Airbus H125
MSFS 2024 - QUICK REFERENCE
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vne | 155 KIAS | Never exceed |
| Vy | 65 KIAS | Best rate of climb |
| Vx | 55 KIAS | Best angle of climb |
| Vauto | 65 KIAS | Best autorotation |
| Vmin (auto) | 30 KIAS | Min autorotation |
| Vmax (auto) | 100 KIAS | Max autorotation |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | 100% Nr, FULL COLLECTIVE as required |
| Climb | 100% Nr, 65 KIAS Vy |
| Cruise | 100% Nr, 120–130 KIAS |
| Approach | 100% Nr, 60–70 KIAS |
| Autorotation | Twist Grip - IDLE, 100% Nr |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| N/A | N/A | No flaps - helicopter uses collective pitch |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| TOT (Takeoff 5 min) | 846 °C |
| TOT (Max Continuous) | 846 °C |
| TOT (Start Max) | 850 °C |
| Ng (Max Continuous) | 104.4% |
| Ng (Transient) | 106% |
| Nr (Normal) | 394 RPM (100%) |
| Oil Pressure | 45–85 PSI |
| Oil Temp | Max 107 °C |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Hover Ceiling (IGE) | 15,200 ft (ISA) |
| Hover Ceiling (OGE) | 12,800 ft (ISA) |
| Fuel Capacity | 540 L (143 US gal) |
| Fuel Burn | ~200 L/hr |
| Max Sling Load | 1,400 kg (3,086 lbs) |
| Rate of Climb | 1,700 ft/min |
| Max Passengers | 5 (+ 1 pilot) |
| Best Glide (auto) | 65 KIAS |