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CLARA MOSCHINI

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Civil aviation

11,458 news found

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

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

Civil aviationFAA Emergency AD on Boeing models 737-747-757 airplanes

USA - To require the flightcrew to maintain certain minimum fuel levels in the center fuel tanks, and to prohibit the use of the horizontal stabilizer fuel tank (model 747-400 series airplanes) and certain center auxiliary fuel tanks (on model 747)

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-NM-309-AD; AD 2002-24-51 Boeing Model 737-600, -700,... more

Civil aviationFAA Emergency AD on Bell Helicopter Textron Canada model 407 helicopters

USA - To detect an incorrect installation of swashplate drive link cup washers, which could limit the travel of the swashplate outer ring and lead to stud failure, failure of both swashplate drive link studs, and loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-SW-51-AD; AD 2002-23-51 Bell Helicopter Textron Canada... more

Civil aviationFAA AD on Eurocopter France model AS355N helicopters

Washington, USA - To prevent excessive starter-generator (S-G) vibration, which may lead to separation of an engine exhaust pipe ejector (ejector), impact with the main or tail rotor, 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-32-AD; Amendment 39-12943; AD 2002-22-16] RIN... more

Civil aviationFAA AD on Boeing model 737 series airplanes

Washington, USA - To prevent an uncommanded rudder hardover event and consequent loss of control of the airplane due to inherent failure modes, including single-jam modes, and certain latent failures or jams combined with a second failure or jam

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-251-AD; Amendment 39-12940; AD 2002-20-07 R1] RIN... more

Civil aviationFAA AD on Pilatus Britten-Norman Limited airplanes

Washington, USA - Models BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R, BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-CE-21-AD; Amendment 39-12926; AD 2002-22-02] RIN... more

Civil aviationFAA AD on Honeywell International, Inc., LF507 and ALF502R series turbofan engines

USA - To prevent separation of the combustor dome baffle from the combustion chamber liner assembly and the flow of hot combustor gases on oil and fuel lines which could result in an engine fire, an in-flight shutdown, and damage to the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-21-AD; Amendment 39-12931; AD 2002-22-06] RIN... more

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes

Washington, USA - To prevent severe flap asymmetry due to fractures of the carriage spindles on an outboard mid-flap, which could result in reduced control or loss of controllability of the airplane

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-214-AD; Amendment 39-12929; AD 2002-22-05] RIN... more

Civil aviationFAA AD on Boeing model 757-200, -200CB, and -300 series airplanes

Washington, USA - To prevent failure of an escape slide to deploy or inflate correctly, which could cause the slide to be unusable during an emergency evacuation and result in consequent injury to passengers or crewmembers

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-NM-392-AD; Amendment 39-12921; AD 2002-21-14] RIN... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes

Washington, USA - To prevent damage to the upper wing skin surface and its structure, due to prolonged short-circuit electrical arcing of the anti-ice system

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-216-AD; Amendment 39-12912; AD 2002-21-06] RIN... more