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CLARA MOSCHINI

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Civil aviation

11,436 news found

Civil aviationFAA AD on Airbus model A-330223, -321, -322, and -323 series airplanes equipped with Pratt & Whitney model PW4164, PW4168, or PW4168A engines

Washington, USA - To prevent reduced structural integrity of the primary structure of the engine pylons, and uncommanded deployment of the thrust reversers, which could result in reduced controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-102-AD; Amendment 39-13040; AD 2003-03-16] RIN... more

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

Washington, USA - To prevent reduced structural integrity of the screws in the aileron, elevator, and rudder trim tabs and the rudder spring tab, due to countersinks that were not manufactured correctly, which could result in reduced controllability plan

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-140-AD; Amendment 39-13042; AD 2003-03-17] RIN... more

Civil aviationFAA AD on Boeing model 737-600, -700, -700C, - 800, and -900 series airplanes

Washington, USA - To prevent severe vibration of the elevator and elevator tab assembly, which could result in severe damage to the horizontal stabilizer followed by possible loss of the elevator tab and consequent loss of controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-240-AD; Amendment 39-13047; AD 2003-03-22] RIN... more

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

Washington, USA - To detect and correct discrepancies in the fuel distribution system, which could cause the center tank to overfill and fuel to leak from the center tank vent system or to 2 become inaccessible, and could result in engine fuel starvation

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-20-AD; Amendment 39-13041; AD 2003-02-51] RIN... more

Civil aviationFAA AD on Hartzell Propeller Inc. propellers installed on Sky International Inc. S- 2S and S-2B airplanes

Washington, USA - To prevent fatigue failure of Hartzell propeller hubs P/N D- 6522-1 or D-2201-16 and blades P/N FC8477A-4 which may result in loss of airplane control

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-48-AD; Amendment 39-13045; AD 2003-03-20] RIN... more

Civil aviationFAA AD on McDonnell Douglas model MD-90 30 airplanes

To prevent failure of a remote control circuit breaker to trip during an overload condition due to a defective braze joint in the RCCB latch assembly, which could result in overheating of the RCCB load wire, and consequent smoke and possible fire in the

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-172-AD; Amendment 39-13033; AD 2003-03-09] RIN... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-10, DC-9- 20, DC-9-30, DC-9-40, and DC-9-50 series airplanes

Washington, USA - To find and fix contamination of certain electrical connectors and prevent future contamination of these connectors, which could cause electrical arcing and result in a fire on the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-277-AD; Amendment 39-13032; AD 2003-03-08] RIN... more

Civil aviationFAA AD on Bae Systems Limited model BAe 146 and Avro 146-RJ series airplanes

Washington, USA - To prevent failure of the engine fire detection and suppression systems to operate properly in the event of a fire, which could result in an undetected and uncontrollable fire in an engine

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-48-AD; Amendment 39-13034; AD 2003-03-10] RIN... more

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

To prevent corrosion of the emergency actuator mechanism, which could cause failure of the emergency actuator striker mechanism on the passenger or emergency doors, and lead to difficulty in opening the passenger or emergency doors during emergency

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 96-NM-179-AD; Amendment 39-13028; AD 2003-03-04] RIN... more

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

Washington, USA - To prevent fatigue cracking of the rod ends of the actuators of the leading edge slats, which could result in failure of the rod ends, uncommanded deployment of the wing leading edge slat, and consequent reduced controllability of plane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-274-AD; Amendment 39-13029; AD 2003-03-05] RIN... more

Civil aviationFAA AD on Eurocopter France model AS-350B, AS-350BA, AS-350B1, AS-350B2, AS-350B3, AS-350C, AS-350D, AS-350D1, AS-355E, AS-355F, AS-355F1, AS-355F2, and AS-355N helicopters

USA - To prevent the roller from coming out of the middle rail when operating the door, which could lead to the sliding door separating from the helicopter during flight, damage to critical flight components, and subsequent loss of control of the copter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-41-AD; Amendment 39-13021; AD 2003-02-05] RIN... more