| TECHNICAL
SPECIFICATIONS |
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| Wing
span |
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32
ft 0 in |
| Wing
area |
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|
117,3
sq ft |
| Wing
loading |
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|
11,3
lbs/sq ft |
| Aspect
ratio |
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8,7 |
| Length |
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19
ft 11 in |
| Fin
height |
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8
ft 6 in |
| Cabin
width at hips |
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40
in |
| Cabin
width at elbows |
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46
in |
| Cabin
headroom |
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41
in |
| Design
gross weight (amateur-built) |
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1320
lbs |
| Gross
weight (ultralight or sportplane) |
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1232
lbs |
| Dry
empty weight |
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|
720-750
lbs |
| Baggage
capacity |
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50-60
lbs |
| Fuel
capacity |
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23
USG |
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PERFORMANCE
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| Engine |
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Rotax
912S |
| Horsepower |
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98
HP |
| Never
exceed speed |
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|
135
kts |
| Cruise
speed, 75% at 6500 ft |
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115
kts |
| Cruise
speed, 65% at 6500 ft |
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110
kts |
| Maximum
range (65%, no reserve) |
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700
s.m. |
| Rate
of climb, sea level |
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1350
fpm |
| Service
ceiling |
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16,000
ft |
| Stall
speed (flaps up) C.A.S. |
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45
kts |
| Stall
speed (flaps down) C.A.S. |
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39
kts |
| Take-off
ground run |
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|
300-400
ft |
| Take-off,
over 50 ft obstacle |
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|
500
ft |
| Fuel
consumption (65%) |
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|
4.1
gph |
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