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Civil aviation

11,047 news found

Civil aviationFAA AD on Dowty Aerospace Propellers Type R321/4- 82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies (2005-20-12)

Washington, Usa - To prevent propeller hub failure due to cracks in the hub, which could result in loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 13, 2005 (Volume 70, Number 197)] [Page 59647-59651] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 757-200, -200PF, and -300 series airplanes, powered by Pratt & Whitney PW2000 series engines (2005-20-41)

Washington, Usa - To prevent such failure, which, in conjunction with sparking of electrical wires, failure of seals that would allow flammable fluids to migrate to compartments with ignition sources could result in an uncontained fire

Airworthiness Directive Federal Register Information [Federal Register: October 13, 2005 (Volume 70, Number 197)] [Page 59644-59647] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 727, 727C, 727-100, and 727-100C series airplanes (2005-20-33)

Washington, Usa - To detect and correct fatigue cracking of the forward and aft edge frames of the lower lobe FCD cutout, which could result in the loss of the FCD and rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59266-59268] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-319/100; A-320/111; A-320/200, A-321/100 and -200 series airplanes (2005-20-28)

Washington, Usa - To prevent inadequate lighting and marking of the escape path, which could delay or impede the flightcrew and passengers when exiting the airplane during an emergency landing

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59256-59258] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on The Cessna Aircraft Company models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, and 441 airplanes (2005-20-25)

Washington, Usa - To prevent failure of the avionics bus circuit breaker switch, which could result in smoke and a burning smell in the cockpit

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59237-59240] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, -145, - 145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes (2005-20-37)

Washington, Usa - To prevent a broken trailing arm and consequent failure of the MLG, which could lead to loss of control and damage to the airplane during takeoff or landing

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59244-59246] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Revision) AD on BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN ASTIR, G103A TWIN II ACRO, and G103C TWIN III ACRO sailplanes

Washington, Usa - To prevent damage to the fuselage during limit load flight, which could result in reduced structural integrity

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59258-59263] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Aviointeriors SpA, series 312 box mounted seats

Washington, Usa - To prevent series 312 box mounted seats from detaching from the passenger compartment floor, which could result in injury to the occupant of the seat, and prevent evacuation of passengers in the event of an emergency

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59243-59244] 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 (2005-20-32)

Washington, Usa - To prevent disbonding of the elevator assembly, which could reduce the structural integrity of the elevator and result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59263-59266] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/301, -321, -322, - 341, and -342; A-340/200 and A-340/300 series airplanes (2005-20-20)

Washington, Usa - To prevent damage to the wheel assembly and equipment in the area adjacent to the MLG and CLG, which could result in a decrease in braking function and possible runway over-run

Airworthiness Directive Federal Register Information [Federal Register: October 6, 2005 (Volume 70, Number 193)] [Page 58298-58300] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model ATP airplanes (2005-20-22)

Washington, Usa - To detect and correct such damage, including corrosion, in the fuselage and wing structure, which could result in cracking and consequent reduced structural integrity of the fuselage and wing structure

Airworthiness Directive Federal Register Information [Federal Register: October 6, 2005 (Volume 70, Number 193)] [Page 58293-58295] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B4-620, A-310/304, A-310/324, and A-310/325 airplanes (2005-20-14)

Washington, Usa - To prevent an ignition source in the ACT, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 6, 2005 (Volume 70, Number 193)] [Page 58303-58304] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-10-10 and DC-10-10F; DC-10-15; DC-10-30 and DC- 10-30F; DC-10-40 and DC-10-40F; MD-10-10F and MD-10-30F; MD-11 and MD-11F airplanes

Washington, Usa - To prevent failure of a rudder pedal torque tube, which could result in loss of rudder control and nose wheel steering controlled by the rudder pedal, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 6, 2005 (Volume 70, Number 193)] [Page 58305-58307] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-100, -200, and -200C series airplanes (2005-20-16)

Washington, Usa - To prevent a lifted slat, which, if the airplane performs any non-normal maneuver during takeoff or landing at very high angles of attack, could lead to the loss of the slat and reduced control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 5, 2005 (Volume 70, Number 192)] [Page 58005-58007] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Honeywell Flight Management System (FMS) installed in, but Not Limited to, McDonnell Douglas model MD-11 and MD-11F, Boeing model 747-400 series airplanes, and Boeing 757 and 767 airplanes

Washington, Usa - To prevent an airplane deviating from the published approach to the runway, which could lead to premature ground contact before reaching the runway

Airworthiness Directive Federal Register Information [Federal Register: October 5, 2005 (Volume 70, Number 192)] [Page 57998-58000] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Revision) AD on Boeing model 767-200, -300, and -300F series airplanes

Washington, Usa - To detect and correct fatigue cracking or corrosion of the fail-safe straps, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: October 5, 2005 (Volume 70, Number 192)] [Page 58000-58002] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, -200B, -200F, - 200C, -100B, -300, -100B SUD, -400, -400D, and -400F; and 747SR series airplanes

Washington, Usa - To prevent cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or retraction of a trailing edge flap, and possible loss of controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 4, 2005 (Volume 70, Number 191)] [Page 57740-57746] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/301, -321, -322, - 341, and -342 airplanes; A-340/200 and A-340/300 series airplanes

Washington, Usa - To detect and correct fatigue cracking in the vertical web of the wing rear spar, which could result in reduced structural integrity of the wing

Airworthiness Directive Federal Register Information [Federal Register: October 3, 2005 (Volume 70, Number 190)] [Page 57493-57497] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Various Transport Category Airplanes Manufactured by McDonnell Douglas (2003-17-07 R1)

Washington, Usa - To prevent failure of the fire extinguishers to fire discharge cartridges, which could result in the inability to put out a fire in an engine or in the APU

Airworthiness Directive Federal Register Information [Federal Register: October 3, 2005 (Volume 70, Number 190)] [Page 57491-57493] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Airbus model A-340/200 and -300 series airplanes

Washington, Usa - To prevent this miscalculation, which, if combined with high takeoff weight, too-short runway length, and high altitude and temperature of the airport, could result in inability of the flightcrew to abort the takeoff in a safe manner

Airworthiness Directive Federal Register Information [Federal Register: September 30, 2005 (Volume 70, Number 189)] [Page 57125] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

To detect and correct cracked or fractured thrust links that could lead to the loss of the load path for the rear engine mount bulkhead and damage to other primary engine mount structure, which could result in the in-flight separation of the engine

Airworthiness Directive Federal Register Information [Federal Register: September 30, 2005 (Volume 70, Number 189)] [Page 57124-57125] Header Information DEPARTMENT OF TRANSPORTATION Federal... more