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Civil aviation

11,047 news found

Civil aviationFAA AD on Airbus model A-330 and model A-340/200 and -300 series airplanes (2004-18-14)

Usa - To prevent uncommanded movement of a spoiler during flight, which could result in reduced controllability of the airplane and consequent significant increased fuel consumption during flight, which could necessitate an in-flight turn-back or diversi

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 14, 2004 (Volume 69, Number 177)] [Page 55326-55329] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4 series airplanes; and model A-300 B4-601, B4-603, B4-605R, B4-620, B4-622R, C4- 605R Variant F, and F4-605R airplanes (2004-18-13)

Usa - To detect and correct cracking of the gantry lower flanges in the MLG bay area, which could result in decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 14, 2004 (Volume 69, Number 177)] [Page 55329-55332] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F, DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F airplanes

Usa - To prevent chafing of the wire bundle located behind the flight engineer's panel caused by the wire bundle coming in contact with the lower edge of the feed-through, and consequent electrical arcing, which could result in smoke and fire in the cock

Airworthiness Directive Federal Register Information [Federal Register: September 14, 2004 (Volume 69, Number 177)] [Page 55323-55326] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 727, 727C, 727-100, -100C, and -200 series airplanes (2004-18-08)

Usa - To detect and correct cracks and corrosion on the attach fitting holes of the forward trunnion attach fittings of the main landing gear (MLG), which could result in the collapse of the MLG

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8, 2004 (Volume 69, Number 173) [Page 54211-54213] Header Information Header... more

Civil aviationFAA AD on Boeing model 737-200, -200C, -300, - 400, and -500 series airplanes (2004-18-06)

Washington, Usa - To find and fix fatigue cracking of certain upper and lower skin panels of the fuselage, which could result in sudden fracture and failure of the skin panels and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8, 2004 (Volume 69, Number 173( [Page 54206-54211] Header Information Header... more

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

Usa - To prevent contact between the lockwire pigtail of the fitting and the stiffener located on the inside surface of the fuel access covers of the wings, which could serve as a potential ignition source within the fuel tank if a cover is struck by lig

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8,2004 (Volume 69, Number 173) [Page 54213-54215] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-14, DC-9- 15, and DC-9-15F airplanes; and model DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes

Washington, Usa - To prevent failure of the outboard idler hinge fitting of the left and right wing flap at station Xw=333.148 due to fatigue cracking, which could result in a deflected flap that may cause asymmetric lift and consequent reduced controlla

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8, 2004 (Volume 69, Number 173) [Page 54201-54204] Header Information Header... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 and Avro 146-RJ series airplanes

Washington, Usa - To prevent the installation of incorrect pressurization discharge valves and cabin pressure controllers, which could subject the airframe to excess stress and adversely affect the airframe fatigue life

Airworthiness Directive Federal Register Information Federal Register Information Federal Register: September 8, 2004 (Volume 69, Number 173) [Page 54204-54205] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model MD-10-10F, MD- 10-30F, MD-11, MD-11F, and 717-200 airplanes

Usa - To prevent, under certain conditions during the FMS PROF descent, the uncommanded descent of an airplane below the selected level-off altitude, which could result in an unacceptable reduction in the separation between the airplane and nearby air tr

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 3, 2004 (Volume 69, Number 171)] [Page 53794-53795] Header Information Header... more

Civil aviationFAA AD on Boeing model 737-600, 737-700, 737- 700C, 737-800, and 737-900 series airplanes (2004-18-02)

Washington, Usa - To prevent high electrical resistance in the squib firing circuit, which could result in insufficient electrical current to fire the fire extinguisher bottle squib and discharge the fire extinguishing agent, which could lead to an uncon

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 2, 2004 (Volume 69, Number 170)] [Page 53605-53607] Header Information Header... more

Civil aviationFAA AD on Boeing model 777 series airplanes (2004-17-05)

Usa - To prevent leakage of fire extinguishing agent through the filter/regulator of the cargo fire extinguishing system, which could result in the inability of the fire extinguishing system to suppress a fire in the cargo compartment of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 2, 2004 (Volume 69, Number 170)] [Page 53607-53609] Header Information Header... more

Civil aviationFAA AD on Bombardier model CL-600-2C10 (Regional Jet Series 700 & 701), and CL-600-2D24 (Regional Jet Series 900) series airplanes

Washington, Usa - To detect and correct cracking in any primary fuel ejector, which could cause fuel leakage into the center fuel tank, and could result in engine shutdown during flight

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 2, 2004 (Volume 69, Number 170)] [Page 53609-53614] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model DC-10 series airplanes, model MD-10 series airplanes, and model MD-11 series airplanes (2001-14-08 R1)

Washington, Usa - To prevent various failures of electric motors of the auxiliary hydraulic pump and associated wiring, which could result in fire at the auxiliary hydraulic pump and consequent damage to the adjacent electrical equipment and/or structure

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: September 1, 2004 (Volume 69, Number 169)] [Page 53336-53337] Header Information Header... more