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Civil aviation

11,047 news found

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

Civil aviationFAA AD on Dornier model 328-300 series airplanes

Washington, Usa - To prevent water or ice accumulating in the elevator assembly, which could result in possible corrosion that reduces the structural integrity of the flight control surface, or in an unbalanced flight control surface

Airworthiness Directive Federal Register Information [Federal Register: May 12, 2005 (Volume 70, Number 91)] [Page 24938-24939] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationAVIONEWS' surveys: "Which reasons could have contributed to determine the recent accidents which involved both Italian Corps and Armed forces’ aircraft?

Rome, Italy - Technical problems, aspects related to human factor and operational procedures or pure chance?

AVIONEWS launches a new survey this time related to safety issue, with reference in particular to the recent accidents which involved several aircraft from both Italian Corps and Armed Forces. Respondents... more

Civil aviationFAA AD on Boeing model 777-200 and 777-300 series airplanes

Washington, Usa - To prevent the display of erroneous heading information to the pilot, which could result in loss of the main sources of attitude data, consequent high pilot workload, and subsequent deviation from the intended flight path

Airworthiness Directive Federal Register Information [Federal Register: May 11, 2005 (Volume 70, Number 90)] [Page 24703-24705] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-319, A-320, and A-321 series airplanes

Washington, Usa - To prevent failure of the MLG side-stay cuff lugs or down-lock spring attachments, which could result in improper down-lock of the MLG during a freefall extension, and possible collapse of the MLG

Airworthiness Directive Federal Register Information [Federal Register: May 11, 2005 (Volume 70, Number 90)] [Page 24699-24701] Header Information DEPARTMENT OF TRANSPORTATION Federal... more