The CH 650 is a low-wing design in the Chris Heintz kit-aircraft family. The manufacturer publishes performance for different engine installations, retained separately in the tables below.
About the CH 650
The manufacturer advertises this aircraft in its kit range. This records a public listing; stock, delivery and regional kit options are not confirmed.
Chris Heintz designs across the CH high-wing and low-wing kit families.
Specifications
| Seats | Not recorded |
|---|---|
| Wingspan | Not recorded |
| Wing area | Not recorded |
| Length | Not recorded |
| Height | Not recorded |
| Cabin width | Not recorded |
| Cabin height | Not recorded |
| Empty weight | Not recorded |
| Gross weight | Not recorded |
| Design gross weight | Not recorded |
| Useful load | Not recorded |
| Useful load, published minimum | Not recorded |
| Useful load, published maximum | Not recorded |
| Fuel capacity | Not recorded |
| Optional fuel capacity | Not recorded |
| Baggage capacity | Not recorded |
| Engine power | Not recorded |
| Suitable power, minimum | Not recorded |
| Suitable power, maximum | Not recorded |
| Published average build time | Not recorded |
| Build time, minimum | Not recorded |
| Build time, maximum | Not recorded |
Performance
| Top speed | Not recorded |
|---|---|
| Cruise speed | Not recorded |
| Economy cruise speed | Not recorded |
| Stall speed | Not recorded |
| Stall speed, clean | Not recorded |
| Never exceed speed | Not recorded |
| Rate of climb | Not recorded |
| Takeoff ground roll | Not recorded |
| Takeoff distance, obstacle basis unspecified | Not recorded |
| Landing ground roll | Not recorded |
| Landing distance, obstacle basis unspecified | Not recorded |
| Ceiling | Not recorded |
| Range | Not recorded |
| Endurance | Not recorded |
Source notes & conditions
- Specification columns publish 1,320 lb gross weight; the performance preface states 1,300 lb. This source discrepancy is preserved in configuration conditions.
- Published useful-load values are transcribed as printed, even where they do not equal gross minus empty weight.
- Cruise numeric field uses the source 75%-power, 8,000-ft TAS row; sea-level maximum-cruise figures are retained in raw notes.