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DA20 Series
Technical Specifications

Power Plant

 DA20i KatanaDA20 C1

Engine

(BRP-Powertrain) Rotax 912 iSc3 Sport with 100 HP

125hp Continental Motors 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, Super EN 228

AVGAS 100LL

Performance (MTOM, ISA)

 DA20i KatanaDA20 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 CAS45 kts CAS67 km/h CAS

36 kts CAS

Rate of climb (MSL)

3.4 m/s667 ft/min4,2 m/s

830 ft/min

Range at 55 % (8,000 ft)

1,302 km703 nm20,1 l/h

5.3 US gal/h

Fuel Consumption at 55 % (8,000 ft)

11.1 l/h2.9 US gal/h20 l/h

5.3 US gal/h

Take-off ground roll / Take off distance (MSL, 50 ft)

254 m / 500 m833 ft / 1,640 ft383 m / 500 m

1,256 ft / 1,640 ft

Landing ground roll / Landing distance (MSL, 50 ft)

204 m / 507 m669 ft / 1,663 ft201 m / 415 m

661 ft/ 1,360 ft

Max. operating altitude

4,000 m13,100 ft4,000 m

13,100 ft

Max. demonstrated crosswind

37 km/h20 kts37 km/h

20 kts

Mass and Loading

 DA20i KatanaDA20 C1

Seats

22

Empty weight

525 kg

1,158 lbs

535 kg

1,180 lbs

Useful load

275 kg606 lbs265 kg

584 lbs

Max. take off mass

800 kg1,764 lbs800 kg1,764 lbs

Useable fuel

84 l / 67.2 kg22.2 US gal / 148.7 lbs91 lt / 65,5 kg

24 US gal / 144,4 lbs

1. Short trip loading, well serviced aircraft condition
Specifications apply to standard equipped aircraft, if not otherwise stated. The above data are approximately specifications and may change without notice.