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Civil aviation

11,047 news found

Civil aviationFAA AD on McDonnell Douglas model DC-10-10, DC- 10-10F, DC-10-30, DC-10-30F, DC-10-40, and DC-10-40F airplanes (2006-16-12)

Washington, Usa - To reduce the potential of ignition sources inside fuel tanks in the event of a lightning strike, which could result in fuel tank explosions, and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: August 9, 2006 (Volume 71, Number 153)] [Page 45368-45370] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-200B, 747-200C, 747- 200F, 747-300, and 747SR series airplanes (2006-16-10)

Washington, Usa - To detect and correct cracking or heat damage of the skin and internal structure of the engine struts, which could result in extensive damage to the engine struts and consequent possible separation of an engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: August 9, 2006 (Volume 71, Number 153)] [Page 45363-45364] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas Model DC-9-81, DC-9-82 , DC-9-83, DC-9-87, and MD-88 airplanes

Washington, Usa - To prevent arcing on the in-tank side of the fueling valve during a lightning strike, which could result in an ignition source that could ignite fuel vapor and cause a fuel tank explosion

Airworthiness Directive Federal Register Information [Federal Register: August 3, 2006 (Volume 71, Number 149)] [Page 43961-43962] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Rolls-Royce Corporation (RRC) 250-B and 250-C series turboshaft and turboprop engines

Washington, Usa - To minimize the risk of sudden loss of engine power and uncommanded shutdown of the engine due to fuel contamination and collapse of the screen in the fuel nozzle

Airworthiness Directive Federal Register Information [Federal Register: August 3, 2006 (Volume 71, Number 149)] [Page 43964-43967] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-40, and DC-10-40F airplanes (2006-16-03)

Washington, Usa - To reduce the potential of ignition sources inside fuel tanks in the event of a severe lightning strike, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: August 3, 2006 (Volume 71, Number 149)] [Page 43962-43964] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon (Beech) model 400 and 400A series airplanes (2006-15-16)

Washington, Usa - To prevent the loss of normal electrical power, damage to some electrical components, or blown fuses during flight, and consequent unrecoverable loss of some or all essential equipment

Airworthiness Directive Federal Register Information [Federal Register: July 31, 2006 (Volume 71, Number 146)] [Page 43039-43041] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-81, DC-9-82, DC-9-83, DC-9-87, and MD-88 airplanes (2006-15-15)

Washington, Usa - To prevent shorted wires or arcing at the auxiliary hydraulic pump, which could result in loss of auxiliary hydraulic power, or a fire in the wheel well of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 31, 2006 (Volume 71, Number 146)] [Page 43035-43036] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McCauley Propeller Systems Propeller models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/ 114HCA-0, and C5JFR36C1104/L114HCA-0

Washington, Usa - To detect cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 26, 2006 (Volume 71, Number 143)] [Page 42258-42260] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model AS-365N2, AS-365 N3, EC-155B, EC-155B1, SA-365N, N1, and SA-366G1 helicopters (2006-16-15R1)

Washington, Usa - To detect a crack in an MGB base plate and prevent failure of one of the MGB attachment points to the frame, which could result in severe vibration and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: July 26, 2006 (Volume 71, Number 143)] [Page 42254-42258] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Construcciones Aeronauticas, S.A. (CASA), model C-212-CC airplanes (2006-15-11)

Washington, Usa - To prevent a hazardous quantity of smoke, flames, and/or fire extinguishing agent from the cargo compartment from entering a compartment occupied by passengers or crew

Airworthiness Directive Federal Register Information [Federal Register: July 25, 2006 (Volume 71, Number 142)] [Page 42019-42021] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 airplanes; A-310; and A-300 B4-600, B4-600R, F4-600R, and C4-605R Variant F airplanes (2006-15-09)

Washington, Usa - To prevent damage to wiring in the wing and center fuel tanks, due to failed P-clips used for retaining the wiring and pipes, which could result in a possible fuel ignition source in the fuel tanks

Airworthiness Directive Federal Register Information [Federal Register: July 25, 2006 (Volume 71, Number 142)] [Page 42026-42028] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Construcciones Aeronauticas, S.A. (CASA), model C-212-CC airplanes (2006-15-12)

Washington, Usa - To prevent a hazardous quantity of smoke, flames, and/or fire extinguishing agent from the cargo compartment from entering a compartment occupied by passengers or crew

Airworthiness Directive Federal Register Information [Federal Register: July 25, 2006 (Volume 71, Number 142)] [Page 42023-42026] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F and Airbus model A-310/200 and -300 series airplanes (2006-15-10)

Washington, Usa - To extend the operational life of the THSA to prevent a possible failure of high- time THSAs, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 25, 2006 (Volume 71, Number 142)] [Page 42021-42023] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-200, -300, and -400 series airplanes

Washington, Usa - To prevent contamination of the fueling float switch of the auxiliary fuel tank by moisture or fuel, and chafing of the float switch wiring against the float switch conduit in the fuel tank, which could present an ignition source inside

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41113-41116] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4; and A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes (2006-15-04)

Washington, Usa - To detect and correct fatigue cracks in the lower flanges of gantries 1 through 5 inclusive in the MLG bay area, which could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41109-41113] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B2-203 and A-300B4-203 airplanes; A-300B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes; and model A-310/200 and -300 series airplanes (2006-15-06)

Washington, Usa - To prevent a sudden change in pitch due to an out-of-trim condition combined with an autopilot disconnect, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41118-41121] 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 (2006-15-03)

Washington, Usa - To detect and correct cracks in the ribs of the inboard integral fuel tanks in the left and right wings, which could lead to wing failure during flight with consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 19, 2006 (Volume 71, Number 138)] [Page 40886-40888] 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 (2006-15-02)

Washington, Usa - To detect and correct increased friction in the aileron control bellcrank assemblies, which could result in failure of the aileron flight-control system

Airworthiness Directive Federal Register Information [Federal Register: July 19, 2006 (Volume 71, Number 138)] [Page 40888-40891] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To prevent a decrease in the torque limiter function, which could result in degradation and damage to the attachment bolts of the leading edge slat, loss of the slat, and consequent reduced control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 17, 2006 (Volume 71, Number 136)] [Page 40387-40389] Header Information DEPARTMENT OF TRANSPORTATION Federal... more