Aerospool WT-9 Dynamic - Climb Performance; Landing Distance; Stall Speed; Take-Off Performance

WT-9 Dynamic Club S FLIGHT MANUAL Section 5 Page 5-
2
5.2.2 Stall speed
Maximum weight 472,5 kg, C.G. in 25% MAC, idle engine speed
Position wing flaps
0°
°°
° 15°
°°
° 38°
°°
°
Stall speed IAS in km/h 60 55 50
Stall speed CAS in km/h 72 70 65
5.2.3 Take-off performance
The data is valid for following conditions: H = 260 m MSL, Temperature t = 15 ° C
Wing flaps position 15° and engine ROTAX 912 ULS
Surface of the
runway
Take-off run
distance
( m )
Take-off distance up
to 15m
( m )
Paved runway 95 264
Non paved – grass 116 285
5.2.4 Landing distance
The data is valid for following conditions: H = 260 m MSL, Temperature t = 15 ° C
Wing flaps position 38° , landing roll is braked.
Surface of the
runway
Landing distance (m)
from height 15 m
Landing roll
distance ( m )
Paved runway 267 152
Non paved - grass 272 144
5.2.5 Climb performance
The data is valid for max.weight 480 kg , without flaps.
Engine ROTAX 912 ULS, speed 5500 r.p.m
Propeller MTV-21A
Altitude (m) Speed IAS km/h
Rate of climb m/s
0 120 5,2
1000 120 4,9
2000 120 4,2
The service ceiling is 5500 m for models equipped by engine ROTAX 912 ULS at the
max. continuous power.
Date: 1.12.2001 „Appr“