent electrical arcing between the wiring and the surrounding conduit, which could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank

Airworthiness Directive Federal Register Information [Federal Register: May 22, 2007 (Volume 72, Number 98)] [Page 28597-28601] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model EMB-145LR, -145XR, and -145MP airplanes; and model EMB- 135BJ and -135LR airplanes (2007-10-11)

Washington, Usa - To prevent loss of bonding protection in the interior of the fuel tanks or adjacent areas, and a consequent potential source of ignition in a fuel tank and possible fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: May 17, 2007 (Volume 72, Number 95)] [Page 27730-27732] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Boeing model 767-200 and -300 series airplanes (2007-10-03)

Washington, Usa - To prevent fire extinguishing agent from leaking out of the tube assembly in the aft cargo compartment which, in the event of a fire in the aft cargo compartment, could result in an insufficient concentration

Airworthiness Directive Federal Register Information [Page 26285-26287] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No.... more

SecurityFAA AD on McDonnell Douglas model DC-9-81, DC-9-82, DC-9-83, DC-9-87, and MD-88 airplanes (2007-10-04)

Washington, Usa - To detect and correct cracks in the upper and lower aft skin panels and rear spar upper caps, which, if not corrected, could lead to the loss of overall structural integrity of the horizontal stabilizer

Airworthiness Directive Federal Register Information [Page 25960-25962] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No.... more

SecurityFAA (Correction) AD on Cessna Aircraft Company models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R airplanes (2007-09-01)

Washington, Usa - To detect and correct interference between the ground power electrical cable, the fuel strainer cable, and the fuel line between the auxiliary electric fuel pump and the engine-driven fuel pump

Airworthiness Directive Federal Register Information [Page 21320] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27786;... more

SecurityFAA AD on Boeing model 737-800 series airplanes (2007-06-52)

Washington, Usa - To detect and correct any spoiler panel that is found in the up position with the speedbrake handle in the down position, which could result in a spoiler actuator hardover, and could cause the spoiler surface

Airworthiness Directive Federal Register Information [Page 21083-21086] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No.... more

SecurityFAA AD on Turbomeca SA Arriel 2B turboshaft engines (2005-13-25R1)

Washington, Usa - To prevent loss of control of engine fuel flow in manual control mode or mixed control mode, which can lead to engine overspeed, and in-flight engine shutdown resulting in a forced autorotation landing

Airworthiness Directive Federal Register Information [Page 19110-19112] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21624;... more

SecurityFAA AD on Cessna Aircraft Company models 172R, 172S, 182T, T182T, 206H, and T206H airplanes (2007-08-03)

Washington, Usa - To detect and correct potential loss of fuel flow, which may result in partial or complete loss of engine power and/or uncontrolled engine compartment fire due to fuel leakage forward of the firewall

Airworthiness Directive Federal Register Information [Page 18380-18383] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No.... more

SecurityFAA AD on Airbus model A-300B4-601, A-300B4-603, A-300B4-605R, A-300C4-605R Variant F, A-310/204, and A-310/304 airplanes equipped with General Electric CF6-80C2 engines (2007-07-15)

Washington, Usa - To prevent electrical arcing in the engine pylon, which could result in loss of the relevant alternating current (AC) bus bar, reduced structural integrity of the engine pylon, possible loss of control of plane

Airworthiness Directive Federal Register Information [Page 17376-17379] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No.... more