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Civil aviation

11,115 news found

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To correct improper aileron assembly configuration, which could result in failure of the aileron mass balance weight

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35778-35781] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737 airplanes (2006-13-13)

Washington, Usa - To prevent failure of the airplane to pressurize and subsequent failure of the flightcrew to recognize and react to a valid cabin altitude warning horn, which could result in incapacitation of the flightcrew due to hypoxia

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35781-35783] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To prevent engine fuel starvation during maximum climb and descent caused by poor fuel tank venting with low fuel levels, which could result in a loss of engine power during critical phases of flight

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35783-35785] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/200, A-330/300, A-340/200, and A-340/300 series airplanes; and model A-340/541 and A-340/642 airplanes

Washington, Usa - To prevent anti-fretting material contamination, which could reduce the effectiveness of the fire extinguisher system to discharge fire extinguishing agents and to lower the concentration of Halon gas in the LDCC or BCRC in timely way

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35789-35792] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2 and A-300B4; A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes

Washington, Usa - To prevent cracking in the web of nose rib 7, which could result in rupture of the attachment fitting between the inner flap and flap track 2, and consequent reduced structural integrity of the flap

Airworthiness Directive Federal Register Information [Federal Register: June 21, 2006 (Volume 71, Number 119)] [Page 35507-35509] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To detect and correct cracks in the rudder end rib, which could result in failure of the rudder end rib

Airworthiness Directive Federal Register Information [Federal Register: June 21, 2006 (Volume 71, Number 119)] [Page 35502-35505] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 757 airplanes (2006-13-03)

Washington, Usa - To prevent arcing or sparking at the interface between the bulkhead fittings of the engine fuel feed tube and the front spar during a lightning strike, which could provide a possible ignition source for the fuel vapor inside the tank

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35381-35383] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 727-200 series airplanes equipped with a No. 3 cargo door (2006-13-01)

Washington, Usa - To detect and correct cracking of the forward frame and fuselage skin of the No. 3 cargo door cutout, which could result in failure of the frame and skin, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35385-35387] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model ERJ-170 airplanes

Washington, Usa - To prevent incorrect operation of the negative pressure relief valve, which could result in negative pressures that exceed the structural strength limits of the airframe and lead to reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35383-35385] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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