Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

Page: 69 / 204

Initial issue Page 4-3
4.1 General
This chapter provides checklists and recommended procedures for normal operation of the aircraft. Normal
procedures associated with equipment can be found in the Chapter 9.
The control surfaces do not return to neutral or trimmed position automatically when the control is released.
CAUTION
The ailerons do not return to neutral automatically when the roll
control is released!
CAUTION
The elevator does not return to the precise trimmed position when
the pitch control is released!
The aircraft may not maintain positive longitudinal stability, when
the pitch control is released!
CAUTION
The rudder does not return to neutral automatically when the yaw
control is released!
NOTE
The pitch trim range may be insufficient for the speeds less than
1.5 V
S0
and above V
C
.
4.2 Airspeeds for Normal Operation
Unless stated otherwise, the following speeds are based on maximum takeoff weight 600 kg / 1323 lb.
Takeoff rotation FLAPS 1 65 – 70 IAS 35 – 38 KIAS
Climb
Normal 122 – 127 IAS 66 – 69 KIAS
Best rate of climb
speed
(at sea level)
127 IAS 69 KIAS
Best angle of climb
speed
(at sea level)
100 IAS 54 KIAS
Landing approach FLAPS 1, FLAPS 2 120 – 130 IAS 65 – 70 KIAS
Balked landing Full power ( FLAPS 1 ) 110 – 130 IAS 60 – 70 KIAS
Rough air penetration Maximum 218 IAS 118 KIAS
Demonstrated crosswind velocity
Takeoff 8.3 m/s 16.1 knots
Landing 7.5 m/s 14.6 knots