DA40 XLS Specifications*PRINTAIRCRAFT ITEM INFORMATION
Engine Lycoming IO-360-M1A
Horsepower 180 hp
Propeller MT 3-blade composite constant-speed
Airworthiness category Normal and utility
Length 26 ft 5 in
Height 6 ft 6 in
Wing Span 39 ft 6 in
Maximum takeoff weight 2,645 lbs
Useful load 860 lbs (standard equipped airplane)
Fuel capacity, usable 50 gal
Fuel AVGAS 100 LL
Takeoff distance, ground roll 1,175 ft
Takeoff distance, 50-foot obstacle 1,700 ft
Landing distance, ground roll 1,155 ft
Landing distance, 50-foot obstacle 2,093 ft
Rate of climb, sea level 1,120 ft/min
Garmin GNC 420W GPS/COM
Garmin GTX 327 transponder with blind altitude encoder
PS Engineering PM 1000 Intercom
Sheepskin seat cushions
Integral instrument lighting
Inertia reel harnesses
Extended glare shield
Electroluminescent panel flood light
Engraved aluminum throttle quadrant cover plates
Premium carpet
AIRCRAFT ITEM INFORMATION
Engine 2x Austro Engine AE 300 turbocharged, common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control
Propellers 2x MT MTV-6-R-C-F / CF187-129 3-blade Constant Speed Propeller
Airworthiness category Normal
Length 28 ft 1 in
Height 8 ft 2 in
Wing span 44 ft
Seats 4
Empty weight 3,119 lbs
Maximum take-off weight (MTOW) 4,189 lbs
Fuel capacity (useable fuel) (standard / long range) 50 US gal / 76 US gal
Fuel grades Jet A1
Rate of climb, sea level MTOW 1,150 fpm
Rate of climb, 10,000 ft MTOW 1,020 fpm
Maximum operating altitude 18,000 ft
DA20 Specifications*PRINTAIRCRAFT ITEM INFORMATION
Engine TCM IO-240-B3B
Horsepower 125 hp
Propeller Sensenich 2-blade fixed pitch
Airworthiness category Utility, spin certified
Length 23 ft 6 in
Height 7 ft 2 in
Wing Span 35 ft 8 in
Maximum takeoff weight 1,764 lbs
Useful load 600 lbs*
Fuel capacity, usable 24.0 gal
Fuel AVGAS 100LL
Takeoff distance, ground roll 1,280 ft
Takeoff distance, 50-foot obstacle 1,640 ft
Landing distance, ground roll 661 ft
Landing distance, 50-foot obstacle 1,360 ft
Rate of climb, sea level 1,000 ft/min
DA40 XLS Standard Features*PRINT 406 Mhz ELT
Centrally located standby instrumentation, including: Electric Attitude Indicator, Airspeed Indicator, Altimeter Magnetic Direction Indicator
Dual Garmin GIA 63W with Integrated radio modules with WAAS-certified IFR-approved GPS; VHF navigation with ILS; and VHF communication with 16-watt transceivers
Electronic carbon monoxide detector
Garmin FliteCharts (subscription required)
Garmin GDC74 Integrated, Digital Air Data Computer, constant display of TAS, CAS, Wind Direction, VSI and TAT
Garmin GDL69A Satellite Data Link - radar, satellite text and graphic weather data with infotainment (subscription required)
Garmin GDU 1044, 10 inch multi function display (MFD)
Garmin GDU 1040, 10 inch primary flight display (PFD)
Garmin GEA 71 Airframe / Engine Interface Unit
Garmin GFC 700 Automatic Flight Control System (AFCS) including 2-axis digital autopilot with Flight Director
Garmin GMA1347 Digital Audio Controller with digital ATC playback recording
Garmin GMU44 Magnetometer
Garmin GRS77 Solid-state Attitude and Heading Reference System (AHRS)
Garmin GTX33 Integrated Mode S Transponder
2X Garmin GIA 63 COM/NAV/GPS
Garmin GDU 1040, 10 inch multi function display (MFD)
Honeywell KAP 140 Dual Axis Autopilot with Altitude Hold and Preselect
Standby instruments (Compass, Horizon, Air Speed Indicator, Altimeter)
2X MT 3-blade constant speed full-feathering propeller
2X Thielert TAE 2.0 Centurion turbo diesel engines
3 point safety belts automatic (all seats)
4-way Baggage Compartment System
52 US gal fuel tank
Alternate static port