Aircraft › Diamond › Diamond DA20 › Diamond DA20-C1
Diamond DA20-C1
The FAA approved the DA20-C1 in April 1998 in the utility category, a two-seat airplane built by Diamond Aircraft Industries in Canada. A Continental IO-240-B engine of 125 horsepower turns a propeller about 69 inches, or 1.75 meters, across. The maximum take-off weight is 1,764 lb, or 800 kg, and the tank holds 24 US gallons, or 91 litres, of usable fuel on airplanes from serial number C0014. The earlier DA20-A1 Katana, with a Rotax 912 engine, is on the same data sheet. No acceptable source read gives its dimensions or speeds, so this page has no drawing.
- Seats
- About 2
- Engines
- One piston engine in the nose: Continental IO-240-B
- Max takeoff weight
- 1,800 lb (800 kg)
Photos from members
No member photos of this aircraft yet. Be the first to add one.
Specifications
| Fuel capacity | 20 US gal (91 L) |
|---|---|
| Status | Still flying with a few operators |
| Type codes | ICAO DV20 |