WT-9 Dynamic Club S FLIGHT MANUAL Section 4 Page 4-
4.5.9. Descending
Descending is conducted at airspeeds 110 – 120 km/h with the throttle lever set to
idle position. For increasing the rate of descent it is recommended wing flaps set to
landing position ( 35° flaps deflection ) and proceed at airspeed 120 km/h. In this
configuration the gliding range is 1:8.
Side slipping is conducted with airspeed 120 km/h, and bank angle 30° with help of
the full rudder deflection. The side slip direction is controlled by the bank.
4.5.10 Landing
Check systems of a fuel before approach for landing. Landing approach conduct at
small glide slope angle due to long distance of the float before aeroplane touch-down
1. Propeller - set minimum fine angle ( take off position )
2. Fuel pump - switched on
3. Approach speed 110-120 km/h according to the weight.
4. Wing flaps - as required flaps down at speed below 135 km/h
5. Elevator trim – adjust as required
6. Begin levelling out at height circa 2-3 m.
7. Actual touchdown should be made with power-idle and on the main wheels
first. The nose wheel should be lowered smoothly to the runway as speed is
diminished.
8. During landing run control the aeroplane with help of the rudder pedals.
9. Apply braking as required. The main wheel brakes are actuated via the
handle on the pedestal between the pilot seats.
4.5.11 Balked landing
1. Smoothly adjust the throttle lever – full open ( a thrust yawing moment is
manifested in case of the steep setting of the throttle lever )
2. Airspeed modify to 120 km/h
3. The wing flaps setting reduced to take-off position
4. Elevator trim – adjust as required and proceed in the climb out
Date: 1.12.2001 „Appr“
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