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CLARA MOSCHINI

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Civil aviation

11,114 news found

Civil aviationFAA AD on Boeing model 727-200 series airplanes equipped with a No. 3 Cargo Door (2005-11-09)

Washington, Usa - To detect and correct cracking of the forward, lower corner frame and forward end of the lower beam of the No. 3 cargo door, which could result in failure of the affected door stops, loss of the cargo door, and consequent rapid decompre

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32984-32986] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes (2005-11-10)

Washington, Usa - To prevent the loss of hydraulic power from both hydraulic systems, which could lead to reduced controllability of the airplane, and to prevent brake failure, which could result in the loss of directional control on the ground and

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32986-32988] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Grob-Werke model G-120A airplanes

Washington, Usa - To replace front and rear main landing gear bearings that are susceptible to damage when exposed to high axial loads, which could result in failure of the landing gear bearing. This failure could lead to loss of control on landing

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32988-32990] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 Airplanes

Usa - To detect and correct fatigue cracking in the fuselage pressure skin above the left and right MLG bay; such fatigue cracking could adversely affect the structural integrity of the fuselage and its ability to maintain pressure differential

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32982-32984] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Precise Flight, Inc. models SVS I and SVS IA Standby Vacuum Systems

Washington, Usa - To correct problems with the SVS before failure or malfunction during instrument flight rules (IFR) flight that can lead to pilot disorientation and loss of control of the aircraft

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32992-32996] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-200, -300, and -300F series airplanes (2005-11-12)

Washington, Usa - To prevent fire extinguishing agent from leaking out of the seals around the ducts in the forward cargo compartment in the event of an in-flight fire, which could result in failure to extinguish the fire and consequent smoke or fire ext

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32996-32998] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Extra Flugzeugproduktions-und Vertriebs-GmbH models EA-300, EA-300S, EA-300L, and EA-300/200 airplanes

Washington, Usa - To prevent fuel from flowing behind the firewall in the case of a fuel leak. This could result in an in-flight fire, which could cause loss of the airplane and crew

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2005 (Volume 70, Number 108)] [Page 32990-32992] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL- 604) Airplanes Modified by Supplemental Type Certificate (STC) SA4900SW

Washington, Usa - To prevent a damaged microphone jack assembly from interfering with movement of the control column, which could result in loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 27, 2005 (Volume 70, Number 102)] [Page 30621-30624] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Boeing model 747 series airplanes

Washington, Usa - To to detect and correct fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 25, 2005 (Volume 70, Number 100)] [Page 29940-29941] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on AeroSpace Technologies of Australia Pty Ltd. models N22B, N22S, and N24A airplanes

Washington, Usa - To detect and correct cracks in the rudder control lever torque shafts and discrepancies in the thickness of the lever shaft side plates, which could result in failure of the rudder control lever torque shaft

Airworthiness Directive Federal Register Information [Federal Register: May 23, 2005 (Volume 70, Number 98)] [Page 29437-29440] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 777-200 and -300 series airplanes (2005-10-17)

Washington, Usa - To prevent fatigue cracks in the lower t-chord at the bolt holes common to the paddle fittings that could result in fractures of one or more of the t-chord segments, which could lead to detachment of the lower wing panel and consequent

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28797-28800] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, 747-100B, 747- 200B, 747-300, 747-400, 747-400D, 747SR, and 747SP series airplanes (2005-10-19)

Washington, Usa - To ensure that the galley cart lift can be sent only from the deck on which it is in use, which will prevent unexpected movement of the cart lift that could result in possible injury to catering personnel or flight attendants

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28795-28797] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747 airplanes (2005-10-21)

Washington, Usa - To detect and correct fatigue cracks in the BS 1000 bulkhead chord, which, if not repaired before they reach critical length, could result in the failure of the adjacent structure and skin and lead to in-flight depressurization of the a

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28803-28806] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on General Electric (GE) CF6-80E1 series turbofan engines

Washington, Usa - To prevent an undetected failure of the ECU DIU, which could result in uncommanded acceleration to the overspeed limit without response to throttle commands. The airplane could then experience asymmetric thrust

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28806-28808] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, and -400D series airplanes; and model 747SR series airplanes (2005-10-18)

Washington, Usa - To detect and correct stress corrosion cracking of the stop support fittings of the MEDs, which could result in damage to the adjacent forward edge frame of the door and consequent loss of a MED and rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28800-28803] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Schweizer Aircraft Corporation model 269C, C-1, and D helicopters

Washington, Usa - To prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of cont

Airworthiness Directive Federal Register Information [Federal Register: May 18, 2005 (Volume 70, Number 95)] [Page 28415-28417] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Rolls-Royce Corporation 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, - C20F, -C20J, -C20S, and -C20W turboprop and turboshaft engines

Washington, Usa - To minimize the risk of uncontained 1st stage turbine wheel fragments from causing damage to the aircraft or damage to the second engine on twin-engine installations, which could lead to loss of control and loss of the aircraft

Airworthiness Directive Federal Register Information [Federal Register: May 18, 2005 (Volume 70, Number 95)] [Page 28420-28423] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, and F4-600R series airplanes, and model C4-605R Variant F Airplanes

Washington, Usa - To prevent electrical arcing inside the fuel tank, due to insufficient bonding, which could result in the ignition of fuel vapors with a potential risk of explosion of the fuel tank

Airworthiness Directive Federal Register Information [Federal Register: May 18, 2005 (Volume 70, Number 95)] [Page 28417-28419] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes (2005-10-10)

Washington, Usa - To detect and correct latent failure of the primary load path of the HSTA, which, in conjunction with a failure of the HSTA secondary nut, could result in loss of horizontal trim control and consequent reduced controllability of the air

Airworthiness Directive Federal Register Information [Federal Register: May 17, 2005 (Volume 70, Number 94)] [Page 28181-28184] Header Information DEPARTMENT OF TRANSPORTATION Federal... more