Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 8-5
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
8.10
After landing
1. Landing light Off
2. Flaps Retract
8.11 Shut down
1. Parking brake Set
2. Radios Off
3. Electrical equipment Off
4. Ignition Off
5. Master switch Off
8.12 Short field takeoff procedure
Flaps 15°
Parking brake Set
Power Full
Brakes Release
Rotate 80 km/h / 44 kts
8.13 Balked landing procedure
Power Full
Flaps 15°
Airspeed 110 km/h / 59 kts
8.14 Information on stalls, spins and other useful pilot information
Stalls
The CTSW exhibits conventional characteristics with a slight buffet at the onset of the
stall. There is no tendency to roll in a coordinated stall. Directional control should be
maintained through use of the rudder.
Recovery is also conventional: release pressure on the control stick to reduce the angle
of attack. Apply full power, and slowly recover.
Spins
The CTSW is not certified for spins.
In the event of an unintentional spin:
1. Reduce power to idle
2. Center the ailerons
3. Apply rudder in the opposite direction of rotation
4. When the rotation stops, smoothly recover from the resultant dive.
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