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Civil aviation

10,840 news found

Civil aviationFAA AD on Boeing model 747-100B SUD, -200B, - 200C, -200F, and -300 series airplanes

Usa - To detect and correct fatigue cracks in the frames and body skin at BS 420, 440, and 460 between stringers S-8 and S-12 inclusive, which could lead to severed frames, and consequent rapid decompression and loss of the structural integrity

Airworthiness Directive Federal Register Information [Federal Register: March 4, 2005 (Volume 70, Number 42)] [Page 10485-10488] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-400, -400D, and -400F series airplanes

Washington, Usa - To prevent disconnection of autoland/autopilot functions and loss of primary flaps control and flaps indication display due to disengagement of all three FCUs at the same time, which could lead to a non-normal high speed landing with th

Airworthiness Directive Federal Register Information [Federal Register: February 18, 2005 (Volume 70, Number 33)] [Page 8239-8241] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model EMB-135 and -145 series airplanes

Washington, Usa - To prevent a flash fire in the nacelle, which would result in the flightcrew shutting down the engine during flight, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: February 17, 2005 (Volume 70, Number 32)] [Page 8028-8032] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 707-100, -100B, -300, -300B, -300C, and -E3A series airplanes; 720 and 720B; 737-100, -200, -200C, -300, -400, and -500; and model 747 airplanes

Washington, Usa - To prevent arcing or sparking at the interface between the bulkhead fittings of the engine fuel feed tube and the front spar inside the fuel tank of the wings and between the overwing fuel fill ports and the airplane structure during a

Airworthiness Directive Federal Register Information [Federal Register: February 16, 2005 (Volume 70, Number 31)] [Page 7841-7845] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 airplanes and model CL-600-1A1, CL-600-2A12, and CL-600-2B16 series airplanes (2005-04-07)

Washington, Usa - To prevent possible loss of control on take-off resulting from even small amounts of frost, ice, snow, or slush on the wing leading edges or forward upper wing surfaces

Airworthiness Directive Federal Register Information [Federal Register: February 17, 2005 (Volume 70, Number 32)] [Page 8025-8028] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model AS-350B, BA, B1, B2, B3, C, D, D1, and EC-130B4 helicopters (2005-03-08)

Washington, Usa - To prevent a fuel bleed lever from separating and striking the tail rotor blade (blade), resulting in damage to or loss of a blade, and subsequent vibration and loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7381-7382] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD (Correction) on Airbus model A-300 B2 and B4 series airplanes (2005-03-14)

Washington, Usa - To prevent failure of both spring boxes of certain VLAs due to corrosion damage, which could result in loss of rudder control and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7384-7386] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model EC-155B, EC-155B1, SA-360C, SA-365C, SA-365C1, SA-365C2, SA-365N, SA-365N1, AS- 365N2, AS 365 N3, and SA-366G1 helicopters (2005-03-09)

Washington, Usa - To detect a crack in the web of the planet gear carrier, which could lead to a MGB seizure and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7382-7384] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon model DH.125, HS.125, and BH.125 series airplanes; BAe.125 series 800A (C-29A and U-125) and 800B airplanes; and Hawker 800 (Including Variant U-125A) and 800XP airplanes; equipped with TFE731 engines

Washington, Usa - To prevent a fire in the engine compartment from causing possible ignition of outgassing wire insulation on the fuselage side of the firewall, which could lead to an uncontrollable fire in the fuselage

Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7389-7390] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD (Correction) on Boeing model 767-200 and -300 series airplanes

Washington, Usa - To detect and correct fatigue cracking of the aft pressure bulkhead, which could result in rapid depressurization of the airplane and possible damage or interference with the airplane control systems that penetrate the bulkhead, and con

Airworthiness Directive Federal Register Information [Federal Register: February 11, 2005 (Volume 70, Number 28)] [Page 7174-7176] Header Information DEPARTMENT OF TRANSPORTATION Federal... more