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CLARA MOSCHINI

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Civil aviation

9,765 news found

Civil aviationFAA AD on Boeing model 747 series airplanes powered by General Electric (GE) CF6-80C2 series engines

Washington, USA - To find and fix discrepant fasteners of the diagonal brace fittings, which could result in reduced structural integrity of the diagonal brace-to-strut attachment, and possible separation of the strut and engine from the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-17-AD; Amendment 39-12968; AD 2002-24-03] RIN... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on Airbus model A300 B2 and B4 series airplanes; A300 B4-600, B4-600R, and F4-600R (Collectively Called A300- 600) series airplanes; and model A310 series airplanes

Washington, USA - To prevent incapacitation of the flightcrew due to lack of oxygen, which could result in loss of control of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-40-AD; Amendment 39-12969; AD 2002-24-04] RIN... more

Civil aviationFAA AD on Dassault model Falcon 2000 series airplanes

Washington, USA - To prevent jamming of the flap jackscrews during the approach to landing, which could result in the inability to move the flaps or an asymmetric flap condition, and consequent reduced controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-417-AD; Amendment 39-12963; AD 2002-23-19] RIN... more

Civil aviationFAA AD on Boeing model 747 series airplanes

Washington, USA - To find and fix discrepancies of certain bolt holes of the fail- safe bar of the flap tracks of the wing trailing edge flaps, which could result in separation of the flap and consequent loss of control of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-24-AD; Amendment 39-12965; AD 2002-23-21] RIN... more

Civil aviationFAA AD on Dassault model Falcon 900EX and Mystere Falcon 900 series airplanes

Washington, USA - To prevent jamming of the flap jackscrews during the approach to landing, which could result in the inability to move the flaps or an asymmetric flap condition, and consequent reduced controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-418-AD; Amendment 39-12964; AD 2002-23-20] RIN... more

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

Washington, USA - To prevent failure of the 9-degree frame (frame) due to a crack at the latch support, loss of a passenger door, damage to the rotor system, and subsequent loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-SW-34-AD; Amendment 39-12948; AD 2002-23-04] RIN... more

Civil aviationFAA AD on Boeing model 747-100, -200B, -200C, - 200F, -300, -400, -400F, and 747SR series airplanes

USA - To find and fix cracking of the lower lobe panel of the fuselage skin of the aft cargo bay, which could lead to reduced structural integrity of the side cargo door cutout of the main deck, and result in rapid depressurization of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-270-AD; Amendment 39-12959; AD 2002-23-15] RIN... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on Pratt & Whitney Canada PT6A series turboprop engines

Washington, USA - To prevent failure of the turbine exhaust duct due to cracking that could result in possible separation of the reduction gearbox and propeller from the engine, and possible loss of control of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-44-AD; Amendment 39-12957; AD 2002-23-13] RIN... more

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

To prevent an undetected anomalous radio altitude signal that is passed along to the flare control law of the flight control computer, which could cause the airplane to flare too high or too low during landing, and consequently result in a hard landing

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-406-AD; Amendment 39-12962; AD 2002-23-18] RIN... more

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

To prevent interference between the cockpit control wheels and the chart holder assembly, which could result in restricted movement of the control wheel travel when rotating the right- and left-wing- down, and consequent reduced controllability of plane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-375-AD; Amendment 39-12960; AD 2002-23-16] RIN... more