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Civil aviation

11,115 news found

Civil aviationFAA AD on Boeing model 737-200, -300, and -400 series airplanes

Washington, Usa - To prevent contamination of the fueling float switch of the auxiliary fuel tank by moisture or fuel, and chafing of the float switch wiring against the float switch conduit in the fuel tank, which could present an ignition source inside

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41113-41116] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4; and A-300 B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes (2006-15-04)

Washington, Usa - To detect and correct fatigue cracks in the lower flanges of gantries 1 through 5 inclusive in the MLG bay area, which could result in reduced structural integrity of the fuselage, and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41109-41113] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300B2-203 and A-300B4-203 airplanes; A-300B4-600, B4-600R, and F4-600R, and C4-605R Variant F airplanes; and model A-310/200 and -300 series airplanes (2006-15-06)

Washington, Usa - To prevent a sudden change in pitch due to an out-of-trim condition combined with an autopilot disconnect, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 20, 2006 (Volume 71, Number 139)] [Page 41118-41121] 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 (2006-15-03)

Washington, Usa - To detect and correct cracks in the ribs of the inboard integral fuel tanks in the left and right wings, which could lead to wing failure during flight with consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 19, 2006 (Volume 71, Number 138)] [Page 40886-40888] 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 (2006-15-02)

Washington, Usa - To detect and correct increased friction in the aileron control bellcrank assemblies, which could result in failure of the aileron flight-control system

Airworthiness Directive Federal Register Information [Federal Register: July 19, 2006 (Volume 71, Number 138)] [Page 40888-40891] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330/200 and -300, and A-340/200 and -300 series airplanes

Washington, Usa - To prevent a decrease in the torque limiter function, which could result in degradation and damage to the attachment bolts of the leading edge slat, loss of the slat, and consequent reduced control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 17, 2006 (Volume 71, Number 136)] [Page 40387-40389] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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