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  2. Aircraft engine controls - Wikipedia

    en.wikipedia.org/wiki/Aircraft_engine_controls

    Therefore, the pilot has to pay attention to the RPM indicator and adjust the throttle/power lever in order to maintain the desired constant speed of the propeller. For example, when the airspeed reduces and the loading increases (e.g., in a climb), RPM will decrease and the pilot has to increase the throttle/power.

  3. Helicopter flight controls - Wikipedia

    en.wikipedia.org/wiki/Helicopter_flight_controls

    Helicopter rotors are designed to operate at a specific rotational speed. The throttle controls the power of the engine, which is connected to the rotor by a transmission. The throttle setting must maintain enough engine power to keep the rotor speed within the limits where the rotor produces enough lift for flight.

  4. Thrust lever - Wikipedia

    en.wikipedia.org/wiki/Thrust_lever

    Thrust levers in a Boeing 747 Classic. The center and rear levers are used during flight, while the forward levers control reverse thrust.. Thrust levers or throttle levers are found in the cockpit of aircraft, and are used by the pilot, copilot, flight engineer, or autopilot to control the thrust output of the aircraft's engines, by controlling the fuel flow to those engines. [1]

  5. Autothrottle - Wikipedia

    en.wikipedia.org/wiki/Autothrottle

    Thrust levers of an A320 set to the autothrust position during cruise flight. An autothrottle (automatic throttle, also known as autothrust, A/T or A/THR) is a system that allows a pilot to control the power setting of an aircraft's engines by specifying a desired flight characteristic, rather than manually controlling the fuel flow.

  6. ATA 100 - Wikipedia

    en.wikipedia.org/wiki/ATA_100

    ATA 100 contains the reference to the ATA numbering system which is a common referencing standard for commercial aircraft documentation. This commonality permits greater ease of learning and understanding for pilots, aircraft maintenance technicians, and engineers alike.

  7. Tecnam P2004 Bravo - Wikipedia

    en.wikipedia.org/wiki/Tecnam_P2004_Bravo

    Data from Jane's All the World's Aircraft 2010-11 General characteristics Crew: 1 Capacity: 3 pax Length: 6.61 m (21 ft 8 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.6 m (8 ft 6 in) Wing area: 11 m 2 (120 sq ft) Empty weight: 336 kg (741 lb) Max takeoff weight: 600 kg (1,323 lb) Max useful weight: 269 kg (593 lb) Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston ...

  8. Engine order telegraph - Wikipedia

    en.wikipedia.org/wiki/Engine_order_telegraph

    On most modern vessels with direct combustion engines or electric propulsors, the main control handle on the bridge acts as a direct throttle with no intervening engine room personnel. As such, it is regarded under the rules of marine classification societies as a remote control device rather than an EOT, though it is still often referred to by ...

  9. Electronic throttle control - Wikipedia

    en.wikipedia.org/wiki/Electronic_throttle_control

    Instead, the position of the throttle valve (i.e., the amount of air in the engine) is fully controlled by the ETC software via the electric motor. But just opening or closing the throttle valve by sending a new signal to the electric motor is an open loop condition and leads to inaccurate control.