(iii)	The front rudder control can be disconnected
		by removing the retaining split pins and dis-
		connecting the rod (38) to the rear rudder bar.
		
	(iv)	The rudder pedals (35) in both cockpits are adjust-
	        able for leg length by removing the safety
	        locking pins.
		
  6.  Control Locks 

	(i)	Provision is made in the rear cockpit for a jig
		which locks the elevators and ailerons in the
		central position.

	(ii)	The rudder is locked by a V shaped wedge
		placed between the fin and the rudder.
				  
  7.  Elevator and Rudder Trim

	(i)	Longitudinal trimming is effected by spring
	        loading the elevators.   The required tension is
	        obtained by a lever and quadrant situated on
	        the left of each cockpit.   These trimming springs (39)
	        are both adjustable for tension in the rear cock-
	        pit.
	        
	(ii)	Directional trimming is assisted by a tension
	        spring (32) fitted to the rudder bar on the right
	        hand side of the rear cockpit.   This spring
	        should be adjusted so that no pressure is re-
	        quired on either rudder pedal when the engine
	        is operating at cruising R.P.M.
				  
  8.  Automatic Slots 

	(i)	Auto slots (7) are fitted to the top mainplanes
	        and are provided with a locking gear.   The
	        operating lever and quadrant are situated on
	        the right hand side of the rear cockpit below
	        the instrument panel.
	        
	(ii)	The operating lever (33) should be near the rear-
	        most position when the slots are locked.   With
	        the lever in the forward position the slots should
	        be quite free.