Navigate / EASA

CS-VLA 779  Motion and effect of cockpit controls

ED Decision 2003/18/RM

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 aeroplane about an axis parallel to the axis control. Axis of roll trim control may be displaced to accommodate comfortable actuation by the pilot. Direction of pilot’s hand movement must be in the same sense as aeroplane 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.

 

Carburettor, air heat or alternate air.

Forward or upward for cold.

 

Super charger.

Forward or upward for low blower.

 

Turbosuper-chargers.

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.