Bell 407
MSFS 2024 - QUICK REFERENCE
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vne | 140 KIAS | Never exceed |
| Vy | 80 KIAS | Best rate of climb |
| Vauto (best glide) | 80 KIAS | Max glide distance |
| Vauto (min RoD) | 55 KIAS | Min rate of descent |
| Vmax (auto) | 100 KIAS | Max autorotation |
| Vcruise | 133 KIAS | Recommended cruise |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | 100% Nr, collective as required |
| Climb | 100% Nr, 80 KIAS |
| Cruise | 100% Nr, 120–133 KIAS |
| Approach | 100% Nr, 60–80 KIAS |
| Autorotation | Throttle - OFF, Nr 97–107% |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| N/A | N/A | No flaps - helicopter uses collective pitch |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| TOT (Start Max 10s) | 927 °C |
| TOT (Takeoff 5 min) | 779 °C |
| TOT (Max Continuous) | 727 °C |
| Ng (Max Continuous) | 105% |
| Ng (Transient) | 106% |
| Nr (Normal) | 100% (413 RPM) |
| Oil Pressure | 90–130 PSI |
| Oil Temp (Max) | 107 °C |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Hover Ceiling (IGE) | 14,200 ft (ISA) |
| Hover Ceiling (OGE) | 10,400 ft (ISA) |
| Fuel Capacity | 495 L (131 US gal) |
| Fuel Burn | ~220 L/hr |
| Rate of Climb | 1,700 ft/min |
| MTOW | 2,381 kg (5,250 lbs) |
| Best Glide (auto) | 80 KIAS |
| Max Crosswind | 17 kts |