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DA20 Series
Technical Specifications

Power Plant

 DA20i KatanaDA20 C1
Engine(BRP-Powertrain) Rotax 912 iSc3 Sport with 100 hp125 hp Continental IO-240-B32B engine
PropellerMT propeller MTV-21-A/175-05, 2-blade constant speed propellerSensenich 2 blade fixed pitch propeller
Fuel gradesAVGAS 100LL, Mogas (min. RON 95), Super EN 228AVGAS 100LL

Performance (MTOM, ISA)

 DA20i KatanaDA20 C1
Max. cruise speed226 km/h TAS122 kts TAS240 km/h TAS130 kts TAS
Stall speed (landing configuration)83 km/h CAS45 kts CAS83 km/h CAS45 kts CAS
Max. rate of climb (MSL)3.4 m/s667 ft/min4.7 m/s920 ft/min
Max. range (8,000 ft, LRC PWR, no reserve)1,302 km703 nm985 km532 nm
Max. range fuel consumption (8,000 ft, LRC PWR)11.1 l/h2.9 US gal/h19.3 l/h5.1 US gal/h
Take-off ground roll / Take-off distance (MSL)254 m / 500 m833 ft / 1,640 ft383 m / 500 m1,256 ft / 1,640 ft
Landing ground roll / Landing distance (MSL)204 m / 507 m669 ft / 1,663 ft201 m / 415 m661 ft/ 1,360 ft
Max. operating altitude4,000 m13,100 ft4,000 m13,100 ft
Max. demonstrated crosswind37 km/h20 kts37 km/h20 kts

Mass and Loading

 DA20i KatanaDA20 C1
Seats22
Empty weight525 kg1,158 lbs535 kg1,180 lbs
Max. useful load275 kg606 lbs265 kg584 lbs
Max. take-off mass800 kg1,764 lbs800 kg1,764 lbs
Max. useable fuel capacity84 l / 60 kg22.2 US gal / 89 lbs91 l / 66 kg24 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.