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Security

5,079 news found

SecurityFAA AD on Eurocopter Deutschland GmbH (ECD) model MBB-BK-117 A-1, A-3, A-4, B-1, B-2, and C-1 helicopters (2009-11-01)

Washington, Usa - To limit the applicability to those blades fitted with lead balance weights that could detach, migrate, and cause severe vibrations leading to blade failure and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Federal Register: May 28, 2009 [Page 25402-25404] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Air Tractor, Inc. Models AT-400, AT- 400A, AT-402, AT-402A, AT-402B, AT-502, AT-502A, AT-502B, AT-503A, AT- 602, AT-802, and AT-802A airplanes (2009-11-05)

Washington, Usa - To detect and correct cracks in the engine mount, which could result in failure of the engine mount. This failure could lead to separation of the engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 22, 2009 (Volume 74, Number 98)] [Page 23938-23941] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

SecurityFAA AD on Lockheed model 382, 382B, 382E, 382F, and 382G series airplanes (2009-11-03)

Washington, Usa - To prevent cracking of the barrel nuts in the upper wing joint which could result in reduced structural integrity of the affected part and consequent detachment of the wing or engine from the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 23614-23617] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA (Correction) AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes (2009-04-06)

Washington, Usa - To detect and correct the propagation of fatigue cracks in the vicinity of oil cans on the web of the aft pressure bulkhead, which could result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 23110] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket... more

SecurityFAA AD on Boeing model 747-400 and 747-400D series airplanes (2009-10-06)

Washington, Usa - To detect and correct cracks in these chords, which could become large and cause the floor beams to become severed and result in rapid decompression or reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 91)] [Page 22424-22426] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Pratt & Whitney models PW2037, PW2037(M), and PW2040 turbofan engines (2009-10-08)

Washington, Usa - To remove nonconforming HPT 2nd stage hubs, which could result in an uncontained release of turbine blades and blade retention lugs, and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 91)] [Page 22426-22429] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14... more

SecurityFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2009-09-06)

Washington, Usa - To detect and correct fatigue cracking of the backup intercostals and upper sill web of the forward airstair doorway, which could result in a rapid loss of cabin pressure

Airworthiness Directive Federal Register Information [Federal Register: May 7, 2009 (Volume 74, Number 87)] [Page 21254-21255] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

SecurityFAA AD on Cessna Aircraft Company models LC40-550FG, LC41-550FG, and LC42-550FG airplanes (2009-09-09)

Washington, Usa - To detect and correct damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 19873-19876] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more

SecurityFAA AD on Airbus model A-318/100 and A-319/100; A-320/111; A-320/200; and A-321/100 and A-321/200 series airplanes (2009-09-05)

Washington, Usa - To prevent contact between the horizontal hinge pin and the adjacent electrical wire harness, which could result in damage to electrical wires, and consequent arcing and/or failure of associated systems

Airworthiness Directive Federal Register Information Federal Register: [Page 19876-19877] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part... more