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Civil aviation

11,448 news found

Civil aviationFAA AD on Raytheon model HS-125 series 700A and 700B airplanes; model BAe.125 series 800A, 800B, 1000A, and 1000B airplanes; and Hawker 800, 800XP, and 1000 airplanes

Washington, Usa - To prevent loss of all primary electrical power, which could result in the airplane operating only under emergency power

Airworthiness Directive Federal Register Information [Federal Register: June 16, 2006 (Volume 71, Number 116)] [Page 34790-34793] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318, A-319, A-320, and A-321 airplanes

Washington, Usa - To ensure that the flightcrew is aware of procedures to prevent the presence of a combustible air-fuel mixture in the fuel tank boost pump, which, in the event of electrical arcing could result in an explosion and loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 16, 2006 (Volume 71, Number 116)] [Page 34814-34817] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on General Machine--Diecron, Inc. Actuator Nut Assembly for the Right Main Landing Gear Installed on Certain Raytheon Aircraft Company airplanes

Washington, Usa - To prevent failure of the actuator nut assembly for the right MLG actuator, which could result in failure of the MLG

Airworthiness Directive Federal Register Information [Federal Register: June 16, 2006 (Volume 71, Number 116)] [Page 34804-34806] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-319, A-320, and A-321 airplanes

Washington, Usa - To detect and correct cracks and/or marks on the RAT carbon blades, which could result in reduced structural integrity of the carbon blade, and consequent loss of the RAT as a source of hydraulic and electrical power in an emergency

Airworthiness Directive Federal Register Information [Federal Register: June 16, 2006 (Volume 71, Number 116)] [Page 34817-34819] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, -314, and -315 airplanes; equipped with certain cockpit door installations

Washington, Usa - To prevent failure of a door attachment, which could result in uncontrolled release of the cockpit door under certain fuselage decompression conditions, and possible damage to the airplane structure

Airworthiness Directive Federal Register Information [Federal Register: June 13, 2006 (Volume 71, Number 113)] [Page 34006-34008] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira del Aeronautica S.A. (EMBRAER) model EMB-120, -120ER, -120FC, -120QC, and -120RT airplanes

Washington, Usa - To prevent a potential source of ignition near a fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 13, 2006 (Volume 71, Number 113)] [Page 34000-34003] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Revision) AD on Boeing model 767-200 and -300 series airplanes (2000-11-19R1)

Washington, Usa - To detect damaged disconnect housings in the off-wing escape slide compartments, which could result in unexpected deployment of an escape slide during maintenance, and consequent injury to maintenance personnel

Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33608-33611] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B4-600R, A-300 C4-605R Variant F, A-300 F4-600R; and model A-310/300 series airplanes

Washington, Usa - To prevent sparking of metal parts and debris from detached and damaged float valves, or a buildup of static electricity, which could result in ignition of fuel vapors and consequent fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33600-33602] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model EC-130 B4 helicopters

Washington, Usa - To detect and prevent jamming of the twist grip assembly, which, if present, could keep the engine from operating above idle speed and result in subsequent loss of control of the engine power of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33598-33600] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and installed on A-330/200 and -300, A-340/200 and -300, A-340/541 and -642 airplanes

Washington, Usa - To prevent loss of pressure in the escape slides/rafts after an emergency evacuation, which could result in inadequate buoyancy to support the raft's passenger capacity during ditching, and increase the chance for injury to passengers

Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33606-33607] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-12-12)

Washington, Usa - To detect and correct fatigue cracks that could extend and fully sever the frame, which could result in development of skin cracks that could lead to rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33595-33598] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B4; A-300B4-600; A-300C4-605R Variant F; A-310/200 series airplanes; and A-310/300 series airplanes (2006-12-05)

Washington, Usa - To detect and correct damage of the center tank fuel pumps and fuel pump canisters, which could result in a possible fuel ignition source in the center fuel tank

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2006 (Volume 71, Number 109)] [Page 32815-32818] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Dornier Luftfahrt GmbH models 228-100, 228-101, 228-200, 228-201, 228-202, and 228-212 airplanes

Washington, Usa - To detect, correct, and prevent chafed or damaged wires in the flight deck overhead panels, which could result in short-circuiting of related wiring. This condition could lead to electrical failure of affected systems and potential fire

Airworthiness Directive Federal Register Information [Federal Register: June 5, 2006 (Volume 71, Number 107)] [Page 32268-32270] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pacific Aerospace Corporation Ltd. model 750XL airplanes

Washington, Usa - To detect and correct damaged wires on the LH and RH sides of the forward end of the cockpit center console, which could lead to electrical failure of affected systems and potential fire in the cockpit

Airworthiness Directive Federal Register Information [Federal Register: June 5, 2006 (Volume 71, Number 107)] [Page 32266-32268] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model AS-350B, BA, B1, B2, B3, C, D, and D1 helicopters (2006-11-17)

Washington, Usa - To prevent restricting full lateral movement of the cyclic control during high lateral center of gravity (CG) load operations in high cross winds and during slope takeoffs or landings and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: June 2, 2006 (Volume 71, Number 106)] [Page 31918-31919] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Honeywell International Inc. T5311A, T5311B, T5313B, T5317A, T5317A-1, and T5317B series turboshaft engines and Lycoming Former Military T53-L-11B, T53-L-11D, T53-L-13B, T53-L- 13B/D, and T53-L-703 series turboshaft engines

Washington, Usa - To prevent in-flight engine failure and forced autorotation landing

Airworthiness Directive Federal Register Information [Federal Register: May 31, 2006 (Volume 71, Number 104)] [Page 30795-30796] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Gulfstream Aerospace LP model Galaxy and model Gulfstream 200 airplanes

Usa - To ensure that the flightcrew is provided with correct information to ensure a safe takeoff at certain altitudes; inadequate takeoff performance tables used in such conditions could result in reduced control of the airplane during takeoff

Airworthiness Directive Federal Register Information [Federal Register: May 31, 2006 (Volume 71, Number 104)] [Page 30796-30798] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU airplanes; and model ERJ 190-100 LR, -100 STD, and -100 IGW airplanes (2006-11-15)

Washington, Usa - To prevent the flightcrew from performing a takeoff with a partially deployed thrust reverser, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 30, 2006 (Volume 71, Number 103)] [Page 30577-30579] Header Information DEPARTMENT OF TRANSPORTATION Federal... more