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Security

4,994 news found

SecurityFAA AD on The Boeing Company model 757 airplanes (2014-05-20)

Washington, Usa - To prevent fracture of the rudder pedal pushrod connecting bolts during pedal use, which could result in large involuntary inputs to the rudder and nose-wheel steering and an asymmetric application of braking

[Federal Register Volume 79, Number 52 (Tuesday, March 18, 2014)] [Rules and Regulations] [Pages 14987-14992] 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 (2014-05-12)

Washington, Usa - To detect and correct cracked, corroded, or fractured carriage spindles, which could lead to severe flap asymmetry, and could result in reduced control or loss of controllability of the airplane

[Federal Register Volume 79, Number 52 (Tuesday, March 18, 2014)] [Rules and Regulations] [Pages 14977-14982] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on Bombardier, Inc. model DHC-8-400 series airplanes (2014-05-18)

Washington, Usa - To prevent incorrectly installed scrapers, which could hinder the operation of the MLG AES, and result in failure of the MLG AES on one side, and consequent unsafe asymmetrical landing configuration

[Federal Register Volume 79, Number 52 (Tuesday, March 18, 2014)] [Rules and Regulations] [Pages 14997-14999] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

SecurityFAA AD on The Boeing Company model 717/200 airplanes (2014-05-22)

Washington, Usa - To detect and correct cracking, which could result in a severed frame and might increase the loading of adjacent frames, resulting in damage to the adjacent structure and consequent loss of structural integrity

[Federal Register Volume 79, Number 47 (Tuesday, March 11, 2014)] [Rules and Regulations] [Pages 13530-13533] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc... more

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