Aerospool WT9 Dynamic LSA / Club, Pilot Operating Handbook

Page: 104 / 204

Page 5-10 EASA Approved Initial issue
5.6 Cruise Performance and Fuel Consumption
Associated conditions: Example:
Weight 600 kg / 1323 lb Cruise pressure altitude
6000 ft
Flaps FLAPS 0 (0°) Engine speed 5000 rpm
Winds Zero
Airspeed
187 IAS / 183 CAS / 200 TAS
MAP
21.3 inHg
Fuel consumption
16.4 l/h
4.33 U. S. gal/h
Pressure
altitude
Engine
speed
Airspeed MAP Fuel consumption
ft rpm IAS CAS TAS inHg (l/h) U. S. gal/h
2000
4 300 165 163 172 21.6 14.5 3.83
4 500 175 172 183 22.4 15.5 4.10
4 800 190 185 196 23.5 17.2 4.54
5 000 200 194 206 24.2 18.5 4.89
5 500 223 215 228 25.8 21.3 5.63
5 800 232 224 237 26.7 23.3 6.16
4000
4 300 160 158 168 20.5 13.6 3.59
4 500 170 167 176 22.2 14.5 3.83
4 800 184 180 191 22.2 16.3 4.31
5 000 194 189 200 22.8 17.4 4.60
5 500 216 209 222 24.4 20.4 5.39
5 800 226 218 232 25.2 22.0 5.81
6000
4 300 153 153 167 19.2 12.6 3.33
4 500 163 161 176 19.8 13.7 3.62
4 800 178 175 191 20.7 15.3 4.04
5 000 187 183 200 21.3 16.4 4.33
5 500 211 204 222 22.6 19.0 5.02
5 800 221 213 233 23.3 20.5 5.42
8000
4 300 145 146 157 18.3 11.8 3.12
4 500 155 156 176 18.8 12.8 3.38
4 800 172 169 191 19.6 14.2 3.75
5 000 181 177 200 20.1 15.3 4.04
5 500 201 195 220 21.4 18.0 4.76
5 720 212 205 231 22.0 19.3 5.10
10000
4 300 138 140 163 17.3 11.2 2.96
4 500 147 148 172 17.7 12.0 3.17
4 800 163 161 187 18.4 13.4 3.54
5 000 172 169 196 18.8 14.3 3.78
5 500 192 187 218 19.9 16.9 4.46
5 660 202 196 228 20.5 18.4 4.86