DA20 AIRCRAFTS
The DA20's instrumentation and standard Garmin G500 avionics are designed for safety, a positive learning transfer, reliability and value. The DA20 is available in two engine variants. Choose between a Bombardier Rotax 912 iS3c Sport with 100 HP (DA20i Katana) and a fuel injected 125 hp Continental Motors IO-240 (DA20-C1 airplane).
15 x DA20 AIRCRAFTS :
- TC-EOA
- TC-EOC
- TC-EOD
- TC-EOE
- TC-EOF
- TC-EOG
- TC-EOH
- TC-EOI
- TC-EOJ
- TC-EOK
- TC-EOS
- TC-EOT
- TC-EOV
- TC-GAS
- TC-GAG
DA20 C1 Mass and Loading
- Seats
- Empty weight
- Useful load
- Max. take off mass
- Fuel capacity total
- 2
- 535 kg.
- 265 kg.
- 800 kg.
- 91 lt./65,5 kg.
- 2
- 1180 lbs.
- 584 lbs.
- 1764 lbs.
- 24 US gal./144,4 lbs.
DA20 C1 PERFORMANCE (MTOM, ISA)
- Max. cruise speed
- Stall speed, landing configuration
- Rate of climb (MSL)
- Range at 55 % (8,000 ft)
- Fuel Consumption at 55 % (8,000 ft)
- Take-off ground roll / Take off distance (MSL, 50 ft)
- Landing ground roll / Landing distance (MSL, 50 ft)
- Max. operating altitude
- Max. demonstrated crosswind
- 240 km/h TAS
- 67 km/h CAS
- 4.2 m/s
- 973 km
- 20 l/h
- 383 m / 500 m
- 201 m / 415 m
- 4,000 m
- 37 km/h
- 130 kts TAS
- 36 kts CAS
- 830 ft/min
- 525 nm
- 5.3 US gal/h
- 1,256 ft / 1,640 ft
- 661 ft/ 1,360 ft
- 13,100 ft
- 20 kts
DA40 AIRCRAFTS
The DA40 fully integrated G1000 NXi flight deck, incorporating the latest features with optional ultra-precise GFC700 Automatic Flight Control System, offers superior situational awareness, convenience and safety. Available equipment provides Traffic Advisories, Synthetic Vision Technology, Satellite WX and Entertainment, and more.
4 x DA40-NG AIRCRAFTS :
DA40 NG DIMENSIONS, MASS and LOADING
- Seats
- Empty weight
- Useful load
- Max. take off mass
- Fuel capacity total
- Main Tank (Fuel)
- Auxiliary Tank (Fuel)
- 4
- 900 kg.
- 410 kg.
- 1310 kg.
- 147 lt./118 kg.
- 106 lt./84 kg.
- 41 lt./33 kg.
- 4
- 1984 lbs.
- 904 lbs.
- 2888 lbs.
- 39 US gal./261 lbs.
- 28 US gal./188 lbs.
- 11 US gal./74 lbs.
DA40 NG PERFORMANCE (MTOM, ISA)
- Max. speed (14,000 ft, MCP)
- Cruise speed at 60 % (14,000 ft)
- Cruise speed at 75 % (6,000 ft)
- Stall speed, landing configuration
- Rate of climb (ISA SL)
- Range at 60 % (incl. auxiliary tank)
- Range at 45 % (incl. auxiliary tank)
- Fuel consumption
- Take-off ground roll (ISA SL)
- Landing ground roll (ISA SL)
- Max. operating altitude
- Max. demonstrated crosswind
- 285 km/h TAS
- 231 km/h TAS
- -
- 107 km/h CAS
- 3.5 m/s
- 1741 km
- -
- 19.5 l/h (@60%)
- 370 m
- 270 m
- 5,000 m
- 46 km/h
- 154 kts TAS
- 125 kts TAS
- -
- 58 kts CAS
- 690 ft/min
- 940 nm
- -
- 5.1 US gal/h (@60%)
- 1,214 ft
- 886 ft
- 16,400 ft
- 25 kts
DA42 AIRCRAFTS
The DA42 is powered by the Austro Engine 168hp AE300 with a single power lever control.
The 3 blade MT hydraulic constant speed propellers feature advanced blade geometry for efficient performance, smoothness and low noise. Automatically controlled by each engine’s digital engine control - feathering is as simple as flipping a single switch.
The fully integrated Garmin G1000 NXi is complemented by a long list of avionics options - such as an integrated weather radar and Synthetic Vision - to perfectly suit your mission.
3 x DA42-NG AIRCRAFTS :
DA40 NG DIMENSION, MASS and LOADING
- Seats
- Empty weight
- Useful load
- Max. take off mass
- Fuel capacity total
- Main Tank (Fuel)
- Auxiliary Tank (Fuel)
- 4
- 1,410 kg.
- 589 kg.
- 1,999 kg.
- 289 lt./231 kg.
- 189 lt./151 kg.
- 100 lt./80 kg.
- 4
- 3,109 lbs.
- 1,299 lbs.
- 4,407 lbs.
- 76.4 US gal./512 lbs.
- 50 US gal./335 lbs.
- 26.4 US gal./177 lbs.
DA42 NG PERFORMANCE (MTOM, ISA)
- Max. speed (16,000 ft, MCP) 1,760 kg TOW
- Cruise speed at 75 % (16,000 ft)
- Stall speed, landing configuration
- Rate of climb (ISA SL) 1,760 kg TOW
- Single Engine Service Ceiling
- Range at 60 % (12,000 ft, incl. auxiliary tank)
- Consumption at 60 % in total
- Take-off ground roll (ISA SL), 1,760 kg TOW
- Landing ground roll (ISA SL)
- Max. operating altitude
- Max. demonstrated crosswind
- 365 km/h TAS
- 325 km/h TAS
- 113 km/h CAS
- 7.9 m/s
- 5,486 km
- 2,250 km
- 39.4 l/h (@60%)
- 280 m
- 340 m
- 5,486 m
- 46 km/h
- 197 kts TAS
- 176 kts TAS
- 61 kts CAS
- 1550 ft/min
- 18,000 ft/min
- 1,215 nm
- 10.4 US gal/h (@60%)
- 919 ft
- 1,115 ft
- 18,000 ft
- 25 kts