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DA40 silhouette

DA40 Series
Technical Specifications

Power Plant

 DA40 NG

DA40 XLT

Engine

Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 hp and EECU single lever control systemLycoming IO-360 M1-A AVGAS Piston Engine with 180 HP

Propeller

MT propeller MTV-6-R-/190-69 3-blade constant speed propeller

Hartzell 2 blade metal constant speed propeller. Optional Hartzell 2 blade composite constant speed propeller. Optional MT 3 blade constant speed propeller

Fuel grades

Jet A-1, Jet A, TS-1 (Russia, Ukraine), RT (Russia, Ukraine), No. 3 Jet Fuel (China), JP-8AVGAS / 100LL / 100 / 130LL

Performance (MTOM, ISA)

 DA40 NG 

DA40 XLT

 
Max. cruise speed (16,000 ft, MCP)285 km/h TAS154 kts TAS  –
Cruise speed at 60% (14,000 ft)230 km/h TAS124 kts TAS  
Max. cruise speed (MSL, MCP)263 km/h TAS

142 kts TAS

Cruise speed at 75% (6,000 ft)

254 km/h TAS137 kts TAS

Stall speed, landing configuration

107 km/h CAS58 kts CAS96 km/h IAS52 kts IAS

Rate of climb (MSL)

3.3 m/s651 ft/min4.0 m/s

780 ft/min

Max. range (FL160, 50% PWR) incl. climb, no reserves1,730 km934 nm

Max. range (10,000 ft, 55% PWR, best eco) no climb, no reserves1,569 km847 nm

Fuel consumption

19.3 l/h

(@60%)

5.1 US gal/h

(@60%)

31 lt/h

(@65%)

8.2 US gal/h

(@65%)

Take-off performance (MSL,
ground roll / take-off obstacle)
397 m / 590 m1,302 ft / 1,935 ft305 m / 450 m1,000 ft / 1,476 ft
Landing performance (MSL,
ground roll / landing distance)
318 m / 650 m1,043 ft / 2,132 ft290 m / 620 m951 ft / 2,033 ft

Max. operating altitude

5,000 m16,400 ft5,000 m

16,400 ft

Max. demonstrated crosswind

46 km/h

25 kts

37 km/h

20 kts

Dimensions

DA40 technical drawing with dimensions. Wingspan 11.63 m/38 ft 3 in. Height 1.97m/6 ft 6 in, lenght 8.06 m /26 ft 5 in.

Mass and Loading

 DA40 NG DA40 XLT 

Seats

4444

Empty weight
without options

903 kg1,991 lbs792 kg

1,746 lbs

Max. useful load

407 kg897 lbs408 kg

900 lbs

Max. take off mass

1,310 kg2,888 lbs1,200 kg

2,646 lbs

Fuel capacity total
main tank
auxiliary tank

147 l / 118 kg
106 l / 84 kg
41.6 l / 34 kg
39 US gal / 260 lbs
28 US gal / 185 lbs
11 US gal / 75 lbs
189 l / 136 kg

50 US gal / 301 lbs

Specifications apply to standard equipped aircraft, if not otherwise stated. The above data are approximately specifications and may change without notice.