Pilatus PC-12
MSFS 2024 - QUICK REFERENCE
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vr | 102 KIAS | Rotation (MTOW) |
| Vx | 120 KIAS | Best angle climb |
| Vy | 130 KIAS | Best rate climb |
| Va | 158 KIAS | Maneuvering (max wt) |
| Vapp (Full) | 84-98 KIAS | Approach (weight dep.) |
| Vfe (F15) | 165 KIAS | Max flap 15 |
| Vfe (F30) | 130 KIAS | Max flap 30/40 |
| Vle | 180 KIAS | Max gear extended |
| Vlo | 180 KIAS | Max gear operating |
| Vmo | 240 KIAS | Max operating below FL300 |
| Vs0 | 67 KIAS | Stall landing config |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | MAX - 1,200 SHP / 100% torque |
| Climb | MCT - Max Continuous Torque |
| Cruise 280 kts | ~1,000-1,100 SHP |
| Approach | Reduce torque - maintain Vapp |
| Ground Idle | PL at ground idle |
| Beta / Reverse | After main gear touchdown |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| 0 (UP) | Any | Cruise / Climb |
| 15 deg | <= 165 KIAS | Takeoff / Initial approach |
| 30 deg | <= 130 KIAS | Landing approach |
| 40 deg (Full) | <= 130 KIAS | Short field landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Max ITT (Takeoff) | 760 deg C |
| Max ITT (Continuous) | 740 deg C |
| Max ITT (Start) | 1,000 deg C |
| Max Torque | 100% |
| Prop RPM (Max) | 1,700 RPM |
| Oil Pressure | 40-90 PSI |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Takeoff Weight | 4,740 kg (9,921 lbs) |
| Max Landing Weight | 4,500 kg |
| Fuel Capacity | 1,182 kg (usable) |
| Fuel Burn (cruise) | ~190-250 kg/hr |
| Passengers | Up to 9 in cargo config |
| Cruise Speed | 280-290 KTAS |
| Max Altitude | FL300 |
| Max Crosswind T/O | 30 kts (F0) |