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Cruise Speed Performance:
| RPM | HP | % Power | Airspeed - Aircraft 1 | Airspeed - Aircraft 2 |
| 5000 | 52 | 81 | 69 | 73 |
| 5200 | 54 | 84 | 73 | 77 |
| 5400 | 55 | 87 | 80 | 81 |
| 5600 | 57 | 90 | 83 | 86 |
| 5800 | 59 | 93 | 87 | 90 |
| 5950 | 60 | 96 | 90 | 92 |
| Stall | 36 | 30 |
Climb Performance:
| Airspeed | FPM | FPM |
| 70 | 400 | 500 |
| 60 | 600 | 700 |
| 55 | 700 - 900 | 900 - 1,000 |
| 1. Flight conditions:
Aircraft 1: 1,100 MSL, 79 degrees, 733 lbs gross weight. CG at 85.46" (almost exactly at the middle of the 80"-90" CG range). CH-II Special (without wheel fairings). Aircraft 2: 1,100 MSL, 63 degrees, 731 lbs gross weight. CG at 85.32" (almost exactly at the middle of the 80"-90" CG range). CH-II Special (with wheel fairings). 2. Warp Drive 3 Blade Carbon Fiber Prop, 64" diameter. 3. Performance numbers listed are indicated airspeeds, in MPH. 4. Performance tests on aircraft 1 were conducted without wheel fairings or main gear leg fairings (installation of same typically adds 2-3 MPH). 5. HP and % power specifications derived from HKS data. |
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