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Civil aviation

11,114 news found

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 series airplanes (2004-10-09)

Washington, Usa - To prevent overheating of the in-line splices of the APU and IDG feeder cables, which can lead to smoke, fumes, and possible fire in the flight deck and cabin

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 21, 2004 (Volume 69, Number 99)] [Page 29217-29218] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 and Avro 146-RJ series airplanes (2004-10-11)

Usa - To prevent the inability of the left-hand fire extinguisher on one or more engines to discharge, and consequent inability to control or suppress an engine fire

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 21, 2004 (Volume 69, Number 99)] [Page 29216-29217] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Garmin International Inc. GTX 330 Mode S Transponders and GTX 330D Diversity Mode S Transponders

Usa - To prevent interrogating aircraft from possibly receiving inaccurate replies due to suppression from aircraft equipped with the GTX 330/330D Mode S Transponders when the pulses are below the MTL

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 21, 2004 (Volume 69, Number 99)] [Page 29212-29215] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes equipped with certain Honeywell Start Converter Units

Usa - To prevent overheating of the electrical connector of the SCU, which could create an ignition source and possible fire in the electrical and electronics (E/E) compartment and cause damage to certain electrical wire bundles on the E2-2 shelf

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 20, 2004 (Volume 69, Number 98)] [Page 29049-29054] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 727-100 and -200; 737-100, -200, -200C, -300, -400 and -500; and 747 series airplanes (2004-10-06)

Washington, Usa - To ensure adequate electrical bonding between the penetration fittings of the hydraulic heat exchanger and the rear spars of the fuel tanks of the left and right wings

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28046-28051] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Airbus model A-300B4-600, A-300B4-600R, and A-300F4-600R (Collectively Called A-300/600), A-310, A-319, A-320, A-321, A-330, and A-340/200 and -300 series airplanes

Washington, Usa - To prevent obstruction of the air intake of the pitot probes, which could result in misleading information being provided to the flightcrew

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28044-28046] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 747-400, 747-400D, 747- 400F, 757-200, 757-200PF, 757-200CB, 767-200, 767-300, and 767-300F series airplanes (2004-10-05)

Washington, Usa - To ensure that the flightcrew is able to silence an erroneous overspeed or stall aural warning

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28051-28058] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model CL-215-6B11 (CL215T Variant), and CL-215-6B11 (CL415 Variant) series airplanes (2004-10-04)

Usa - To prevent failure of the rear engine mount struts, which could subsequently result in reduced structural integrity of the nacelle and engine support structure

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 17, 2004 (Volume 69, Number 95)] [Page 27831-27833] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dassault model Mystere-Falcon 50 series airplanes

Usa - To find and fix improper installation of the electrical wiring of the basic/optional cabin lighting, which could result in overheating of the wiring and possible smoke/fire in the cabin during an emergency situation

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 12, 2004 (Volume 69, Number 92)] [Page 26299-26301] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes

Usa - To find and fix damage and prevent subsequent failure of the rear spar fittings between the flex shaft of the flap secondary drive and the wing-to-fuselage structure, which could result in loss of the wing

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26010-26012] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes

Washington, Usa - To prevent the roll and pitch disconnect handles from being difficult to operate, which could result in an increase in pilot workload and subsequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26003-26004] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 340B series airplanes equipped with Hamilton Sundstrand propellers

Usa - To prevent erroneous tripping of the remote controlled circuit breakers (RCCB) (even though an overload condition does not exist), premature failure of the RCCBs, loss of power to the feather pump system, and consequent reduced controllability of

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26001-26003] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model DHC-7-100 series airplanes

Usa - To detect and correct fatigue cracking in the baggage door fittings and the support structure, which could result in structural failure, and consequent rapid decompression of the airplane during flight

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26025-26027] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dornier model 328-300 series airplanes

Usa - To prevent failure of certain ground spoiler support arms due to interference between the ground spoiler assemblies and the wing flaps, which could result in loss of function of affected ground spoiler assemblies and consequent reduced controllabil

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26017-26018] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes (2004-09-21)

Usa - To prevent failure of the windshield wiper assembly, which could result in loss of visibility, damage to the propeller(s) and/or engine(s), or penetration of the fuselage skin and consequent rapid depressurization of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26006-26008] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Usa - To prevent oil leakage from the engine oil coolers, consequent in-flight engine shutdown due to low oil pressure, and reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26013-26015] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 727 series airplanes (2004-09-36)

Usa - To prevent undetected cracking of the H-11 bolts or excessive wear of the cadmium-plated bolts, which would compromise the primary load path of the engine support and could result in separation of the engine from the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26015-26017] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 747-400 and 747-400D series airplanes (2004-09-33)

Usa - To prevent a chafed hole in the fire extinguishing system tube of the aft cargo compartment, which could result in a lack of fire extinguishing agent and consequent uncontained fire in the aft cargo compartment

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26012-26013] Header Information Header Information DEPARTMENT... more