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  2. Flight control surfaces - Wikipedia

    en.wikipedia.org/wiki/Flight_control_surfaces

    The rudder is a fundamental control surface which is typically controlled by pedals rather than at the stick. It is the primary means of controlling yaw—the rotation of an airplane about its vertical axis. The rudder may also be called upon to counter-act the adverse yaw produced by the roll-control surfaces.

  3. Rudder pedal - Wikipedia

    en.wikipedia.org/wiki/Rudder_pedal

    Green pedals in the floor of a Polikarpov I-15. A rudder pedal is a foot-operated aircraft flight control interface for controlling the rudder of an aircraft. [1] [2] The usual set-up in modern aircraft is that each pilot has a pedal set consisting of a pair of pedals, with one pedal for each foot. Each right and left pedal works together so ...

  4. Aircraft flight control system - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_control_system

    Rudder pedals, or the earlier, pre-1919 "rudder bar", control yaw by moving the rudder; the left foot forward will move the rudder left for instance. Thrust lever or throttle, which controls engine speed or thrust for powered aircraft. The control yokes also vary greatly among aircraft. There are yokes where roll is controlled by rotating the ...

  5. NTSB probing ‘stuck’ control incident on Boeing 737 Max

    www.aol.com/ntsb-probing-stuck-control-incident...

    In a newly-released preliminary report of the February 6 incident, the National Transportation Safety board says the pilots of the Boeing 737 Max 8 “experienced ‘stuck’ rudder pedals during ...

  6. Another Boeing Max mishap: NTSB probes 'stuck' rudder pedals ...

    www.aol.com/news/another-boeing-max-mishap-ntsb...

    The rudder pedal system on the aircraft is identical to that of the 737 NG. Boeing said it was aware of two similar past occurrences on the 737 NG model, both in 2019, which were resolved with ...

  7. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    Yawing generates side forces due to incidence at the rudder, fin and fuselage. N β {\displaystyle N_{\beta }} Yawing moment due to sideslip forces. Sideslip in the absence of rudder input causes incidence on the fuselage and empennage , thus creating a yawing moment counteracted only by the directional stiffness which would tend to point the ...

  8. Investigation underway into rare, unsafe airliner roll ...

    www.aol.com/investigation-underway-rare-unsafe...

    “Then you stomp on a rudder pedal really hard to try to initiate [the roll] in the simulator,” Bangs said. To get out of a Dutch roll, pilots can slow the aircraft and descend to thicker air.

  9. Yoke (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Yoke_(aeronautics)

    Collection of control yokes at Boeing Future of Flight Museum: 747, 707, B-29, Trimotor.The former two yokes are W-shaped, while the latter two are circular. The cockpit of Concorde, which has an M-shaped yoke mounted on a control column The cockpit of an Embraer ERJ with an M-shaped yoke "W"/"U" style yoke in a Cessna 152 light aircraft, mounted on a horizontal tube protruding from the ...

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