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Civil aviation

11,047 news found

Civil aviationFAA AD on Eurocopter France model EC-120 helicopters

Washington, Usa - To detect incorrect positioning of the drive shaft half-clamps, and to prevent interference of the half-clamps with the drive shaft, which could result in scoring on the drive shaft, failure of the drive shaft, and subsequent loss of co

Airworthiness Directive Federal Register Information [Federal Register: May 9, 2005 (Volume 70, Number 88)] [Page 24304-24305] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA AD on Kelly Aerospace Power Systems Part Number (P/N) 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, C23D04, or P23D04 Fuel Regulator Shutoff Valves

Washington, Usa - To prevent failure of the fuel regulator shutoff valve, which could result in fuel leakage in aircraft with these combustion heaters

Airworthiness Directive Federal Register Information [Federal Register: May 6, 2005 (Volume 70, Number 87)] [Page 23930-23934] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA (Correction) AD on General Electric Company (GE) CF6-80A1/ A3 and CF6-80C2A series turbofan engines, installed on Airbus Industrie A-300/600 and A-310 series airplanes

Washington, Usa - To prevent inadvertent thrust reverser deployment, which, if it occurs in-flight, could result in loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: May 5, 2005 (Volume 70, Number 86)] [Page 23783] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation... more

Civil aviationFAA (Correction) AD on Boeing model 737-300, -400, and -500 series airplanes modified in accordance with Supplemental Type Certificate (STC) ST00127BO

Washington, Usa - To prevent unsafe levels of current or energy from entering the fuel tank, due to hot short faults or threat conditions associated with the safe side harness assembly, which could result in a fire or explosion of the fuel tank

Airworthiness Directive Federal Register Information [Federal Register: April 28, 2005 (Volume 70, Number 81)] [Page 21924] Header Information DEPARTMENT OF TRANSPORTATION Federal... 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 MD-88 Airplanes

Washington, Usa - To prevent fatigue cracking of the MLG pistons, which could result in failure of the pistons and consequent damage to the airplane structure or injury to airplane occupants

Airworthiness Directive Federal Register Information [Federal Register: April 28, 2005 (Volume 70, Number 81)] [Page 21924-21927] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747 series airplanes (2005-09-02)

Washington, Usa - To detect and correct fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 25, 2005 (Volume 70, Number 78)] [Page 21141-21144] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 707 airplanes and model 720 and 720B series airplanes (2005-08-15)

Washington, Usa - To detect and correct this cracking, which could result in reduced structural integrity of the engine nacelle, and consequent separation of an engine from the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 25, 2005 (Volume 70, Number 78)] [Page 21136-21137] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on McDonnell Douglas model DC-8-33 and -43; DC-8F-54 and DC-8F-55; DC-8-50, - 60, -60F, -70, and -70F series airplanes

Washington, Usa - To detect and correct cross-wired electrical connectors of the fire extinguishing system, which could release fire extinguishing agent into the incorrect engine nacelle in the event of an engine fire

Airworthiness Directive Federal Register Information [Federal Register: April 21, 2005 (Volume 70, Number 76)] [Page 20713-20715] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 747-200B, -200C, -200F, and -400F series airplanes (2005-08-09)

Washington, Usa - To find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20273-20275] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 737-600, -700, and -800 series airplanes (2005-08-10)

Washington, Usa - To prevent flammable fluid (such as fuel or hydraulic fluid) from leaking onto a hot engine exhaust nozzle or into the engine core fire zone, and consequently causing an uncontrolled fire or explosion

Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20275-20276] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Cessna model 680 airplanes

Washington, Usa - To prevent a simultaneous loss of data from all four cockpit display units, and loss of primary navigation instruments, autopilot, flight director, master caution/ warning lights, aural warnings, global positioning system position infor

Airworthiness Directive Federal Register Information [Federal Register: April 14, 2005 (Volume 70, Number 71)] [Page 19682-19685] Header Information DEPARTMENT OF TRANSPORTATION Federal... more