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Civil aviation

11,047 news found

Civil aviationFAA (Correction) AD on Boeing model 757-200 series airplanes modified by Supplemental Type Certificate (STC) SA979NE

Washington, Usa - To prevent structural overload of the cargo barriers, which could cause the barriers to fail, allowing the cargo to shift, resulting in damage to the auxiliary fuel tanks, residual fuel leakage, and consequent increased risk of a fire

Airworthiness Directive Federal Register Information [Federal Register: July 13, 2006 (Volume 71, Number 134)] [Page 39521-39522] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 airplanes, CL-600-2D15 airplanes, and CL-600-2D24 airplanes (2006-14-05)

Washington, Usa - To prevent failure of the lower panel of the MLG door, departure of the lower panel from the airplane, and consequent damage to airplane structure, which could adversely affect the airplane's continued safe flight and landing

Airworthiness Directive Federal Register Information [Federal Register: July 11, 2006 (Volume 71, Number 132)] [Page 38979-38985] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 F4-600R series airplanes and model A-300 C4-605R Variant F airplanes (2006-14-06)

Washington, Usa - To prevent fatigue cracking of the fuselage skin, which could result in loss of the structural integrity of the fuselage and consequent rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 7, 2006 (Volume 71, Number 130)] [Page 38515-38516] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/200 and A-330/300 series airplanes, and Airbus model A-340/200 and A-340/300 series airplanes (2006-14-02)

Washington, Usa - To prevent failure of the landing gear lengthening system, which could result in reduced controllability of the airplane on the ground during landing

Airworthiness Directive Federal Register Information [Federal Register: July 5, 2006 (Volume 71, Number 128)] [Page 38062-38064] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-31, DC-9- 32, DC-9-32F, DC-9-33F, DC-9-34, and DC-9-34F airplanes; and model DC- 9-40 and DC-9-50 series airplanes

Washington, Usa - To prevent point-contact arcing or filament heating in the fuel tank, which, in the event of a short or ground fault inside the fuel tank, could result in a fuel tank explosion and consequent loss of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 5, 2006 (Volume 71, Number 128)] [Page 38053-38054] 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 model A-340/541 and A-340/642 airplanes (2006-14-01)

Washington, Usa - To detect and correct improper routing of the electrical harnesses of certain slide/rafts, which could prevent proper deployment of the slide/rafts and delay evacuation of passengers and flightcrew during an emergency

Airworthiness Directive Federal Register Information [Federal Register: July 5, 2006 (Volume 71, Number 128)] [Page 38059-38062] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Boeing model 737 airplanes

Washington, Usa - To prevent failure of the airplane to pressurize and subsequent failure of the flightcrew to recognize and react to a valid cabin altitude warning horn, which could result in incapacitation of the flightcrew due to hypoxia and loss

Airworthiness Directive Federal Register Information [Federal Register: July 3, 2006 (Volume 71, Number 127)] [Page 37980] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA (Correction) AD on Boeing model 757-200 series airplanes modified by Supplemental Type Certificate (STC) SA979NE (2006-13-17)

Washington, Usa - To prevent structural overload of the cargo barriers, which could cause the barriers to fail, allowing the cargo to shift, resulting in damage to the auxiliary fuel tanks, residual fuel leakage, and consequent increased risk of a fire

Airworthiness Directive Federal Register Information [Federal Register: June 28, 2006 (Volume 71, Number 124)] [Page 36671-36674] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus model A-330/200 and -300 series airplanes, model A-340/200 and -300 series airplanes, and model A-340/541 and -642 airplanes

Washington, Usa - To prevent loss of pressure in the escape slides/rafts after an emergency evacuation, which could result in inadequate buoyancy to support the raft's passenger capacity during ditching, and increase the chance for injury to passengers

Airworthiness Directive Federal Register Information [Federal Register: June 28, 2006 (Volume 71, Number 124)] [Page 36674] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Mitsubishi Heavy Industries MU-2B series airplanes

Washington, Usa - To detect and correct cracks, corrosion, fractures, and incorrect torque values in the wing attach barrel nuts, which could result in failure of the wing barrel nuts and/or associated wing attachment hardware

Airworthiness Directive Federal Register Information [Federal Register: June 29, 2006 (Volume 71, Number 125)] [Page 36984-36986] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Raytheon Aircraft Company 65, 90, 99, and 100 series airplanes

Washington, Usa - To prevent water accumulation in the rudder trim tab, which could result in a change in the mass properties and possibly a lower flutter speed of the airplane. A lower airplane flutter speed could result in failure and loss of control

Airworthiness Directive Federal Register Information [Federal Register: June 26, 2006 (Volume 71, Number 122)] [Page 36185-36187] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To correct improper aileron assembly configuration, which could result in failure of the aileron mass balance weight

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35778-35781] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737 airplanes (2006-13-13)

Washington, Usa - To prevent failure of the airplane to pressurize and subsequent failure of the flightcrew to recognize and react to a valid cabin altitude warning horn, which could result in incapacitation of the flightcrew due to hypoxia

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35781-35783] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To prevent engine fuel starvation during maximum climb and descent caused by poor fuel tank venting with low fuel levels, which could result in a loss of engine power during critical phases of flight

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35783-35785] 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 model A-340/541 and A-340/642 airplanes

Washington, Usa - To prevent anti-fretting material contamination, which could reduce the effectiveness of the fire extinguisher system to discharge fire extinguishing agents and to lower the concentration of Halon gas in the LDCC or BCRC in timely way

Airworthiness Directive Federal Register Information [Federal Register: June 22, 2006 (Volume 71, Number 120)] [Page 35789-35792] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2 and A-300B4; A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes

Washington, Usa - To prevent cracking in the web of nose rib 7, which could result in rupture of the attachment fitting between the inner flap and flap track 2, and consequent reduced structural integrity of the flap

Airworthiness Directive Federal Register Information [Federal Register: June 21, 2006 (Volume 71, Number 119)] [Page 35507-35509] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes

Washington, Usa - To detect and correct cracks in the rudder end rib, which could result in failure of the rudder end rib

Airworthiness Directive Federal Register Information [Federal Register: June 21, 2006 (Volume 71, Number 119)] [Page 35502-35505] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 757 airplanes (2006-13-03)

Washington, Usa - To prevent arcing or sparking at the interface between the bulkhead fittings of the engine fuel feed tube and the front spar during a lightning strike, which could provide a possible ignition source for the fuel vapor inside the tank

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35381-35383] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 727-200 series airplanes equipped with a No. 3 cargo door (2006-13-01)

Washington, Usa - To detect and correct cracking of the forward frame and fuselage skin of the No. 3 cargo door cutout, which could result in failure of the frame and skin, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35385-35387] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica S.A. (EMBRAER) model ERJ-170 airplanes

Washington, Usa - To prevent incorrect operation of the negative pressure relief valve, which could result in negative pressures that exceed the structural strength limits of the airframe and lead to reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 20, 2006 (Volume 71, Number 118)] [Page 35383-35385] Header Information DEPARTMENT OF TRANSPORTATION Federal... more