14 C.F.R. § 23.779   Motion and effect of cockpit controls.


Title 14 - Aeronautics and Space


Title 14: Aeronautics and Space
PART 23—AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
Subpart D—Design and Construction
Personnel and Cargo Accommodations

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§ 23.779   Motion and effect of cockpit controls.

Cockpit controls must be designed so that they operate in accordance with the following movement and actuation:

(a) Aerodynamic controls:

                                                  Motion and effect (1) Primary controls:    Aileron...........................  Right (clockwise) for right wing                                         down.    Elevator..........................  Rearward for nose up.    Rudder............................  Right pedal forward for nose                                         right.(2) Secondary controls:    Flaps (or auxiliary lift devices).  Forward or up for flaps up or                                         auxiliary device stowed;                                         rearward or down for flaps down                                         or auxiliary device deployed.    Trim tabs (or equivalent).........  Switch motion or mechanical                                         rotation of control to produce                                         similar rotation of the                                         airplane about an axis parallel                                         to the axis control. Axis of                                         roll trim control may be                                         displaced to accommodate                                         comfortable actuation by the                                         pilot. For single-engine                                         airplanes, direction of pilot's                                         hand movement must be in the                                         same sense as airplane response                                         for rudder trim if only a                                         portion of a rotational element                                         is accessible. 

(b) Powerplant and auxiliary controls:

                                                  Motion and effect (1) Powerplant controls:    Power (thrust) lever..............  Forward to increase forward                                         thrust and rearward to increase                                         rearward thrust.    Propellers........................  Forward to increase rpm.    Mixture...........................  Forward or upward for rich.    Fuel..............................  Forward for open.    Carburetor, air heat or alternate   Forward or upward for cold.     air.    Supercharger......................  Forward or upward for low                                         blower.    Turbosuperchargers................  Forward, upward, or clockwise to                                         increase pressure.    Rotary controls...................  Clockwise from off to full on.(2) Auxiliary controls:    Fuel tank selector................  Right for right tanks, left for                                         left tanks.    Landing gear......................  Down to extend.    Speed brakes......................  Aft to extend. 

[Amdt. 23–33, 51 FR 26656, July 24, 1986, as amended by Amdt. 23–51, 61 FR 5136, Feb. 9, 1996]

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