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Civil aviation

11,114 news found

Civil aviationFAA AD on McDonnell Douglas model MD-10-10F, MD- 10-30F, MD-11F, DC-10-10F, and DC-10-30F airplanes

Washington, Usa - To identify and provide corrective action for a potentially inoperative smoke detector in the cargo compartment and ensure that the flightcrew is alerted in the event of a cargo compartment fire

Airworthiness Directive Federal Register Information [Federal Register: January 24, 2005 (Volume 70, Number 14)] [Page 3296-3299] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Garmin International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Washington, Usa - To prevent interrogating aircraft from possibly receiving inaccurate replies due to suppression from aircraft equipped with the GTX 33/33D/330/330D Mode S transponders when the pulses are below the MTL

Airworthiness Directive Federal Register Information [Federal Register: January 19, 2005 (Volume 70, Number 12)] [Page 2937-2941] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-300 series airplanes (2005-01-13)

To prevent mineral build-up on the APU and engine fire shutoff switches, which could lead to the switches failing to discharge fire suppressant to the affected fire zone and result in an uncontrolled engine or APU fire and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 13, 2005 (Volume 70, Number 9)] [Page 2339-2342] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Rolls-Royce plc RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 series turbofan engines (2005-01-15)

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: January 13, 2005 (Volume 70, Number 9)] [Page 2336-2339] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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