The General Electric CF6, US military designations F103 and F138, is a family of high-bypass turbofan engines produced by GE Aviation. Based on the TF39, the first high-power high-bypass jet engine, the CF6 powers a wide variety of civilian airliners. The basic engine core also powers the LM2500 and LM6000 marine … See more After developing the TF39 for the C-5 Galaxy in the late 1960s, GE offered a more powerful variant for civilian use, the CF6, and quickly found interest in two designs being offered for a recent Eastern Airlines contract, … See more • Airbus A300/Airbus Beluga • Airbus A310/Airbus A310 MRTT/Airbus CC-150 Polaris • Airbus A330/Airbus A330 MRTT/EADS/Northrop Grumman KC-45 See more Related development • General Electric GE90 • General Electric TF39 See more CF6-6 The CF6-6 was a development of the military TF39. It was first used on the McDonnell Douglas DC-10-10. This initial version … See more In 1973, a CF6-6 fan assembly disintegrated, resulting in the loss of cabin pressurization of National Airlines Flight 27 over See more • Official website • "CF6-80C2 engine history and evolution" (PDF). The Engine Yearbook. 2007. • Stephen Trimble (21 Dec 2010). "General Electric celebrates 25th anniversary of best-selling widebody engine" See more http://www.fi-powerweb.com/Engine/General-Electric-CF6.html
CF6-80E1 Datasheet - Home GE Aviation
WebSummary report for CF6 jet engine diagnostics program Cockpit cruise recordings and test cell data in conjunction with hardware inspection results from airline overhaul shops were … WebMar 30, 2024 · For service information identified in this SNPRM, contact General Electric Company, GE Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215; phone: 513-552-3272; email: [email protected]. You may view this service information at the FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA. nike slippers official website
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WebOct 27, 2015 · ENGINE DATAIntake efficiency = 0.980Fan polytropic efficiency = 0.930Compressor polytropic efficiency = 0.910Turbine polytropic efficiency = 0.930Isentropic nozzle efficiency = 0.950Mechanical efficiency = 0.990Combustion pressure loss (ratio) = 0.050Fuel combustion efficiency = 0.990 Area of hot nozzle = 1.0111 m2Area of cold … WebMar 28, 2003 · General Electric CF6: The Engine: Specifications (CF6-50) The CF6 high-bypass turbofan was based on the TF39 and was designed to power the McDonnell … WebDec 8, 2024 · The FAA proposes to supersede Airworthiness Directive (AD) 2012-02-07, which applies to certain General Electric Company (GE) CF6-45 and CF6-50 series model turbofan engines with a specified low-pressure turbine (LPT) rotor stage 3 disk installed. ntf pll