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Civil aviation

10,840 news found

Civil aviationFAA AD on Boeing model 757-200, -200PF, and - 200CB series airplanes (2005-01-12)

Usa - To prevent a flap skew due to insufficient secondary load path of the ballscrew of the trailing edge flaps in the event that the primary load path fails, which could result in possible loss of a flap and reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 10, 2005 (Volume 70, Number 6)] [Page 1655-1659] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, -200B, -200F, -200C, -100B, -300, -100B SUD, -400, -400D, -400F, and 747SR series airplanes (2005-01-09)

Washington, Usa - To find and fix discrepancies of the frame web and inner chords, which could result in cracking, subsequent severing of the frame, and consequent rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 7, 2005 (Volume 70, Number 5)] [Page 1340-1341] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-310 series airplanes; and model A-300 B4-600, B4-600R, and F4-600R series airplanes, and model C4 605R Variant F airplanes (2005-01-08)

Washington, Usa - To prevent possible short circuits in the wire looms supplying the fuel pump systems and the pitot probe heating system, which could lead to a possible loss of function of flight-critical systems and reduced controllability of the plane

Airworthiness Directive Federal Register Information [Federal Register: January 7, 2005 (Volume 70, Number 5)] [Page 1338-1340] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-310 series airplanes (2005-01-06)

Washington, Usa - To prevent chafing damage to wiring 2M and 2S, which could result in a short circuit and consequently introduce an electrical current into the wiring of the FQIS and create an ignition source in the fuel tank

Airworthiness Directive Federal Register Information [Federal Register: January 7, 2005 (Volume 70, Number 5)] [Page 1335-1336] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-300 and 767-300F Series Airplanes Equipped With General Electric or Pratt & Whitney Engines

Washington, Usa - To prevent undetected loss of the diagonal brace fuse pins of the wings and consequent increased loads in other wing-to-strut joints, which could result in separation of the struts and engines from the wings

Airworthiness Directive Federal Register Information [Federal Register: January 6, 2005 (Volume 70, Number 4)] [Page 1178-1180] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Gulfstream Aerospace LP model Gulfstream 100 Airplanes; and model Astra SPX and 1125 Westwind Astra series airplanes

Washington, Usa - To prevent a false "Ground" position signal, which could result in deployment of the ground airbrakes and reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 6, 2005 (Volume 70, Number 4)] [Page 1180-1182] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318, A-319, A-320, and A-321 series airplanes (2004-26-07)

Washington, Usa - To prevent interference between the inflation hose and slide fabric and rupture of the inflation hose, which could result in incomplete inflation of the emergency escape slides and consequent unavailability of those slides during an eme

Airworthiness Directive Federal Register Information [Federal Register: January 6, 2005 (Volume 70, Number 4)] [Page 1176-1178] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To detect and correct cracking in the midspar assembly, which could result in the loss of the midspar assembly load path, and could, combined with the loss of the nacelle station 180 bulkhead load path, lead to the separation of the eng

Airworthiness Directive Federal Register Information [Federal Register: January 5, 2005 (Volume 70, Number 3)] [Page 679-680] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (Embraer) model EMB-135 and EMB-145 series airplanes

Washington, Usa - To prevent separation of the wheels from the nose landing gear due to the failure of the outer wheel bearings, and consequent loss of control of the airplane during takeoff and landing

Airworthiness Directive Federal Register Information [Federal Register: January 5, 2005 (Volume 70, Number 3)] [Page 690-691] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-215-6B11 (CL215T Variant) and CL-215-6B11 (CL415 Variant) series airplanes

Washington, Usa - To prevent fracturing of the pump body, which could result in loss of engine oil, and consequent inability to maintain engine oil pressure and to feather the propeller

Airworthiness Directive Federal Register Information [Federal Register: January 5, 2005 (Volume 70, Number 3)] [Page 684-685] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model ERJ-170 series airplanes

Washington, Usa - To prevent temporary or possible sustained loss of all modular avionics units (MAU), which triggers a cascade of failures in systems dependent on MAUs functionalities

Airworthiness Directive Federal Register Information [Federal Register: December 30, 2004 (Volume 69, Number 250)] [Page 78300-78303] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747 series airplanes

Washington, Usa - To detect and correct fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 23, 2004 (Volume 69, Number 246)] [Page 76839-76841] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (Embraer) model EMB-135 and -145 series airplanes

Washington, Usa - To prevent the temporary loss of the pitch trim command, which could result in reduced controllability of the airplane and consequent injury to the flightcrew and passengers

Airworthiness Directive Federal Register Information [Federal Register: December 22, 2004 (Volume 69, Number 245)] [Page 76605-76610] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on GE Aircraft Engines (GE) CF34-3A, CF34- 3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1 Series Turbofan Engines

Washington, Usa - To prevent LCF cracks and failure of the HPC forward spool, which could result in an uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 22, 2004 (Volume 69, Number 245)] [Page 76610-76611] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) series airplanes

Washington, Usa - To prevent a delay in the stall computer commands for stall warning, stick shaker, and stick pusher operation, due to premature wear of the potentiometers of the AOA transducers, which may cause the airplane to enter a stall condition,

Airworthiness Directive Federal Register Information [Federal Register: December 20, 2004 (Volume 69, Number 243)] [Page 75830-75833] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company Beech models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) airplanes

Washington, Usa - To detect and correct cracking in the wing structure of the affected airplanes, which could result in the wing separating from the airplane with consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 20, 2004 (Volume 69, Number 243)] [Page 75833-75835] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationNorth Korea: "We will strengthen our nuclear deterrent if the USA do not change their policy on Pyongyang"

Pyongyang, North Korea - The defensive shield, Japan's fears and the diplomatic difficulties are among the causes of the Communist regime's hostility

North Korea tightened its policy regarding the criticism addressed by the United States to its nuclear programme. The development of the American defensive shield, the cooperation with Japan which proves... more

Civil aviationFAA AD (Correction) on Cessna Aircraft Company 120, 140, 140A, 150, F-150, 170, 172, F-172, FR-172, P-172D, 175, 177, 180, 182, 185, A-185E, 190, 195, 206, P-206, U-206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 series airplanes (2004-19-01)

Washington, Usa - To prevent slippage of the pilot/co-pilot shoulder harness, which could result in failure of the shoulder harness to maintain proper belt length adjustment and tension

Airworthiness Directive Federal Register Information [Federal Register: December 16, 2004 (Volume 69, Number 241)] [Page 75236] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company, model 390, Premier 1 airplanes (2004-25-15)

Washington, Usa - To prevent damage to the wire harnesses, which could result in loss of pressurization, loss of transponder responses to interrogations, and failure of other systems utilizing air/ground status signals

Airworthiness Directive Federal Register Information [Federal Register: December 16, 2004 (Volume 69, Number 241)] [Page 75223-75225] Header Information DEPARTMENT OF TRANSPORTATION Federal... more