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AVIONEWS - World Aeronautical Press Agency

101,829 news found

Civil aviationFAA AD on Fokker model F.28 Mark 1000, 2000, 3000, and 4000 airplanes

Washington, Usa - To detect and correct improperly installed bushings, which could result in reduced tensile strength of the reinforcing strap of the wing's lower skin, and consequently a reduction of the structural capability of the wing and possible

Airworthiness Directive Federal Register Information [Federal Register: June 27, 2005 (Volume 70, Number 122)] [Page 36831-36833] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B2 and B4; A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes; and model A-310/200 and -300 series airplanes (2005-13-26)

Washington, Usa - To ensure that crewmembers are informed of the risks associated with forcibly opening passenger/crew, emergency exit, and cargo doors before an airplane is fully depressurized, which will prevent injury to crewmembers, and subsequent

Airworthiness Directive Federal Register Information [Federal Register: June 27, 2005 (Volume 70, Number 122)] [Page 36819-36821] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-10; DC-9-20; DC-9-30; DC-9-40; DC-9-50; DC-9-81, DC-9-82, DC-9-83, and DC-9-87 and model MD-88 airplanes

Washington, Usa - To prevent internal shorting, arcing, and loss of emergency battery power due to failed battery screws, which could result in loss of emergency power to electrical flight components or other emergency power systems required in the event

Airworthiness Directive Federal Register Information [Federal Register: June 27, 2005 (Volume 70, Number 122)] [Page 36824-36826] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To prevent air leakage around the temperature sensor for the aft cargo compartment, which, in the event of a fire in the aft cargo compartment, could result in an insufficient concentration of fire extinguishing agent, and consequent

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36476-36479] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model MD-90-30 airplanes

Washington, Usa - To prevent metallic fibers from the first stage filter of the servo valves inside the DACM from becoming lodged in the first stage nozzle of the servo valve, which could lead to tire failure during high speed/high energy braking and

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36479-36480] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-400, -400D, -400F; 767-200, -300, -300F; and 777-200 and -300 series airplanes (2005-13-20)

Washington, Usa - To prevent a latent open circuit that could leave the fuel spar shutoff valve in a partially open position when the engine fire switch is activated, which could result in fuel from the engine feeding an uncontrolled fire in the engine

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36474-36476] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-200, -200C, -300, - 400, -500, -600, -700, -700C, -800, and -900 series airplanes (2005-13-15)

Washington, Usa - To prevent fuel or fuel vapors from leaking into the cargo or passenger compartments and coming into contact with a possible ignition source, which could result in fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36486-36488] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model EC-155B, EC-155B1, SA-365N, SA-365N1, AS-365N2, and AS-365N3 helicopters

Washington, Usa - To prevent failure of a hose, resulting in failure of hydraulic pressure to the brakes on the affected landing gear wheel, and subsequent loss of control of the helicopter during a run-on landing

Airworthiness Directive Federal Register Information [Federal Register: June 24, 2005 (Volume 70, Number 121)] [Page 36482-36484] Header Information DEPARTMENT OF TRANSPORTATION Federal... more