Power Plant
| DA20i Katana | DA20-C1 | |
|---|---|---|
| Engine | (BRP-Powertrain) Rotax 912 iSc3 Sport with 100 hp | 125 hp Continental IO-240-B32B engine |
| Propeller | MT propeller MTV-21-A/175-05, 2-blade constant speed propeller | Sensenich 2 blade fixed pitch propeller |
| Fuel grades | AVGAS 100LL, Mogas (min. RON 95), Super EN 228 | AVGAS 100LL |
Performance (MTOM, ISA)
| DA20i Katana | DA20-C1 | |||
|---|---|---|---|---|
| Max. cruise speed | 226 km/h TAS | 122 kts TAS | 240 km/h TAS | 130 kts TAS |
| Stall speed (landing configuration) | 83 km/h CAS | 45 kts CAS | 83 km/h CAS | 45 kts CAS |
| Max. rate of climb (MSL) | 3.4 m/s | 667 ft/min | 4.7 m/s | 920 ft/min |
| Max. range (8,000 ft, LRC PWR, no reserve) | 1,302 km | 703 nm | 985 km | 532 nm |
| Max. range fuel consumption (8,000 ft, LRC PWR) | 11.1 l/h | 2.9 US gal/h | 19.3 l/h | 5.1 US gal/h |
| Take-off ground roll / Take-off distance (MSL) | 254 m / 500 m | 833 ft / 1,640 ft | 383 m / 500 m | 1,256 ft / 1,640 ft |
| Landing ground roll / Landing distance (MSL) | 204 m / 507 m | 669 ft / 1,663 ft | 201 m / 415 m | 661 ft/ 1,360 ft |
| Max. operating altitude | 4,000 m | 13,100 ft | 4,000 m | 13,100 ft |
| Max. demonstrated crosswind | 37 km/h | 20 kts | 37 km/h | 20 kts |
Dimensions
Mass and Loading
| DA20i Katana | DA20-C1 | |||
|---|---|---|---|---|
| Seats | 2 | 2 | ||
| Empty weight | 525 kg | 1,158 lbs | 535 kg | 1,180 lbs |
| Max. useful load | 275 kg | 606 lbs | 265 kg | 584 lbs |
| Max. take-off mass | 800 kg | 1,764 lbs | 800 kg | 1,764 lbs |
| Max. useable fuel capacity | 84 l / 60 kg | 22.2 US gal / 89 lbs | 91 l / 66 kg | 24 US gal / 144 lbs |
Specifications apply to standard equipped aircraft, if not otherwise stated. The above data are approximately specifications and may change without notice.