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CLARA MOSCHINI

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Civil aviation

11,436 news found

Civil aviationFAA AD on Airbus model A-319/113 and -114 series airplanes; and model A-320/111, -211, and -212 series airplanes

Washington, Usa - To prevent jamming of a thrust reverser door during operation or inadvertent deployment of a thrust reverser door in-flight, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-61-AD; Amendment... more

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

Washington, Usa - To prevent chafing of the external ground power feeder cables against the adjacent structure, which could result in arcing and fire

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-08-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300 B4-600 series airplanes, model A-300 B4-600R series airplanes, model A-300 C4-605R variant F airplanes, and model A-300 F4-605R airplanes

Washington, Usa - To prevent short circuits between 115 Volts Alternating Current (VAC) wiring and certain fuel system electrical wire runs with subsequent overheating of the cadensicon sensor thermistor or fuel level sensor, which could be great enough

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-119-AD; Amendment... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Washington, Usa - To prevent failure of the engine rear mount struts on the left and right engine nacelles, which could result in reduced structural integrity of the nacelle and engine support structure

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-266-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300 B4-622R and A-300 F4- 622R airplanes, and model A-310/324 and -325 series airplanes

Washington, Usa - To prevent failure of the oil pressure indicator and low-oil- pressure warning in the event of an engine fire, which could result in an unannounced shutdown of the engine

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-137-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-319 and A-320 series airplanes equipped with elevator and aileron computer (ELAC) L80 standard

Washington, Usa - To prevent activation of the high angle-of-attack protection during final approach for landing, which could result in loss of the ability to flare properly during landings

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-57-AD; Amendment... more

Civil aviationFAA AD on Boeing model 777-200 and 777-300 series airplanes

Washington, Usa - To prevent leakage of hydraulic fluid into the strut aft dry bay, where high temperatures associated with the adjacent primary exhaust nozzle may ignite the fluid, resulting in an uncontrolled fire in the strut aft dry bay

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-295-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model AS-332C, C1, L, L1, AS-350B, BA, B1, B2, B3 and D, and AS-355E, F, F1, F2 and N helicopters

Washington, Usa - To prevent failure of the hoist pyrotechnic squib electrical control unit, lack of adequate current to activate the hoist pyrotechnic squib, an inability of the pilot to cut the rescue hoist cable in the event of cable entanglement or

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-15-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 airplanes

Usa - To prevent chafing damage to the wire assembly, and consequent arcing and smoke and fire in the electrical power center (EPC), and to prevent damage to the wire assembly terminal lugs and overheating of the power feeder cables on the No. 3 and No.

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-68-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes

Washington, Usa - To prevent smoke and fire in various areas of the airplane due to heat damage and/or electrical arcing of improperly installed wiring

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-150-AD; Amendment... more

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

Washington, Usa - To prevent failure of the rudder pedal arm assembly, which, under certain conditions, could result in reduced controllability of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-207-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-31 and DC- 9-32 airplanes

Washington, Usa - To prevent people on board the airplane from striking their heads on exposed metal frames in the tailcone area, which could cause injury and delay or impede their evacuation during an emergency

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-08-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, -300, -400, and -500 series airplanes

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

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-249-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model SA-365N, N1, AS-365N2, and AS-365 N3 helicopters

Washington, Usa - To prevent fuel leakage, toxic fumes inside the cabin creating a fire hazard that could lead to a fire and smoke in the cabin, and subsequent loss of control of the helicopter

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-09-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 series airplanes

Washington, Usa - To prevent the wing anti-ice (WAI) ducts from collapsing, cracking, or rupturing, consequent leakage of hot air in the under- floor pressurized area of the fuselage when the anti-ice system is turned on, insufficient heat for the anti-

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-159-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-100, -200, and -200C series airplanes

Washington, Usa - To detect and correct discrepancies in the upper and lower skins of the fuselage lap joint and circumferential joint, which could result in sudden fracture and failure of a lap joint or circumferential joint and rapid decompression of

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-150-AD; Amendment... more

Civil aviationFAA AD on Cessna model 560 airplanes

Washington, Usa - To prevent a single-point failure in the trim system from causing a runaway trim condition that the pilot may be unable to stop by using the autopilot disconnect switch, which could result in loss of control of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-225-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747-400, -400D, and -400F series airplanes

Washington, Usa - To detect and correct cracking in the yaw damper actuator portion of the upper and lower rudder power control module (PCM) main manifolds, which could result in an uncommanded left rudder hardover, consequent increased pilot workload, a

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-173-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL- 604) series airplanes

Washington, Usa - To prevent flat spots on the potentiometers of the AOA transducers due to wear, which may cause a delay in the commands for stall warning, stick shaker, and stick pusher operation

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-157-AD; Amendment... more