(b)
Powerplant and auxiliary controls :
(1)Primary Controls Motion and e.ect
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) Forwardor upfor .aps up or auxiliarydevice stowed; rearward or down for .aps down or auxiliary device deployed.
Trim tabs (or equiva-lent) Switch motion or mechanical rotation or control to produce similar rotation ofthe airplane aboutan axis parallel to the axis control. Axis of roll trim control may be displaced to accommodate comfortable ac-tuation by the pilot. For single-engine airplanes, di-rection ofpilot’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.
(1)Powerplant Controls Motion and e.ect
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 air Forward or upward for cold.
Supercharger Forward or upward for low blower.
Turbo-superchargers Forward, upward, or clockwise to increase pressure.
Rotary controls Clockwise from o. 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. 23-51, E.. 03/11/96
FAR 23.781 : Cockpit control knob shape.
(a) [Flapandlandinggear] controlknobs must conformtothegeneral shapes(but not necessarily the exact sizes or speci.c proportions) in the following .gure (Figure 31.1, p. 329) :
Landing gear control knob
Fig. 31.1 – Control Knob
(b) [Powerplant controlknobs must conformtothegeneralshapes(but not necessarily the exact sizes of speci.c proportions) in the following .gure (Figure 31.2, p. 330):]
Amdt. 23-33, E.. 08/11/86
′
Elodie Roux. Septembre 2003
Subpart D : Design and Construction
Panel.
Quadrant.
mounted
mounted
Power or thrust control knob.
RPM control knob.
Mixture control knob.
Carb heat or alternate air control knob.
Supercharger control knob.
Fig. 31.2 – Control Knob
FAR 23.783 : Doors.
(a)
Each closed cabin with passenger accommodations must have at least one adequate and easily accessible external door.
(b)
[Passengerdoors mustnotbelocated with respect to anypropellerdisk or any other potentialhazard so asto endangerpersons using thedoor.]
(c)
Each externalpassenger or crewdoor must comply with the following requirements :
(1)
There must be a means to lock and safeguard the door against inadvertent openingduring.ightbypersons,by cargo,orasaresult of mechanicalfailure.
(2)
The door must be openable from the inside and the outside when the internal locking mechanism is in the locked position.
(3)
There must be a means of opening which is simple and obvious and is arran-ged and marked inside and outside so that the door can be readily located, unlocked, and opened, even in darkness.
(4)
The door must meet the marking requirements of Sec. 23.811 of this part.
