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Civil aviation

11,115 news found

Civil aviationFAA (Revision) AD on Gulfstream model GIV-X and GV-SP series airplanes

Washington, Usa - To ensure that the flightcrew is advised of the appropriate procedures to follow in the event that the cockpit displays go blank or malfunction, which could result in a possible loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 13, 2006 (Volume 71, Number 71)] [Page 19114-19117] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model SA-360C, SA- 365C, SA-365C1, and SA-365C2 helicopters

Washington, Usa - To detect a crack in a 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: April 13, 2006 (Volume 71, Number 71)] [Page 19110-19114] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 757-200 and -300 series airplanes (2006-07-24)

Washington, Usa - To prevent intermittent indications in the flight deck, incorrect circuitry operation in the panels, and airplane system malfunctions that may adversely affect the alternate flaps, alternate gear extension, and fire extinguishing

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18197-18199] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 757 airplanes powered by Pratt & Whitney engines (2006-07-21)

Washington, Usa - To detect and correct cracking in the midspar fittings of the nacelle struts, consequent reduced structural integrity of the struts, and possible separation of an engine and strut from the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18207-18210] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 and model Avro 146-RJ airplanes

Washington, Usa - To prevent deformation of the cable duct structure in the event of a rapid decompression, which could result in restriction of the primary flight controls and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18199-18201] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43; DC-8F-54, DC-8F-55; DC-8-50, -60, - 60F, -70, and -70F and other airplanes

Washington, Usa - To prevent failure of the rudder pedal bracket assembly, which could result in the loss of rudder and braking control at either the captain’s or first officer’s position

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18201-18205] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200F, 747-300, 747-400, 747-400D, 747SP, 747SR, 767-200, 767-300, 777-200, 777-300, and 777-300ER series airplanes (2005-05-20)

Washington, Usa - To prevent failure of the equipment, which could jeopardize flight safety

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18210-18213] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model DHC-8-400 series airplanes

Washington, Usa - To prevent corrosion or perforation of domed anchor nuts, which could result in arcing and ignition of fuel vapor in the center wing fuel tank during a lightning strike and consequent explosion of the fuel tank

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2006 (Volume 71, Number 67)] [Page 17694-17696] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To detect and correct corrosion in the torque tubes of the elevators, which could lead to an unbalanced elevator and result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 7, 2006 (Volume 71, Number 67)] [Page 17698-17699] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on BURKHART GROB LUFT-UND-RAUMFAHRT GmbH & Co. KG, model G 103 C Twin III SL sailplanes

Washington, Usa - To prevent loss of the sailplane propeller caused by increased play in the current design propeller bearing and upper pulley wheel. This could result in loss of control of the sailplane

Airworthiness Directive Federal Register Information [Federal Register: April 10, 2006 (Volume 71, Number 68)] [Page 17983-17985] 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, and DC-9-50 series airplanes (2006-07-08)

Washington, Usa - To detect and correct stress corrosion cracking of the main fuselage frame, which could result in extensive damage to adjacent structure and reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16201-16203] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318/100 and A-319/100; A-320/111; and A-320/200, A-321/100, A-321/200 (2006-07-09)

Washington, Usa - To ensure the integrity of the THSA's primary load path, which if failed, could result in an eventual failure of the THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16203-16206] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B4-600, B4-600R, and F4-600R series airplanes, and model C4-605R Variant F airplanes (2006-07-07)

Washington, Usa - To prevent crack formation in the sealing angles and lead to subsequent crack formation in the bottom skin of the wing, and resultant reduced structural integrity of the center spar section of the wing

Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16206-16208] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Cirrus Design Corporation models SR-20 and SR-22 airplanes

Washington, Usa - To detect, correct, and prevent damage to the fuel line and wire bundles, which could result in fuel leaks. This failure could lead to unsafe fuel vapor within the cockpit and possible fire

Airworthiness Directive Federal Register Information [Federal Register: March 30, 2006 (Volume 71, Number 61)] [Page 16027-16029] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-319/131, -132, and -133; A-320/232 and -233; and A-321/131, -231, and -232 airplanes (2006-07-05)

Washington, Usa - To prevent structural failure of the secondary load path of the forward engine mount, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: March 30, 2006 (Volume 71, Number 61)] [Page 16025-16027] Header Information DEPARTMENT OF TRANSPORTATION Federal... more