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CLARA MOSCHINI

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Civil aviation

9,321 news found

Civil aviationFAA AD on Aerospatiale model ATR-42 and ATR-72 series airplanes

Washington, Usa - To prevent failure of the spacer base of the swinging lever spacers in the left and right leg assemblies of the main landing gear (MLG) and consequent asymmetrical braking, which could result in the airplane overrunning the runway durin

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-116-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-330 and A-340/200 and -300 series airplanes

Usa - To prevent failure of the escape slides/rafts to deploy correctly at door 3 Type I emergency exits, which could result in the escape slides/rafts being unusable during an emergency evacuation, and consequent injury to passengers or crew members

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-284-AD; Amendment... more

Civil aviationFAA AD on Dassault model Falcon 900EX series airplanes

Usa - To prevent failure of the fail-safe lugs of the forward engine mount, and consequent cracking of the pick-up folded sheet of the pylon forward rib, which could rupture the mast case box and result in loss of the two forward engine mounts and conseq

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-283-AD;... more

Civil aviationFAA AD on Airbus model A-330/200, A-330/300, A-340/200, and A-340/300 series airplanes

Usa - To ensure proper functioning of the elevator surfaces, and to detect and correct cracking of the attachment lugs of the mode selector valve position transducers on the elevator servocontrols, which could result in partial loss of elevator function

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-223-AD; Amendment... more

Civil aviationFAA AD on Bombardier model CL-215-1A10 and CL- 215-6B11 series airplanes

Usa - To prevent cracking in the inner bearing surface of the main landing gear (MLG) axles, which could result in failure of an axle, subsequent separation of the wheel from the airplane, and consequent reduced controllability of the airplane during tak

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-139-AD; Amendment... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 series airplanes

Washington, Usa - To find and fix damage and prevent subsequent failure of the rear spar fittings between the flex shaft of the flap secondary drive and the wing-to-fuselage structure, which could result in loss of the wing

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-154-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-320-111, -211, and -231 series airplanes

Washington, Usa - To detect and correct fatigue cracking in the transition and pick-up angles of the lower part of the center fuselage, which could result in reduced structural integrity of the wing-fuselage support and fuselage pressure vessel

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-118-AD; Amendment... more

Collins AerospaceCollins Aerospace

Civil aviationFAA AD on BAE Systems (Operations) Limited (Jetstream) model 4101 airplanes

Washington, Usa - To find and fix cracking of the casing of the nose landing gear (NLG), which could result in failure of the NLG, and consequent reduced controllability of the airplane during takeoff and landing

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-355-AD; Amendment... more

Civil aviationFAA AD on Boeing model 747-200C and -200F series airplanes

Usa - To find and fix cracking in certain upper deck floor beams, which could extend and sever floor beams at a floor panel attachment hole location and could result in rapid decompression and consequent loss of controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-278-AD; Amendment... more

Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600) series airplanes; and model A-310 series airplanes (2004-03-10)

Usa - To ensure that the flight crew is advised of the potential hazard associated with an in-flight deployment of the thrust reverser, and the procedures necessary to address it

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-303-AD; Amendment... more

Civil aviationFAA AD on Boeing model 777-200 series airplanes (2004-03-05)

Usa - To detect and correct cracks or damage to the web of the aft pressure bulkhead, which could enlarge if undetected, leading to rapid decompression of the airplane and consequent possible loss of flight critical systems

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-320-AD; Amendment... more

Civil aviationFAA AD on Boeing model 737-200 and -300 series airplanes equipped with a main deck cargo door installed in accordance with supplemental type certificate (STC) SA2969SO (2004-03-23)

Washington, Usa - To detect and correct cracking of the lower portion of the main deck cargo door frames, which could result in sudden depressurization, loss or opening of the main deck cargo door during flight, and loss of control of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-170-AD, Amendment... more

Civil aviationFAA AD on Airbus model A-320-111, -211, -212, and -231 series airplanes (2004-03-07)

Usa - To detect and correct fatigue cracking around the fasteners connecting the pressure panel to the flexible bracket at frame 36, adjacent to the longitudinal beams on the left and right sides of the airplane, which could result in reduced structural

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-107-AD; Amendment... more

Collins AerospaceCollins Aerospace

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

Usa - To ensure that the flightcrew is aware of the procedures required to prevent ice from contacting the ice impact panels on the engine fan case, which could result in a panel coming loose during flight and blocking the bypass flow through the engine

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-10-AD; Amendment... 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

Usa - To prevent internal overheating and arcing of circuit breakers and airplane wiring due to long-term use and breakdown of internal components of the circuit breakers, which could result in smoke and fire in the flight compartment and main cabin

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-82-AD; Amendment... more

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 (KC-10A- and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F; and model MD- 11 and MD-11F airplanes

Washington, Usa - To prevent separation of the inboard flap outboard hinge from the wing structure and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-43-AD; Amendment... more