It does not receive public funding
Editor in chief:
CLARA MOSCHINI

Facebook Twitter Youtube Instagram LinkedIn

Security

5,163 news found

SecurityFAA AD on Airbus Helicopters model AS-332C, AS-332L, AS-332L1, AS-332L2, EC-225LP, and SA-330J helicopters (2014-05-11)

Washington, Usa - To detect corrosion or a crack on a turnbuckle and prevent the failure of a turnbuckle, loss of control of the tail rotor and subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 47 (Tuesday, March 11, 2014)] [Rules and Regulations] [Pages 13519-13521] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on Eurocopter Deutschland GmbH (Eurocopter) model EC-135P1, EC-135P2, EC-135P2+, EC-135T1, EC-135T2, and EC-135T2+ helicopters (2014-05-01)

Washington, Usa - To detect wear in the MGB that could lead to a gear tooth rupture, failure of the MGB, loss of power to the main rotor, and subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 46 (Monday, March 10, 2014)] [Rules and Regulations] [Pages 13201-13204] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on certain 328 Support Services GmbH model 328/100 and 328/300 airplanes (2014-03-15)

Washington, Usa - To prevent incidents of inadvertent opening and possible detachment of a passenger door in-flight, resulting in damage to airframe and systems and loss of control of the airplane

[Federal Register Volume 79, Number 43 (Wednesday, March 5, 2014)] [Rules and Regulations] [Pages 12370-12373] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Bombardier, Inc. model CL-600-2B19 airplanes (2014-04-08)

Washington, Usa - To prevent burr marks on the primary wheels, and cracked rings on the primary wheel shaft, on certain HSTAs, which may lead to a disconnect of the pitch trim surface and subsequent loss of pitch control

[Federal Register Volume 79, Number 41 (Monday, March 3, 2014)] [Rules and Regulations] [Pages 11691-11693] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on Airbus Helicopters, model EC-225LP helicopters (2014-04-12)

Washington, Usa - To prevent oscillations in the main rotor that can transfer dynamic loads to the structure, the MGB, and the main servo-control inputs, which could result in subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 41 (Monday, March 3, 2014)] [Rules and Regulations] [Pages 11701-11703] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on The Boeing Company, model 737/100, 200, 200C, 300, 400, and 500 series airplanes (2014-05-02)

Washington, Usa - To detect and correct corrosion or cracking of the aft pressure bulkhead, which could result in loss of the aft pressure bulkhead web and stiffeners, and consequent rapid decompression of the airplane

[Federal Register Volume 79, Number 42 (Tuesday, March 4, 2014)] [Rules and Regulations] [Pages 12045-12049] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on Airbus Airplanes, model A-318, A-319, A-320, and A-321 series airplanes (2014-03-08)

Washington, Usa - To detect and correct latent failure of the flap down drive disconnection due to an already-failed interconnecting strut sensor, which could result in a consequent loss of control of the plane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9398-9400] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on ATR–GIE Avions de Transport Régional Airplanes, model ATR-42 and Model ATR-72 (2014-03-09)

Washington, Usa - To prevent the decrease of the fire extinguishing agent efficiency, which could delay fire extinction and allow fire propagation out of the nacelle fire protected area, resulting in damage to the airplane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9387-9389] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Airbus Helicopters, model AS-332C, AS-332L, AS-332L1, AS-332L2, and SA-330J helicopters (2014-03-02)

Washington, Usa - To prevent failure of a main servo-control upper end fitting, and subsequent failure of the flight controls and loss of control of the helicopter

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9395-9397] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Airbus Airplanes, model A-330/200 and /300 series airplanes, and A-340/200, /300, /500, and /600 (2014-03-14)

Washington, Usa - To prevent ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9382-9385] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on The Boeing Company, model MD-11 and MD-11F airplanes (2014-03-07)

Washington, Usa - To reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9392-9395] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Bombardier, Inc. model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes (2014-03-17)

Washington, Usa - To detect and correct incorrectly oriented or fractured fasteners, which could result in detachment of the flap hinge-box and the flap surface, and consequent reduced controllability of the airplane

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9389-9392] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Various Restricted Category Helicopters by Bell, model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, and UH-1P (2014-03-10)

Washington, Usa - To prevent disengagement of the cable from the barrel, failure of the T/R pitch control, and subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9385-9387] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more

SecurityFAA AD on Boeing Company, model 767 airplanes (2013-25-03)

Washington, Usa - To prevent certain failures or jams in the elevator system from causing a hardover of the elevator surface, resulting in a significant pitch upset and possible loss of control of the airplane

[Federal Register Volume 79, Number 17 (Monday, January 27, 2014)] [Rules and Regulations] [Pages 4269-4274] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on Airbus model A-340/200 and A-340/300 series airplanes (2013-26-03)

Washington, Usa - To prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane

[Federal Register Volume 78, Number 250 (Monday, December 30, 2013)] [Rules and Regulations] [Pages 79292-79295] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR... more