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CLARA MOSCHINI

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Civil aviation

11,419 news found

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

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

Washington, Usa - To prevent corrosion of the barrel nut holes of the upper spar caps and skin panel of the horizontal stabilizer, which could result in structural damage 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-06-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 and CL-600-2D24 series airplanes

Washington, Usa - To prevent failure of the lower panel of the main landing gear (MLG) door, the lower panel's departure from the airplane, and consequent damage to airplane structure, which could adversely affect the airplane's continued safe flight and

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-209-AD; Amendment... more

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

Washington, Usa - To prevent separation of the control rod outboard spherical bearing (bearing) ball from its outer race, rubbing of the body of the control rod against the tail rotor blade pitch horn clevis, failure of the control rod, and subsequent lo

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-SW-12-AD; Amendment... more

Civil aviationFAA AD on Eurocopter France model AS-332C, AS-332L, AS-332L1, and AS-332L2 helicopters

Washington, Usa - To detect disbonding between the stainless steel protective strip and the MRB skin, which could cause loss of the protective strip, an out-of-balance condition, 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. 2002-SW-58-AD; Amendment... more