1 / 3
The RV-10 is a four-seat aircraft in Van’s RV kit family. Its published data covers separate gross-weight and light-weight configurations, with space, useful load and cross-country performance central to the design.
About the RV-10
The manufacturer advertises this aircraft in its kit range. This records a public listing; stock, delivery and regional kit options are not confirmed.
The RV family, from early homebuilding landmarks to today’s kit range.
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
- The source has separate gross-weight and light-weight performance columns. The light-weight test mass is not stated; it is not treated as a gross-weight result.
- The brochure repeats the 75%-power label on its second light-weight cruise row (180 mph). That ambiguous row is not imported as an economy-cruise measurement.
- Maximum useful load is published as a 1,050-1,100 lb range. No single numeric useful_load_lb is assigned.
- The brochure gives takeoff and landing distances without an obstacle-height definition. They are not relabeled as ground rolls.
- Engine power range is 210-260 hp; the narrative describes a 260 hp IO-540. The performance tables do not explicitly assign a tested engine power.
- The linked file is the source provided in the user reference tab; source URL path is not treated as its publication date.