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Civil aviation

11,458 news found

Civil aviationFAA AD on Honeywell International Inc. ALF502L series and ALF502R series turbofan engines

Washington, USA - To prevent total loss of engine power, in-flight engine shutdown, release of turbine blades, separation of the exhaust nozzle, and possible damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 9, 2006 (Volume 71, Number 89)] [Page 26823-26826] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Airbus model A-319/100 and A-320/200 series airplanes; and model A-320/111 airplanes

Washington, Usa - To ensure that the fuel pumps do not run while dry, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 8, 2006 (Volume 71, Number 88)] [Page 26685-26687] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B4-600, B4-600R, and F4-600R, model C4-605R Variant F airplanes; A-310/200 and A-310/300 series airplanes

Washington, Usa - To prevent an insulation blanket or other debris from being ingested into and jamming the forward outflow valve of the pressure regulation subsystem, which could lead to the inability to control cabin pressurization and adversely affect

Airworthiness Directive Federal Register Information [Federal Register: May 4, 2006 (Volume 71, Number 86)] [Page 26191-26194] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-09-06)

Washington, Usa - To detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 3, 2006 (Volume 71, Number 85)] [Page 25926-25928] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Dassault model Falcon 900EX airplanes

Washington, Usa - To detect and correct missing rivets in the front section of the central engine mast, which could result in reduced structural integrity of the central engine mast, possible separation of the engine from the airplane during flight

Airworthiness Directive Federal Register Information [Federal Register: May 3, 2006 (Volume 71, Number 85)] [Page 25924-25926] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Airbus model A-310/200 and -300 series airplanes (2006-09-05)

Washington, Usa - To detect and correct fatigue cracks of the rear spar internal angle and tee fitting, which could lead to the rupture of the internal angle, tee fitting, and rear spar, and consequent reduced structural integrity of the wings

Airworthiness Directive Federal Register Information [Federal Register: May 3, 2006 (Volume 71, Number 85)] [Page 25921-25924] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/200, A-330/300, A-340/200, and A-340/300 series airplanes; and A-340/541 and A-340/642 airplanes (2006-09-07)

Washington, Usa - To prevent fatigue cracking, damage, or corrosion, which could result in reduced structural integrity of these airplanes

Airworthiness Directive Federal Register Information [Federal Register: May 3, 2006 (Volume 71, Number 85)] [Page 25919-25921] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Boeing model 757-200 and -200PF series airplanes equipped with Pratt & Whitney engines (2006-09-02)

Washington, Usa - To detect and correct any gaps between the strut fitting and the forward engine mount assembly of both engines, which could result in separation of the engine from the wing and subsequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 26, 2006 (Volume 71, Number 80)] [Page 24571-24573] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Washington, Usa - To prevent cracked or fractured thrust links that could lead to the loss of the load path for the rear engine mount bulkhead and damage to other primary engine mount structure

Airworthiness Directive Federal Register Information [Federal Register: April 21, 2006 (Volume 71, Number 77)] [Page 20528-20530] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Air Tractor, Inc. models AT-802 and AT- 802A airplanes (206-08-09)

Washington, Usa - To detect and correct cracks in the wing main spar lower cap at the center splice joint, which could result in failure of the spar cap and lead to wing separation and loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2006 (Volume 71, Number 75)] [Page 19994-19998] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Air Tractor, Inc. models AT-400; AT- 401, AT-401B, AT-402, AT-402A, and AT-402B airplanes (2006-08-08)

Washington, Usa - To prevent fatigue cracks from occurring in the wing lower spar cap before the originally established safe life is reached which if not detected and corrected, could result in wing separation and loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2006 (Volume 71, Number 75)] [Page 19986-19994] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on General Electric Company CT64-820-4 turboprop engines

Washington, Usa - To prevent cracks in the rotating parts that could cause compressor and turbine wheel fracture and uncontained engine failure. An uncontained engine failure could cause possible damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2006 (Volume 71, Number 75)] [Page 20001-20005] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Revision) AD on Gulfstream model GIV-X and GV-SP series airplanes

Washington, Usa - To ensure that the flightcrew is advised of the appropriate procedures to follow in the event that the cockpit displays go blank or malfunction, which could result in a possible loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 13, 2006 (Volume 71, Number 71)] [Page 19114-19117] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Eurocopter France model SA-360C, SA- 365C, SA-365C1, and SA-365C2 helicopters

Washington, Usa - To detect a crack in a MGB base plate and prevent failure of one of the MGB attachment points to the frame, which could result in severe vibration and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: April 13, 2006 (Volume 71, Number 71)] [Page 19110-19114] Header Information DEPARTMENT OF TRANSPORTATION Federal... more