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CLARA MOSCHINI

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Civil aviation

11,459 news found

Civil aviationFAA AD on Boeing model 747-200B and -200F series airplanes powered by Pratt & Whitney JT9D-70 series engines

Washington, Usa - To find and fix heat damage of the pylon skin and internal structure of the nacelle struts, which could result in cracking or fracture of the struts, and consequent reduced structural integrity and possible separation of the strut

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-23-AD; Amendment 39-13059; AD 2003-04-11] RIN... more

Civil aviationFAA AD on Fokker model F-28 Mark 1000, 2000, 3000, and 4000 series airplanes

Washington, Usa - To detect and correct heat damage to the fuselage skin panels caused by the leakage of hot air from one of the bleed air ducts inside the stub wing, and consequent reduced structural integrity of the engine support structure

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-334-AD; Amendment 39-13057; AD 2003-04-09] RIN... more

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

Washington, Usa - To prevent a significant latent failure in the rudder travel limiter (RTL), which could lead to a critical loss of RTL function under certain conditions, and consequent loss of controllability of the airplane or structural damage

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-93-AD; Amendment 39-13076; AD 2003-04-27] RIN... more

Civil aviationFAA AD on Bell Helicopter Textron Canada model 427 helicopters

Washington, Usa -To prevent restricted flow of hydraulic fluid to the flight control hydraulic actuators resulting in loss of hydraulic control, excessive stiffness in the flight controls, and a subsequent forced landing of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-19-AD; Amendment 39-13063; AD 2003-04-14] RIN... more

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Washington, Usa - To find and fix cracking of the support fitting assemblies of the main spoiler actuator, which could result in damage of adjacent structure such as the rear spar or upper skin panel, and consequent reduced structural integrity of plane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-353-AD; Amendment 39-13073; AD 2003-04-24] RIN... more

Civil aviationFAA AD on Eurocopter France model SA-341G and SA-342J helicopters

Washington, Usa - To prevent failure of the hoist emergency load jettison switch, resulting in an inability of the pilot to cut the rescue hoist cable in the event of cable entanglement or other emergency and subsequent loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-47-AD; Amendment 39-13062; AD 2003-04-13] RIN... more

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