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CLARA MOSCHINI

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Civil aviation

9,266 news found

Civil aviationFAA AD on Boeing model 767 series airplanes

Usa - To prevent ice accumulation on the lateral flight control cables and/or components due to water entering the wheel well of the main landing gear and freezing, which could restrict or jam control cable movement, resulting in loss of controllability

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-342-AD; Amendment... more

Civil aviationFAA AD on Dornier model 328-100 and -300 series airplanes

Usa - To prevent failure of the nose landing gear (NLG) or main landing gear (MLG) due to corroded or missing bolts, which could cause loss of connection pins, and consequent collapse of the landing gear during ground maneuvers or upon landing

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-60-AD; Amendment... more

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

Usa - To prevent failure of the bolt and bushing that attach the hinge fitting to the flap, which could result in loss of the flap and consequent reduced controllability of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-164-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 airplanes

Usa - To detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-179-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-319/131 and -132; A-320/231, -232, and -233; and A-321/131 and -231 series airplanes

Washington, Usa - To prevent separation of the engine fan cowl door from the airplane in flight, which could result in damage to the airplane and hazards to persons or property on the ground

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-411-AD; Amendment... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on Gulfstream model G-V series airplanes

Washington, Usa - To prevent separation of the balance weights of the aileron, which could result in jamming of the pilot's aileron control system, subsequent loss of aileron control and consequent reduced 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-190-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-310 series airplanes

Washington, Usa - To prevent decreased structural integrity of the two half fittings and loss of the ram air turbine (RAT) during extension, which could lead to reduced controllability of the airplane in the event of a dual engine failure, or in the even

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-179-AD; Amendment... more

Civil aviationFAA AD on Aerospatiale model ATR-42/200, -300, - 320, and -500 series airplanes; and model ATR-72 series airplanes

Washington, Usa - To ensure that the flightcrew is advised of the potential effects of Type II or IV de-icing or anti-icing fluids on the airplane's performance during takeoff, and to ensure that the flightcrew is advised of the revised performance calcu

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-306-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model EC-155B, SA-365N and N1, AS-365N2, and AS-365 N3 helicopters

Washington, Usa - To prevent failure of the hose, resulting in failure of hydraulic pressure to the brakes on the affected landing gear wheel and subsequent loss of control of the helicopter during a run-on landing

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-53-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-330 and A-340 series airplanes

Usa - To prevent desynchronization of the rudder servo-controls, which could result in high load factors on the rudder servo-controls, and consequent reduced structural integrity of the attachment fittings for the rudder servo-controls

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-187-AD; Amendment... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on General Dynamics model P4Y-2, LB-30 and model C-87A airplanes

Washington, Usa - To find and fix fatigue cracking in the lower rear cap of the wing front spar, front spar web, and lower skin of the wings, which could result in structural failure of the wings and consequent 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-164-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300B2 and B4; A-300 B4-600, A-300 B4-600R, and A-300 F4-600R; A-310; A-319; A-320; A-321; A-330; and A-340 series airplanes

Washington, Usa - To prevent failure of both structural plies of the windshield caused by overheating of the power lead wire, which could cause reduced structural integrity of the windshield assembly, and consequent loss of the windshield during flight

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-50-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 and MD- 11F airplanes

Washington, Usa - To prevent internal overheating and arcing of circuit breakers and airplane wiring due to long-term use and breakdown of internal components of the circuit breakers, which could result in smoke and fire in the flight compartment and mai

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-74-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 damage to the elevator trailing edge due to a broken or missing elevator stop bumper, which could result in jamming of the spring tab and consequent 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-109-AD; Amendment... more