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Civil aviation

11,047 news found

Civil aviationFAA AD on Airbus model A-318/100, A-319/100, A-320/200, A-321/100, and A-321/200 series airplanes; and model A-320/111 airplanes

Washington, Usa - To ensure that the flightcrew is advised of appropriate procedures to follow in the event of a fuel leak, such as isolating the fuel tanks, stopping any fuel transfers, and landing as soon as possible

Airworthiness Directive Federal Register Information [Federal Register: December 27, 2005 (Volume 70, Number 247)] [Page 76378-76381] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-1A11, CL-600-2A12, and CL-600-2B16 airplanes (2005-26-04)

Washington, Usa - To prevent migration of the lower gimbal pin of the HSTA, which could result in loss of the horizontal stabilizer and consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 21, 2005 (Volume 70, Number 244)] [Page 75725-75727] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Aviointeriors SpA (formerly ALVEN), 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: December 19, 2005 (Volume 70, Number 242)] [Page 75004-75005] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-200, -300, and -300F series airplanes (2005-25-25)

Washington, Usa - To prevent corrosion of the input override mechanism bearings of the lateral central control actuator, which, in the event of a subsequent jam in the pilot's aileron control system, could result in failure of the aileron override system

Airworthiness Directive Federal Register Information [Federal Register: December 16, 2005 (Volume 70, Number 241)] [Page 74645-74647] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 777-200 and -300 series airplanes (2005-25-24)

To prevent damage and eventual fracture of the yoke assembly, pin assembly, and attachment bolts that connect the inboard and outboard PCUs to a flaperon, which could lead to the flaperon becoming unrestrained and consequently departing from the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 16, 2005 (Volume 70, Number 241)] [Page 74641-74645] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/243, -341, -342, and -343 airplanes equipped with Rolls-Royce RB211 TRENT 700 engines (2005-25-21)

Washington, Usa - To prevent fatigue cracking of the hinges integrated into the 12 o'clock beam of the thrust reversers, which could result in separation of a thrust reverser from the airplane, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73919-73921] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model EMB-135BJ, -135ER, -135KE, -135KL, and -135LR; EMB-145, 145ER, -145MR, -145LR, -145XR, -145MP, and -145EP (2005-25-17)

Washington, Usa - To prevent fuel accumulation and subsequent flammable fuel vapors in the APU cowling, which, combined with an ignition source, could result in a fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73933-73935] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (Embraer) model ERJ-170 airplanes (2005-25-16)

Washington, Usa - To detect and correct missing attachment rods, which could result in reducing the ability of the seat to withstand a hard landing or rejected takeoff and possible injury to passengers

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73921-73923] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-200 and -300 series airplanes

To prevent failed deployment of the emergency escape slide during an emergency, which could impede an evacuation and result in injury to passengers or airplane crewmembers, or inadvertent inflation and loss of an emergency escape slide during flight

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73935-73937] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2, A-300 B4, A-310/200, A-310/300; A-300 B4-600, B4-600R, F4-600R, and model C4-605R Variant F airplanes (2005-25-19)

Washington, Usa - To prevent failure of the stiffener fittings, which could result in the reduced structural integrity of the floor and rods around FR 12A

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73930-73933] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Sabreliner model NA-265, NA-265-20, NA- 265-30, NA-265-40, NA-265-50, NA-265-60, NA-265-65, NA-265-70, and NA- 265-80 series airplanes

Washington, Usa - To detect and correct cracking or other discrepancies in these areas, which could result in structural failure of the wing

Airworthiness Directive Federal Register Information [Federal Register: December 14, 2005 (Volume 70, Number 239)] [Page 73923-73925] 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

Washington, Usa - To prevent failure of the rudder control rods, which could result in jamming of the rudder II; and possible structural failure and reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 8, 2005 (Volume 70, Number 235)] [Page 72902-72904] Header Information DEPARTMENT OF TRANSPORTATION Federal... more