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  2. Airbus Industrie Flight 129 - Wikipedia

    en.wikipedia.org/wiki/Airbus_Industrie_Flight_129

    The last test flown was to certify the plane's takeoff capability with a single engine failure. [1] It was the first fatal accident involving an Airbus A330 as well as the first hull loss of the type. [3] It remained the only fatal accident involving an A330 until the crash of Air France Flight 447 on 1 June 2009. [3]

  3. Flex temp - Wikipedia

    en.wikipedia.org/wiki/Flex_temp

    The particular take-off distance required may be shorter than the available runway length. In this case a lower thrust may be used. Lower thrust settings increase engine life and reduce maintenance costs. The take-off thrust available from a civil engine is a constant value up to a particular ambient temperature.

  4. Why high temperatures can make planes too heavy to take off - AOL

    www.aol.com/why-high-temperatures-planes-too...

    The team then put those temperatures and headwinds into an aircraft takeoff performance calculator for a variety of different aircraft types, including the Airbus A320 – one of the most popular ...

  5. Takeoff Acceleration Monitoring System - Wikipedia

    en.wikipedia.org/wiki/Takeoff_Acceleration...

    A Takeoff Acceleration Monitoring System automates the pilot monitoring of Distance to Go (DTG), "to sense, in a timely fashion the development of insufficient acceleration, which would extend the takeoff roll, perhaps precipitously". [1] Over the years, recommendations have been made to develop a Take Off Performance Management System.

  6. Rolls-Royce Trent 7000 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Trent_7000

    At take-off, the fan displaces up to 1.3 t (2,900 lb) of air per second, the jet nozzle velocity is almost 1,000 mph (450 m/s) and each high pressure turbine blade generates around 800 hp (600 kW), rotating at 12,500 rpm with their tips reaching 1,200 mph (540 m/s). [6] Rolls-Royce reports the engine is 10 dB quieter than the Trent 700. [11]

  7. Fuel fraction - Wikipedia

    en.wikipedia.org/wiki/Fuel_fraction

    With a fuel fraction of nearly 85%, the GlobalFlyer could carry 5 times its weight in fuel.. In aerospace engineering, an aircraft's fuel fraction, fuel weight fraction, [1] or a spacecraft's propellant fraction, is the weight of the fuel or propellant divided by the gross take-off weight of the craft (including propellant): [2]

  8. Takeoff/go-around switch - Wikipedia

    en.wikipedia.org/wiki/Takeoff/go-around_switch

    A takeoff/go-around switch (TO/GA; / ˈ t oʊ ɡ ə /) is a switch on the autothrottle of modern large aircraft, with two modes: takeoff (TO) and go-around (GA). The mode is dependent on the phase of flight; usually, on approach to land, the autopilot will be set to approach mode, therefore if the TO/GA switch is pressed it will activate the go-around mode of the autothrottle (about 90–92% ...

  9. Maximum takeoff weight - Wikipedia

    en.wikipedia.org/wiki/Maximum_takeoff_weight

    The maximum takeoff weight (MTOW) or maximum gross takeoff weight (MGTOW) or maximum takeoff mass (MTOM) of an aircraft, also known as the maximum structural takeoff weight or maximum structural takeoff mass, [1] is the maximum weight at which the pilot is allowed to attempt to take off, due to structural or other limits.