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Civil aviation

11,114 news found

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

Civil aviationFAA AD on Boeing model 767-200, -300, and -300F series airplanes (2004-09-11)

Usa - To detect and correct cracks in the outer cylinder of the main landing gear (MLG), which could result in collapsed MLG and consequent reduced controllability of the airplane during takeoff and landing

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 30, 2004 (Volume 69, Number 84)] [Page 23644-23646] Header Information Header... more

Civil aviationFAA AD on Boeing model 747 series airplanes (2004-09-10)

Usa - To prevent overheating of the heater tape on potable water fill and drain lines, which may ignite accumulated debris or contaminants on or near the potable water fill and drain lines, resulting in a fire in the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 30, 2004 (Volume 69, Number 84)] [Page 23647-23650] Header Information Header... more

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

Usa - To prevent loss of the relevant alternating current (AC) bus bar, reduced structural integrity of the engine pylon, and consequent loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23090-23093] Header Information Header... more

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

To prevent leakage of hydraulic fluid from the parking brake operated valve (PBOV), which could cause the loss of the parking brake accumulator, and render the alternate braking system and the parking/emergency braking system inoperative, as well as caus

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23095-23097] Header Information Header... more

Civil aviationFAA AD on Boeing model 747-400 and -400D series airplanes

Usa - To prevent passenger service unit (PSU) panels from moving and falling from the PSU support rails during takeoff or landing, which could result in injury to passengers and could impede evacuation of the passengers in an emergency situation

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 28, 2004 (Volume 69, Number 82)] [Page 23098-23099] Header Information Header... more

Civil aviationFAA AD on Airbus model A-330/200 series airplanes

To prevent failure of the driving finger of the rudder servo control and consequent loss of the rudder servo control function in driving the rudder to its commanded position, which, if combined with an engine failure during takeoff or go around,

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 26, 2004 (Volume 69, Number 80)] [Page 22389-22392] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300B2 series airplanes; A-300B4 series airplanes; A-300B4-600, B4-600R, F4-600R, and C4-605R Variant F (Collectively Called A-300/600) series airplanes; and A-310 series airplanes

Washington, Usa - To detect and correct cracking of certain skin lap joints, which could result in reduced structural integrity and decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: April 21, 2004 (Volume 69, Number 77)] [Page 21397-21401] Header Information Header... more