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CLARA MOSCHINI

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Civil aviation

11,459 news found

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

Civil aviationFAA Emergency 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 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; AD 2003-02-51 Bombardier Model CL-600-2C10... more

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

USA - To prevent false smoke warnings from the smoke detectors in the cargo compartment, which prompt the flightcrew to discharge fire extinguisher bottles, leaving those bottles depleted in the event of an actual fire, or which create uncertainty as to

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-250-AD; Amendment 39-13013; AD 2003-01-02] RIN... more

Civil aviationFAA AD on Boeing model 757-200 series airplanes

USA - To prevent failure of the stowage bin attachment fitting at Station 680, which could result in the overhead stowage bin falling onto the passenger seats below and injuring passengers or impeding the evacuation of passengers in an emergency

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-402-AD; Amendment 39-12997; AD 2002-26-09] RIN... more

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

Washington, USA - To prevent fluid contamination inside the fueling float switch or changing of the wiring to the in-tank conduit, which could generate an ignition source and consequent fire and explosion in the fuel tank

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-44-AD; Amendment 39-13006; AD 2002-26-18] RIN... more

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

Washington, USA - To detect and correct cracking in the fuselage skin or doubler at the corner of the forward lower cargo doorjamb, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-78-AD; Amendment 39-12998; AD 2002-26-10] RIN... more

Civil aviationFAA AD on Saab model SAAB 2000, SAAB SF340A, and SAAB 340B series airplanes

Washington, USA - To prevent ice from blocking the pitot system, due to the pitot tube not having enough heating capacity to stay above freezing temperature, which could result in erroneous airspeed indications

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-104-AD; Amendment 39-13007; AD 2002-26-19] RIN... more

Civil aviationFAA AD on Boeing model 747 series airplanes

To detect and correct wear damage of the fuselage skin in the area at the interface between the vertical stabilizer and fuselage skin, which could result in thinning and cracking of the fuselage skin, and consequent in-flight depressurization of the plan

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-85-AD; Amendment 39-13003; AD 2002-26-15] RIN... more

Civil aviationFAA AD on Fokker model F-28 Mark 0070 and 0100 series airplanes

USA - To detect and correct an insufficient over-center force in the corresponding thrust reverser operating lever, and incorrect setting of the thrust reverser selector switch (S9), which could result in uncommanded deployment of the thrust reversers

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-290-AD; Amendment 39-13004; AD 2002-26-16] RIN... more