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This airplane is a new HPA design. Several versions are planned
for production by different landing gear systems and engines.
Technical Data:
| Top speed |
265 mph |
426 km/h |
230 kts |
| Cruise speed @ 75% power |
240 mph |
386 km/h |
210 kts |
| Stall speed |
50 mph |
80 km/h |
43,5 kts |
| Range @ 55% power |
1265 mi |
2035 km |
1100 nm |
| Rate of climb @ sea level |
3500 fpm |
17 m/s |
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| Take off run distance |
300 ft |
100m |
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| Ground roll distance |
700 ft |
220 m |
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| Power range |
150 - 330+ hp |
110 - 242+ kW |
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| Fuel cpacity |
60 US gals |
227 l |
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| Empty weight |
1300 lbs |
590 kg |
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| Gross weight |
2100 lbs |
953 kg |
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| Length |
21 ft |
6,40 m |
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| Span |
26,9 ft |
8,20 m |
| Wing area |
110 sq ft |
10,25 m³ |
| No. of seats |
2 |
2 |
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| Cockpit width |
45" |
1,14 m |
| Engine used |
Lycoming IO-540 (parallel valve type) |
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| Landing gear |
Taildragger or Tricycle |
Measures in ft/mm |
| Construction materials |
Metal structure and surface with various metal
fairlings |
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