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Civil aviation

11,229 news found

Civil aviationFAA AD on Airbus model A-330/322, -341, and -342 airplanes; and Airbus model A-340/200 and -300 series airplanes (2005-19-22)

Washington, Usa - To prevent fatigue cracks in the duct structure of the ram air outlet, which could lead to hot air damage and consequent loss of function of the hydraulics systems

Airworthiness Directive Federal Register Information [Federal Register: September 22, 2005 (Volume 70, Number 183)] [Page 55529-55531] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318/100, A-319/100, A-320/200, A-321/100, and A-321/200 series airplanes; and model A-320/111 airplanes (2005-19-14)

Washington, Usa - To prevent electrical arcing in the center fuel tank due to inadequate bonding, which could result in an explosion of the center fuel tank and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 21, 2005 (Volume 70, Number 182)] [Page 55228-55230] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/301, -321, -322, - 341, and -342 airplanes; and model A-340/200 and A-340/300 series airplanes (2005-19-12)

Washington, Usa - To detect and correct such cracking, which could propagate and result in reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: September 21, 2005 (Volume 70, Number 182)] [Page 55236-55239] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-300, -400, -500, -600, -700, -700C, -800 and -900 series airplanes

Washington, Usa - To prevent the FMC from displaying the incorrect actual navigation performance value to the flightcrew, which could prevent adequate alerting of a potential navigation error

Airworthiness Directive Federal Register Information [Federal Register: September 21, 2005 (Volume 70, Number 182)] [Page 55239-55242] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Lycoming Engines AEIO-360, IO-360, O-360, LIO-360, LO-360, AEIO-540, IO-540, O-540, and TIO-540 Series Reciprocating Engines

Washington, Usa - To prevent failure of the crankshaft, which could result in total engine power loss, in-flight engine failure, and possible loss of the aircraft

Airworthiness Directive Federal Register Information [Federal Register: September 16, 2005 (Volume 70, Number 179)] [Page 54618-54622] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747 airplanes

Washington, Usa - To prevent the loss of a DSB or underwing midspar fitting load path, which could result in the transfer of loads and motion to other areas of a strut, and possible separation of a strut and engine from the airplane during flight

Airworthiness Directive Federal Register Information [Federal Register: September 16, 2005 (Volume 70, Number 179)] [Page 54612-54616] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-14, DC-9- 15, and DC-9-15F airplanes; DC-9-20, DC-9- 30, DC-9-40, and DC-9-50 series airplanes

Washington, Usa - To detect and correct fatigue cracks in the shock strut cylinder of the MLG, which could result in a collapsed MLG during takeoff or landing, and possible reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 16, 2005 (Volume 70, Number 179)] [Page 54616-54618] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To detect and correct cracked or fractured thrust links that could lead to the loss of the load path for the rear engine mount bulkhead and damage to other primary engine mount structure, which could result in the in-flight separation

Airworthiness Directive Federal Register Information [Federal Register: September 15, 2005 (Volume 70, Number 178)] [Page 54474-54477] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes (2005-18-23)

Washington, Usa - To prevent corrosion and subsequent moisture ingress into the electrical connectors, which could result in an electrical short and consequent incorrect functioning of critical airplane systems essential to safe flight and landing plane

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2005 (Volume 70, Number 177)] [Page 54253-54258] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-340/200 and -300 series airplanes

Washington, Usa - To prevent this miscalculation, which, if combined with high takeoff weight, too-short runway length, and high altitude and temperature of the airport, could result in inability of the flightcrew to abort the takeoff in a safe manner

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2005 (Volume 70, Number 177)] [Page 54251-54253] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Aerospatiale model ATR-42/500 airplanes

Washington, Usa - To prevent discrepancies between the elevator trim tab control rod and the forward edge of the lower skin of the elevator, which could result in reduced control of the elevator and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2005 (Volume 70, Number 177)] [Page 54249-54251] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (EMBRAER) model ERJ-170 airplanes (2005-19-01)

Washington, Usa - To prevent cracking of the hydraulic pressure pipes, which could result in failure of hydraulic system 1 or 2 or both, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2005 (Volume 70, Number 177)] [Page 54247-54248] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (EMBRAER) model ERJ-170 airplanes (2005-19-01)

Washington, Usa - To prevent cracking of the hydraulic pressure pipes, which could result in failure of hydraulic system 1 or 2 or both, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2005 (Volume 70, Number 177)] [Page 54247-54248] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company models 1900, 1900C, 1900C (C-12J), and 1900D airplanes (2005-18-21)

Washington, Usa - To detect and correct any looseness in the elevator hinge support attachments, which could result in binding of the elevator control system. This elevator binding could lead to loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 13, 2005 (Volume 70, Number 176)] [Page 53910-53912] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company model 390 Premier 1 airplanes (2005-18-22)

Washington, Usa - To detect and correct chafing conditions in the engine installation, which could result in leaking flammable fluids near an ignition source. This failure could lead to fire damage or loss of airplane control

Airworthiness Directive Federal Register Information [Federal Register: September 13, 2005 (Volume 70, Number 176)] [Page 53912-53914] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Revision) AD on Rolls-Royce plc RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 series turbofan engines

Washington, Usa - To prevent multiple LPC fan blade failures due to cracks, which could result in uncontained engine failure and possible damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 12, 2005 (Volume 70, Number 175)] [Page 53725-53728] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Fokker model F27 Mark 200, 400, 500, and 600 airplanes

Washington, Usa - To ensure that the rotary knobs are not inadvertently moved to the shut position, which could result in fuel starvation to both engines and consequent inability to maintain controlled flight and landing

Airworthiness Directive Federal Register Information [Federal Register: September 9, 2005 (Volume 70, Number 174)] [Page 53556-53558] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Goodrich De-icing and Specialty Systems "FASTprop" Propeller De-icers (2005-18-20)

Washington, Usa - To prevent Goodrich "FASTprop" propeller de-icers from detaching from the propeller blade, resulting in damage to the airplane, and possible injury to passengers and crewmembers

Airworthiness Directive Federal Register Information [Federal Register: September 9, 2005 (Volume 70, Number 174)] [Page 53550-53554] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 777 airplanes (2005-18-51)

Washington, Usa - To prevent the OPS from using data from faulted (failed) sensors, which could result in anomalies of the fly-by-wire primary flight control, autopilot, auto-throttle, pilot display, and auto-brake systems

Airworthiness Directive Federal Register Information [Federal Register: September 9, 2005 (Volume 70, Number 174)] [Page 53547-53550] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Avions Marcel Dassault-Breguet model Falcon 10 airplanes

Washington, Usa - To prevent collapse of the flexible hoses in the slat anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 9, 2005 (Volume 70, Number 174)] [Page 53540-53543] Header Information DEPARTMENT OF TRANSPORTATION Federal... more