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Civil aviation

11,047 news found

Civil aviationFAA AD on Air Tractor, Inc. models AT-401, AT-401B, AT-402, AT-402A, AT-402B, AT-501, AT-502, AT-502A, AT-502B, AT-503A, AT-602, AT-802, and AT-802A airplanes

Washington, Usa - To detect and correct cracks in the upper aft longeron, which could cause the fuselage to fail. Such failure could result in loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 30, 2004 (Volume 69, Number 146)] [Page 45566-45570] Header Information Header... more

Civil aviationFAA AD on Empresa Brasileira de Aeronautica SA (Embraer) model EMB-135 and -145 series airplanes

Usa - To ensure that there is sufficient lightning bonding at the electrical harness for the tail boom strobe light, and to prevent the simultaneous failure of multiple avionics systems in the event of a lightning strike, which could result in reduced co

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 30, 2004 (Volume 69, Number 146)] [Page 45565-45566] Header Information Header... more

Civil aviationFAA AD on Airbus model A-330/202, -203, -223, and -243 airplanes, and A-330/300 series airplanes (2004-15-12)

Usa - To prevent uncommanded in-flight shutdown of the auxiliary power unit (APU), which could result in loss of critical electrical systems when the airplane is operated in emergency electrical configuration, and consequent reduced controllability of th

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 29, 2004 (Volume 69, Number 145)] [Page 45241-45243] Header Information Header... more

Civil aviationFAA AD on McDonnell Douglas model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and model MD-88 airplanes

Usa - To prevent failure of freeze protection ribbon heaters, which could result in the charring, scorching, smoking, and shorting out of freeze protection ribbon heaters in the lavatory water supply system and could also result in electrical arcing of f

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 29, 2004 (Volume 69, Number 145)] [Page 45239-45241] Header Information Header... more

Civil aviationFAA AD on Boeing model 737-200, -200C, -300, -400, and -500 series airplanes

Usa - To prevent contamination of the fueling float switch by moisture or fuel, and chafing of the float switch wiring against the fuel tank conduit, which could present an ignition source inside the fuel tank that could cause a fire or explosion

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 27, 2004 (Volume 69, Number 143)] [Page 44580-44586] Header Information Header... more

Civil aviationFAA AD on BAE Systems (Operations) Limited (Jetstream) model 4101 airplanes (2004-15-06)

Usa - To detect and correct fatigue cracking in the primary structure of the nose of the airplane at the forward avionics bay (fuselage stations 4 to 11), which could result in reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 27, 2004 (Volume 69, Number 143)] [Page 44589-44591] Header Information Header... more

Civil aviationFAA AD on BAE Systems (Operations) Limited model BAe-146 and Avro 146-RJ series airplanes (2004-15-05)

Usa - To prevent air from the auxiliary power unit (APU) bay being ingested into the flight deck and passenger cabin resulting in poor air quality and, if the air is contaminated, possible incapacitation of the flightcrew and passengers

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 27, 2004 (Volume 69, Number 143)] [Page 44594-44595] Header Information Header... more

Civil aviationFAA AD on Saab model SAAB SF-340A series airplanes

Usa - To prevent a momentary loss of data on the left-hand electronic flight instrumentation system screens, which could lead to the pilot's loss of situational awareness during initial climb or approach/landing, and possibly result in reduced control of

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 27, 2004 (Volume 69, Number 143)] [Page 44587-44589] Header Information Header... more

Civil aviationFAA AD on Airbus model A-319/111, -112, -113, and -114; A-320/111, -211, -212, and -214; and A-321/111, -112, and -211 series airplanes

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

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 19, 2004 (Volume 69, Number 137)] [Page 42858-42860] Header Information Header... more

Civil aviationFAA AD on Boeing model 767 series airplanes

Usa - To detect and correct the propagation of fatigue cracks in the vicinity of oil cans on the web of the aft pressure bulkhead, which could result in rapid decompression of the passenger cabin, possible damage or interference with the airplane control

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 16, 2004 (Volume 69, Number 136)] [Page 42549-42551] Header Information Header... more

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