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CLARA MOSCHINI

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Civil aviation

11,114 news found

Civil aviationFAA AD on Boeing model 777-200 series airplanes

Washington, Usa - To prevent the possibility of the airplane departing the runway during Category IIIB autoland operations due to autopilot disconnect in low visibility weather conditions, and to warn the flightcrew of the potential for autopilot disconn

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2004-NM-28-AD; Amendment... more

Civil aviationFAA AD on Boeing model 727, 727-100C, 727-200F, and 727C series airplanes

Usa - To detect and correct fatigue cracks in the fuselage skin, strap (bearstrap), or doubler at the forward and aft hinge fittings for the main deck cargo door, which could reach critical crack length and result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-191-AD; Amendment... more

Civil aviationFAA AD on Raytheon model Beech 400A and 400T series airplanes

Usa - To prevent intermittent sticking of the relays on the roll trim printed circuit board (PCB) in either the open or closed position, which could result in an out-of-trim condition that could require using considerable control wheel force to keep the

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-225-AD; Amendment... more

Civil aviationFAA AD on Boeing model 727, 727C, 727-100, and 727-100C series airplanes

Usa - To detect and correct fatigue cracks in the web, inner chord, and outer chord of the forward and aft frames of the aft cargo door opening, which could result in loss of the aft cargo door and rapid decompression of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-205-AD; Amendment... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes

Usa - To prevent failure of the dual shuttle valve in the number 2 hydraulic system, with reduced maximum elevator rate on the left side, which could result in pilot induced pitch oscillation, 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. 2001-NM-365-AD; Amendment... more

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

Usa - To prevent the latch cable assembly from disconnecting from the latch block assembly of the door mounted escape slides, which could result in an escape slide not deploying in an emergency situation

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-156-AD; Amendment... more

Civil aviationFAA AD on McDonnell Douglas model 717-200 airplanes

Washington, Usa - To detect material defects in the inboard ends of the outer skin panels of the horizontal stabilizer at Station Xh=7.234, which could lead to cracks and an associated loss of strength in the attachments, and consequent reduced structura

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-213-AD; Amendment... more

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

Washington, Usa - To prevent the failure of an emergency slide or slide/raft to fully inflate during an emergency situation, which could impede an evacuation and result in injury to passengers or airplane crewmembers

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-84-AD; Amendment... more

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

Washington, Usa - To prevent separation of the screws in the autopilot clutch assembly of the SM-300 servo, which could result in uncommanded engagement of the autopilot servo 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. 2002-NM-79-AD; Amendment... more

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

Usa - To find and fix fatigue cracking of structure near and common to the upper chord and splice fittings of the rear spar of the wing, which could result in loss of structural integrity of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-238-AD; Amendment... more

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

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