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Civil aviation

10,840 news found

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

Civil aviationFAA AD on Boeing model 747-100, -100B, 100B SUD, -200B, -200C, -200F, and -300 series airplanes; and model 747SP and 747SR series airplanes (2005-08-01)

Washington, Usa - To detect and correct fatigue cracks in the body frames, skin and other internal structure in fuselage section 41, which could lead to rapid decompression and loss of the structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18290-18294] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Boeing model 777-200 and -300 series airplanes equipped with Rolls Royce model RB-211 Trent 800 engines (2005-07-24)

Washington, Usa - To prevent failure of a thrust reverser and adjacent components and their consequent separation from the airplane, which could result in a rejected takeoff (RTO) and cause asymmetric thrust and consequent loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18285-18287] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Saab model Saab 2000 series airplanes

Washington, Usa - To prevent a broken terminal stud on the main relay of an electrical power generator, which could reduce the redundancy of electrical power systems, result in increased pilot workload, and contribute to reduced controllability of the ai

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18275-18277] Header Information DEPARTMENT OF TRANSPORTATION Federal... more

Civil aviationFAA AD on Dassault model Falcon 10 series airplanes

Washington, Usa - To prevent collapse of the flexible hoses in the wing anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 11, 2005 (Volume 70, Number 68)] [Page 18282-18285] Header Information DEPARTMENT OF TRANSPORTATION Federal... more