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Civil aviation

11,047 news found

Civil aviationFAA AD on Boeing model 727-100 and -200; 737-100, -200, -200C, -300, -400 and -500; and 747 series airplanes (2004-10-06)

Washington, Usa - To ensure adequate electrical bonding between the penetration fittings of the hydraulic heat exchanger and the rear spars of the fuel tanks of the left and right wings

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28046-28051] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Airbus model A-300B4-600, A-300B4-600R, and A-300F4-600R (Collectively Called A-300/600), A-310, A-319, A-320, A-321, A-330, and A-340/200 and -300 series airplanes

Washington, Usa - To prevent obstruction of the air intake of the pitot probes, which could result in misleading information being provided to the flightcrew

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28044-28046] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 747-400, 747-400D, 747- 400F, 757-200, 757-200PF, 757-200CB, 767-200, 767-300, and 767-300F series airplanes (2004-10-05)

Washington, Usa - To ensure that the flightcrew is able to silence an erroneous overspeed or stall aural warning

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 18, 2004 (Volume 69, Number 96)] [Page 28051-28058] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model CL-215-6B11 (CL215T Variant), and CL-215-6B11 (CL415 Variant) series airplanes (2004-10-04)

Usa - To prevent failure of the rear engine mount struts, which could subsequently result in reduced structural integrity of the nacelle and engine support structure

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 17, 2004 (Volume 69, Number 95)] [Page 27831-27833] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dassault model Mystere-Falcon 50 series airplanes

Usa - To find and fix improper installation of the electrical wiring of the basic/optional cabin lighting, which could result in overheating of the wiring and possible smoke/fire in the cabin during an emergency situation

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 12, 2004 (Volume 69, Number 92)] [Page 26299-26301] Header Information Header Information DEPARTMENT... more

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

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 Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26010-26012] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes

Washington, Usa - To prevent the roll and pitch disconnect handles from being difficult to operate, which could result in an increase in pilot workload and subsequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26003-26004] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 340B series airplanes equipped with Hamilton Sundstrand propellers

Usa - To prevent erroneous tripping of the remote controlled circuit breakers (RCCB) (even though an overload condition does not exist), premature failure of the RCCBs, loss of power to the feather pump system, and consequent reduced controllability of

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26001-26003] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model DHC-7-100 series airplanes

Usa - To detect and correct fatigue cracking in the baggage door fittings and the support structure, which could result in structural failure, and consequent rapid decompression of the airplane during flight

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26025-26027] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dornier model 328-300 series airplanes

Usa - To prevent failure of certain ground spoiler support arms due to interference between the ground spoiler assemblies and the wing flaps, which could result in loss of function of affected ground spoiler assemblies and consequent reduced controllabil

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26017-26018] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes (2004-09-21)

Usa - To prevent failure of the windshield wiper assembly, which could result in loss of visibility, damage to the propeller(s) and/or engine(s), or penetration of the fuselage skin and consequent rapid depressurization of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26006-26008] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Bombardier model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Usa - To prevent oil leakage from the engine oil coolers, consequent in-flight engine shutdown due to low oil pressure, and reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26013-26015] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 727 series airplanes (2004-09-36)

Usa - To prevent undetected cracking of the H-11 bolts or excessive wear of the cadmium-plated bolts, which would compromise the primary load path of the engine support and could result in separation of the engine from the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26015-26017] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 747-400 and 747-400D series airplanes (2004-09-33)

Usa - To prevent a chafed hole in the fire extinguishing system tube of the aft cargo compartment, which could result in a lack of fire extinguishing agent and consequent uncontained fire in the aft cargo compartment

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26012-26013] Header Information Header Information DEPARTMENT... 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) series airplanes

Usa - To detect and correct gaps between the flap vane bracket and the adjacent lower skin and between the flap vane bracket and vane actuator beam, and premature cracking of the flap vane brackets, which could result in failure of the flap vane bracket

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 7, 2004 (Volume 69, Number 89)] [Page 25485-25488] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Gulfstream Aerospace LP model Galaxy and Gulfstream 200 airplanes

Usa - To prevent ice accumulation due to water entering the artificial feel unit (AFU), which could restrict or jam the aileron, resulting in reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 7, 2004 (Volume 69, Number 89)] [Page 25483-25485] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 757-200 series airplanes

Usa - To detect and correct cracking of the fuselage skin and bear strap at the forward, upper corner of the L1 entry door cutout, which could result in reduced structural integrity of the L1 entry door and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 7, 2004 (Volume 69, Number 89)] [Page 25481-25483] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model EMB-135 and EMB-145 series airplanes (2004-09-15)

Usa - To prevent separation of the wheels from the nose landing gear due to the failure of the outer wheel bearings, and consequent loss of control of the airplane during takeoff and landing

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24940-24941] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model EMB-135BJ and EMB-145XR series airplanes (2004-09-13)

Usa - To detect and correct cracking in the firewall of the auxiliary power unit (APU), which could result in reduced structural integrity of the firewall, and a consequent uncontained APU fire that could spread to the airplane structure

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24945-24946] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dornier model 328-100 and -300 series airplanes (2004-09-17)

Usa - To prevent fracture and/or breakage of the hinge bolt of the output rod of the rudder spring tab lever assembly, which could result in migration of the bolt tail, a loose spring tab, and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24952-24953] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dornier model 328-100 and -300 series airplanes (2004-09-16)

Usa - To prevent failure of the rudder flight control system due to cracking of the bearing lugs of the rudder spring tab lever assembly, which could result in loss of rudder control and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24953-24954] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Fokker model F-27 Mark 100, 200, 300, 400, 500, 600, and 700 series airplanes

Usa - To prevent the loss of both direct current (DC) generator systems and loss of several other airplane systems, which could lead to the pilot's inability to maintain controlled flight

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24954-24956] Header Information Header Information DEPARTMENT... more

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

Usa - To detect and correct corrosion on the seat rails for the passenger seats, which could result in the reduced structural integrity of the passenger seats, detachment of the seats from the seat rails, and injury to passengers

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24950-24952] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Dornier model 328-100 and model 328-300 series airplanes

Usa - To prevent failure due to cracking of the seat frame attach caps on the passenger seat assemblies, which could result in separation of the passenger seat from the supporting structure during an emergency landing, hard landing, or turbulence, and

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24944-24945] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on Boeing model 767 series airplanes powered by General Electric or Pratt & Whitney engines

Usa - To prevent fatigue cracking in the primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 5, 2004 (Volume 69, Number 87)] [Page 24947-24950] Header Information Header Information DEPARTMENT... more