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Civil aviation

11,114 news found

Civil aviationFAA AD on Airbus model A-300 B2 and B4 series airplanes; and model A-300 B4-600, B4-600R, and F4-600R series airplanes, and model C4-605R Variant F airplanes (2004-20-11)

Usa - To find and fix previously done repairs of the wing slats that have inadequate static and/or fatigue strength, which, if not corrected, could result in loss of the slats and consequent reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 13, 2004 (Volume 69, Number 197)] [Page 60801-60802] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-300 B2 and B4 series airplanes; model A-300 B4-600, A300 B4-600R, A300 F4-600R series airplanes, and A-300 C4-605R Variant F airplanes (Collectively Called A300-600); and model A-310 series airplanes (2004-20-12)

Usa - To detect and correct frayed or corroded control cables for the elevator and rudder, which could result in a ruptured control cable, and possible reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: October 13, 2004 (Volume 69, Number 197)] [Page 60799-60801] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-200B, -200C, -200F, -300, -400, -400D, and -400F series airplanes; and model 747SP series airplanes (2004-20-16)

Usa - To prevent mineral build-up on the auxiliary power unit (APU) and engine fire shutoff switches, which could lead to failure of the switches to discharge fire suppressant in the affected area and could result in an uncontrolled fire that could sprea

Airworthiness Directive Federal Register Information [Federal Register: October 13, 2004 (Volume 69, Number 197)] [Page 60807-60809] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationDepleted uranium: an investigation by Health Commission of the Sardinia Region Council started

Cagliari, Italy - Council, private committees, health care units and military representatives acting to verify the existance of concrete damaging effects in the territory

The issue regarding the depleted uranium are not only in the centre of Italian Parliament’s attention, as it is already attending to perform an investigation promoted by Italian Senate Defence Commission (... more

Civil aviationFAA AD (Correction) on Boeing model 727 series airplanes modified in accordance with supplemental Type Certificate SA-1444SO, SA-1509SO, SA-1543SO, or SA-1896SO (2002-16-22)

To prevent structural failure of the main deck cargo door hinge or failure of the cargo door system, which could result in the loss or opening of the cargo door while the airplane is in flight, and consequent rapid decompression of the airplane, includin

Airworthiness Directive Federal Register Information [Federal Register: October 7, 2004 (Volume 69, Number 194)] [Page 50299] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD (Correction) on Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 series airplanes

Washington, Usa - To prevent slippage of the pilot/co-pilot shoulder harness, which could result in failure of the shoulder harness to maintain proper belt length adjustment and tension. Such failure could result in pilot/co- pilot injury

Airworthiness Directive Federal Register Information [Federal Register: October 7, 2004 (Volume 69, Number 194)] [Page 60081] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Pratt & Whitney Canada models PW-123, PW-123B, PW-123C, PW-123D, PW-123E, PW-123AF, PW-124B, PW-125B, PW-126A, PW-127, PW-127E, PW-127F, and PW-127G turboprop engines (2004-20-01)

Washington, Usa - To prevent loss of throttle response and overspeed, resulting in engine in-flight shutdown

Airworthiness Directive Federal Register Information [Federal Register: October 1, 2004 (Volume 69, Number 190)] [Page 58826-58828] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-318, A-319, A-320, and A-321 series airplanes

Usa - To provide procedures to the flightcrew to restore operation of these LCD units and prevent prolonged loss of critical flight information to the flightcrew and the consequent reduced ability of the flightcrew to control the airplane during adverse

Airworthiness Directive Federal Register Information [Federal Register: September 30, 2004 (Volume 69, Number 189)] [Page 58251-58253] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 707 and 720 series airplanes

Usa - To prevent stress corrosion cracking of the bolts and wearing of the joint between the lock support fitting and the support link, which could lead to failure of the joint and could cause the collapse of the main landing gear

Airworthiness Directive Federal Register Information [Federal Register: September 30, 2004 (Volume 69, Number 189)] [Page 58256-58257] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Airbus model A-330 and A-340 series airplanes (2004-20-06)

Usa - to provide procedures to the flightcrew to restore operation of these LCD units and prevent prolonged loss of critical flight information to the flightcrew and the consequent reduced ability of the flightcrew to control the airplane during adverse

Airworthiness Directive Federal Register Information [Federal Register: September 30, 2004 (Volume 69, Number 189)] [Page 58253-58256] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, and -315 airplanes

Usa - To prevent reduced aerodynamic smoothness of the wing leading edge de-icer boots and possible reduced stall margin, which could result in a significant increase in stall speeds, leading to a possible stall prior to activation of the stall warning

Airworthiness Directive Federal Register Information [Federal Register: September 29, 2004 (Volume 69, Number 188)] [Page 58043-58047] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 767-200, -300, and -300F series airplanes (2004-19-06)

Usa - To detect and correct fatigue cracking or corrosion of the fail- safe straps, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: September 27, 2004 (Volume 69, Number 186)] [Page 57636-57638] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2004-19-10)

Usa - To prevent failure of the outer and inner hinge pins due to corrosion or cracking, which could allow the pins to migrate out of the joint and result in intermittent movement of the horizontal stabilizer structure and consequent loss of controllabil

Airworthiness Directive Federal Register Information [Federal Register: September 27, 2004 (Volume 69, Number 186)] [Page 57632-57636] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Bombardier model DHC-8-102 airplanes

Usa - To prevent component failure in the radar indicator, resulting in an overcurrent condition and consequent overheating or burning of an internal component or the ribbon cable, which could lead to smoke in the cockpit, resulting in incapacitation of

Airworthiness Directive Federal Register Information [Federal Register: September 22, 2004 (Volume 69, Number 183)] [Page 56682-56683] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

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

Usa - To prevent incorrect operation of the precooler differential pressure switches, which could result in inappropriate automatic shutoff of the engine bleed valve, and consequent inability to perform engine cross-bleed restarts or possible failure of

Airworthiness Directive Federal Register Information [Federal Register: September 22, 2004 (Volume 69, Number 183)] [Page 56676-56679] Header Information DEPARTMENT OF TRANSPORTATION Federal... more