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Civil aviation

11,458 news found

Civil aviationFAA AD on The Cessna Aircraft Company model 525 airplanes

Usa - To correct this single-point failure in the electric pitch trim system, which will result in a runaway pitch trim condition where the pilot could not disconnect using the control wheel autopilot/trim disconnect switc

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41920-41923] Header Information Header... more

Civil aviationFAA AD on Boeing model 747-100, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747 SR series airplanes

Usa - To prevent fractured discharge heads, which could cause the fire extinguishing agent to leak, which could result in an uncontrolled engine fire that could spread to the strut and wing, or an uncontrolled auxiliary power unit (APU) fire that could s

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41926-41928] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, and F4-600R series airplanes; A-310 series airplanes; equipped with Pratt & Whitney JT9D-7R4 or 4000 series engines (2004-14-17)

Washington, Usa - To prevent in-flight deployment of a thrust reverser, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41930-41934] Header Information Header... more

Civil aviationFAA AD on Airbus model A-300 B4-600, B4-600R, C4- 605R Variant F, and F4-600R, and A-310 series airplanes (2004-14-08)

Usa - To prevent failure of the attachment system of the cargo insulation blankets, which could result in detachment and consequent tearing of the blankets, resulting in blanket pieces being ingested into and jamming the forward outflow valve of the pres

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41925-41926] Header Information Header... more

Civil aviationFAA AD on Bombardier model DHC-8-102, -103, and -106 airplanes

Washington, Usa - To prevent increased roll forces due to cracking of the left and right aileron tab actuator arm channels, which could be interpreted by the pilot as a flight control problem and might lead to loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41928-41930] Header Information Header... more

Civil aviationFAA AD on The New Piper Aircraft, Inc., models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32- 301FT, PA-32-301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP airplanes

Usa - To detect and correct inadequate control wheel attachment design features, which could result in loss of control of the ailerons and elevator

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41407-41410] Header Information Header... more

Civil aviationFAA AD on Airbus model A-310 series airplanes (2004-13-24)

Usa - To prevent failure of the retaining ring on the pressure-off brakes (POBs) of the power control units of the slats and flaps, which could result in slat or flap blowback or runaway, with consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41396-41398] Header Information Header... more

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

Usa - To prevent possible failure of the fuel quantity indication (FQI) system, which could cause the flightcrew to act on misleading information and possibly lead to in-flight fuel exhaustion

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41417-41418] Header Information Header... more

Civil aviationFAA AD on Saab model SAAB 2000 series airplanes

Usa - To prevent failure of the backup struts in the left and right nacelles due to fatigue cracking, which could result in loss of fail-safe redundancy in the design of the nacelle in terms of load capability, and consequent separation of the engine fro

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41405-41407] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas DC-9-82 (MD-82) and DC-9-83 (MD-83) airplanes; and model MD-88 airplanes

Usa - To prevent uncommanded movement of the captain's and first officer's seats during takeoff and landing, which could result in interference with the operation of the airplane and consequent temporary loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41419-41421] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model MD-11 and -11F airplanes (2004-14-10)

Usa - To prevent arcing and heat damage to the attachment points of the main external and galley power receptacle ground wire, insulation blankets outboard and aft of the receptacle area, and adjacent power cables, which could result in smoke and fire in

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41414-41416] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model DC-8-11, DC-8- 12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC- 8F-54, and DC-8F-55; DC-8-50, -60, -60F, -70 and - 70F series airplanes (2004-14-05)

Washington, Usa - To prevent uncommanded seat movement during takeoff and/or landing, which could result in interference with the operation of the airplane and consequent temporary loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41403-41405] Header Information Header... more

Civil aviationFAA AD on Israel Aircraft Industries, Ltd., model 1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes

Washington, Usa - To detect and correct cracking of the skins of the rudder assembly, which could result in reduced structural capability of the rudder and reduced controllability of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 9, 2004 (Volume 69, Number 131)] [Page 41411-41413] Header Information Header... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 series airplanes (2004-10-09)

Washington, Usa - To prevent overheating of the in-line splices of the APU and IDG feeder cables, which can lead to smoke, fumes, and possible fire in the flight deck and cabin

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 21, 2004 (Volume 69, Number 99)] [Page 29217-29218] Header Information Header Information DEPARTMENT... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe 146 and Avro 146-RJ series airplanes (2004-10-11)

Usa - To prevent the inability of the left-hand fire extinguisher on one or more engines to discharge, and consequent inability to control or suppress an engine fire

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 21, 2004 (Volume 69, Number 99)] [Page 29216-29217] Header Information Header Information DEPARTMENT... more