Eurocopter EC135 T1
MSFS 2024 - QUICK REFERENCE
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vne | 140 KIAS | Never exceed |
| Vy | 75 KIAS | Best rate of climb |
| Vauto (max range) | 90 KIAS | Max range autorotation |
| Vauto (min RoD) | 50 KIAS | Min rate of descent auto |
| Vmax (auto) | 100 KIAS | Max autorotation |
| Vcruise | 137 KIAS | Recommended cruise |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | 100% Nr, collective as required |
| Climb | 100% Nr, 75 KIAS |
| Cruise | 100% Nr, 120–137 KIAS |
| Approach | 100% Nr, 60–80 KIAS |
| Autorotation | Both engines - IDLE, maintain 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) | 903 °C |
| TOT (Max Continuous) | 835 °C |
| N1 (Max Continuous) | 100% |
| Nr (Normal) | 100% (394 RPM) |
| FLI (Max Continuous) | ≤ 1.0 |
| FLI (Takeoff) | ≤ 1.0 (5 min) |
| Oil Pressure | Min 2 bar |
| Oil Temp (Max) | 135 °C |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Hover Ceiling (IGE) | 12,500 ft (ISA) |
| Hover Ceiling (OGE) | 9,500 ft (ISA) |
| Fuel Capacity | 680 L (180 US gal) |
| Fuel Burn (both) | ~260 L/hr |
| Rate of Climb | 1,450 ft/min |
| MTOW | 2,835 kg (6,250 lbs) |
| OEI Ceiling | 8,000 ft |
| Max Crosswind | 25 kts |