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MSFS 2024 · General Aviation
Diamond DA40 NG (G1000 NXi) Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vr | 67 KIAS | Rotation at 1,280 kg (56 at 940 kg, 58 at 1,000, 61 at 1,100, 65 at 1,200) |
| V50 | 72 KIAS | Speed to 50 ft at 1,280 kg (62 at 940 kg) |
| Vy (Flaps T/O) | 72 KIAS | Climb up to a safe altitude |
| Cruise Climb (Flaps UP) | 88 KIAS | - |
| Vref (Flaps LDG) | 76 KIAS | At 1,216 kg (66 at 940 kg, 72 at 1,100, 77 at 1,280 and above) |
| Vref (Flaps T/O) | 77 KIAS | At 1,216 kg (68 at 940 kg, 78 at 1,280 and above) |
| Vref (Flaps UP) | 82 KIAS | At 1,216 kg (71 at 940 kg, 83 at 1,280 and above) |
| Min Go-Around (Flaps T/O) | 72 KIAS | - |
| Best Glide | 88 KIAS | Flaps up, windmilling propeller |
| Vo (up to 1,080 kg) | 101 KIAS | Operating maneuvering speed |
| Vo (1,081 - 1,180 kg) | 108 KIAS | - |
| Vo (above 1,180 kg) | 113 KIAS | - |
| Vfe (Flaps T/O) | 110 KIAS | - |
| Vfe (Flaps LDG) | 98 KIAS | - |
| Vno | 130 KIAS | Max structural cruising; yellow arc 130 to 172 KIAS |
| Vne | 172 KIAS | Never exceed, smooth air only |
| Vs (Flaps UP) | 66 KIAS | At 1,310 kg (58 at 1,000 kg) |
| Vs (Flaps T/O) | 62 KIAS | At 1,310 kg (54 at 1,000 kg) |
| Vs0 (Flaps LDG) | 60 KIAS | At 1,310 kg (55 at 1,000 kg) |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Idle | 710 +/- 30 RPM |
| Warm-Up / Taxi | Max 50% until engine temperatures in green |
| Available Power Check | 10 sec at MAX - 2,200 to 2,300 RPM (min 2,100 below -10 degC) |
| Take-Off | MAX - 100% (123.5 kW), 2,300 RPM, max 5 min |
| Climb | Max continuous 92% (114 kW), 2,100 RPM |
| Cruise (High Speed) | 92% - 8.3 US gal/h, 150 kt TAS at 12,000 ft |
| Cruise (Normal) | 75% - 6.6 US gal/h, 135 kt TAS at 12,000 ft |
| Cruise (Economy) | 60% - 5.1 US gal/h, 121 kt TAS at 12,000 ft |
| Cool Down Before Shutdown | Max 10% for 1 min |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| UP | Up to Vne 172 KIAS | Cruise and cruise climb |
| T/O | <= 110 KIAS | Take-off, downwind / base, go-around |
| LDG | <= 98 KIAS | Final approach and landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | Austro Engine AE300 (E4-A) turbo-diesel, 168 hp (123.5 kW) |
| Max Take-Off RPM | 2,300 RPM (max 5 min) |
| Max Continuous RPM | 2,100 RPM |
| Max Overspeed | 2,500 RPM (max 20 sec) |
| Max Take-Off Power | 100% / 123.5 kW (max 5 min) |
| Max Continuous Power | 92% / 114 kW |
| Oil Pressure | 2.5 - 6.0 bar normal; 0.9 bar min at idle, 6.5 bar max |
| Oil Temperature | 50 - 135 degC green; 140 degC max |
| Oil Quantity | 5.0 - 7.0 l (max consumption 0.1 l/h) |
| Coolant Temperature | 60 - 95 degC green; 105 degC max, 60 degC min at full load |
| Gearbox Temperature | 35 - 115 degC green; 120 degC max, 35 degC min at full load |
| Fuel Temperature | -20 to 55 degC green; -25 degC min, 60 degC max |
| Fuel Pressure | 4 bar min / 7 bar max (not indicated - warning only) |
| Voltage | 25 - 30 V green; 24.1 V min, 32.0 V max |
| Ammeter | Up to 60 A green; 70 A max |
| Max Restart Altitude | 16,400 ft PA immediate; 10,000 ft PA within 2 min |
| Approved Fuel | JET A, JET A-1, TS-1, RT, No. 3 Jet Fuel, JP-8 |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Take-Off Mass | 1,280 kg / 2,822 lbs (1,310 kg with MAEM 40-662) |
| Max Landing Mass | 1,216 kg / 2,681 lbs (1,280 kg with MAEM 40-574) |
| Max Zero Fuel Mass | 1,200 kg / 2,646 lbs (1,265 kg with MAEM 40-574) |
| Min Flight Mass | 940 kg / 2,072 lbs |
| Max Baggage | 45 kg cockpit compartment + 18 kg extension, 45 kg total |
| Fuel Capacity (Standard) | 2 x 15.0 US gal total / 2 x 14.0 US gal usable |
| Fuel Capacity (Long Range) | 2 x 20.5 US gal total / 2 x 19.5 US gal usable |
| Max Fuel Unbalance | 9 US gal (long range tanks) |
| Takeoff Ground Roll | 1,283 ft (391 m) |
| Takeoff Over 50 ft | 1,906 ft (581 m) |
| Landing Ground Roll | 1,043 ft (318 m) |
| Landing Over 50 ft | 2,133 ft (650 m) |
| Max Demonstrated Crosswind | 25 kts |
| Glide Ratio | 1:9.7 - 1.59 NM per 1,000 ft |
| Max Operating Altitude | 16,400 ft pressure altitude |
| Load Factors | +3.8 / -1.52 g flaps up; +2.0 / 0 g flaps T/O or LDG |
| Occupants | 1 minimum crew, 4 maximum |