DIMENSIONS
|
|
ft
|
m
|
|
Wing span
|
|
27.17
|
8.28
|
Aspect ratio
|
|
7.00
|
|
Overall length
|
|
19.17
|
5.84
|
Overall height (Monowheel)
|
|
4.33
|
1.32
|
Overall height (Tri-Gear)
|
|
7.00
|
2.13
|
|
|
ft³
|
m³
|
Baggage space
|
|
22.50
|
.64
|
|
|
|
|
WEIGHTS
AND LOADING
|
|
lb
|
kg
|
Empty weight (typically equipped)
|
Monowheel
|
750
|
340
|
|
Tri-gear
|
780
|
354
|
Max Take-off weight*
|
Monowheel
|
1370
|
623
|
|
Tri-gear
|
1370
|
623
|
Useful load
|
Monowheel
|
620
|
281
|
|
Tri-gear
|
590
|
268
|
Wing area
|
|
102ft²
|
9.48m²
|
Wing loading at max T.O.W.
|
|
13.43lb/ft²
|
66kg/m²
|
Power loading (Rotax 912S)
|
|
13.70lb/hp
|
8.4kg/kw
|
g loading
|
|
Design
|
Ultimate
|
|
|
+3.80/
-1.90
|
+8.55/
-4.27
|
|
|
|
|
PERFORMANCE
(1,370lb)
|
|
mph
|
kts
|
kph
|
Stall speed flaps extended
|
|
51
|
44
|
81
|
Stall speed clean
|
|
57
|
49
|
90
|
Cruise speed 8000ft 75% pwr
(Rotax 912S)(TAS)
|
Mono Wheel
|
161
|
140
|
259
|
|
Tri-gear
|
155
|
135
|
250
|
Max Cruise speed
10,000ft (Rotax 914 turbo)(TAS)
|
Mono Wheel
|
200
|
174
|
322
|
|
Tri-gear
|
191
|
166
|
307
|
Rate of Climb at 1370 lb gross weight
(Rotax 912S)
|
|
1000fpm
|
5.1m per sec
|
Rate of Climb at 1370 lb gross weight
(Rotax 914 turbo)
|
|
1300fpm
|
6.6m per sec
|
|
|
ft
|
m
|
|
Take-off
ground roll at gross weight (Rotax 912S)
|
|
590
|
180
|
Take-off ground roll at gross
weight (Rotax 914 turbo)
|
|
500
|
153
|
Landing roll
|
|
600
|
184
|
|
|
imp gal
|
us gal
|
litres
|
Max fuel (standard)
|
|
15
|
18
|
70
|
Max fuel (with aux tank)
|
|
23
|
28
|
105
|
|
|
imp
gal/hr
|
ltr/hr
|
|
Fuel
consumption at economy cruise 95-100 kts (Rotax 912)
|
|
2
|
9
|
|
|
nm
|
km
|
sm
|
Range at economy cruise
|
Standard tanks
|
732
|
1355
|
841
|
|
Aux tanks
|
1093
|
2023
|
1256
|