D - EFCM, Diamond DA40 NG


Baujahr: 2011
Motor: Austro Engine E4-A 165.5 PS
Sitzplätze: 4
Reisegeschwindigkeit: 140kt TAS
Reichweite: ca 1444 km
Startrollstrecke: ca 584m
Einsatz im Flugschulbetrieb: PPL-Schulung / IR Schulung / CPL Schulung / AOC - Commercial Operations / Charter
System: Autopilot GFC700, Garmin 1000

Checklist: DA40-NG Official English; DA40-NG AAFC Short English
POH: DA40-NG Basic Manual
Additional Information: G1000-CockpitReferenceGuide

Power Plant

Engines Austro Engine AE 300 turbocharged common-rail injected 2.0 liter diesel engine with 168 HP and EECU single lever control system 
Propeller MT propeller MTV-6-R-/190-69 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-8 
 

Performance/Consumption (max. mass)

 
Max. cruise speed (14,000 ft, MCP), 1760 kg TOW 285 km/h TAS 154 kts TAS
Max. cruise speed at 60% (14,000 ft) 231 km/h TAS 125 kts TAS
Stall speed, clean 117 km/h CAS 63 kts CAS
Stall speed, landing configuration 107 km/h CAS 58 kts CAS
Rate of climb (ISA SL) 3.5 m/s 690 fpm
Rate of climb (10,000 ft) 3.2 m/s 630 fpm
Range at 60%, standard-/ long range tank 1.250 km/ 1.741 km 675 nm/ 940 nm
Consumption at 60% 19.7 lt/hr 5.2 US gal/hr
Take-off distance 50 ft (ISA SL) 560 m 1.837 ft
Take-off ground roll (ISA SL) 370 m 1.214 ft
Landing distance 50 ft (ISA SL) 600 m 1.968 ft
Landing ground roll (ISA SL) 270 m 886 ft
Max. operating altitude 5.000 m 16.400 ft
Max. demonstrated crosswind 46 km/h 25 kts

Dimensions/Mass/Loading

Length 8.06 m 26 ft 5 in
Height 1.97 m 6 ft 6 in
Wing span 11.63 m 38 ft 2 in
Seats 4 4
Empty weight  880 kg 1.940 lbs
MTOM 1.280 kg 2.822 lbs
Payload  400 kg 882 lbs
Fuel capacity standard- / long range tank 106 lt / 147 lt 28 US gal / 39 US gal