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AVIONEWS - World Aeronautical Press Agency

101,303 news found

AirlinesAlitalia (3): measures which have been adopted for this carrier will not be sufficient, according to Wall Street Journal Europe

New York, USA - Italian Government's aim would consist in making this carrier survive at least till the end of general national election

According to Wall Street Journal Europe, a complete forecasting blindness exists with reference to Alitalia's problems and choices subscribed by Italian Government, trade unions and private shareholders.... 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