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MSFS 2024 · General Aviation
Pilatus PC-12 Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vr (flaps 15) | 82 KIAS | MTOW 10,450 lb sea level ISA |
| Vr (flaps 30) | 76 KIAS | Reduced takeoff distance |
| Vx | 120 KIAS | Best angle climb |
| Vy | 130 KIAS | Sea level; 125 KIAS to 15,000 ft; 120 KIAS above 20,000 ft |
| Vo | 166 KIAS | Max operating maneuvering at 10,450 lb |
| Vfe (15 deg) | 165 KIAS | Flaps at or below 15 deg |
| Vfe (30/40 deg) | 130 KIAS | Flaps above 15 deg |
| Vlo | 180 KIAS | Max gear operating, extension and retraction |
| Vle | 240 KIAS | Max speed gear extended |
| Vmo / Mmo | 240 KIAS / M0.49 | 240 KIAS at or below 16,300 ft, then per VMO schedule |
| Vapp (flaps 40) | 85 KIAS | MLW 9,921 lb; flaps 30 is 89 KIAS, flaps 15 is 99 KIAS, flaps 0 is 120 KIAS |
| Best Glide | 119 KIAS | Propeller feathered at 10,450 lb; 110 KIAS at 9,040 lb |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | 1,200 SHP / 44.84 psi torque / ITT 850 degC / Np 1,700 RPM (5 min limit) |
| Max climb | 1,200 SHP / 44.84 psi torque / ITT 825 degC |
| Cruise | 1,100 SHP / 40.63 psi torque / ITT 820 degC |
| Max reverse | 900 SHP / 34.26 psi torque / ITT 820 degC / Np 1,650 RPM |
| Min idle | Ng 64.5% / ITT 750 degC |
| Transient (20 sec) | 61.00 psi torque / ITT 900 degC / Ng 104.3% / Np 1,870 RPM |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| 0 (UP) | Any | Cruise and climb; retract at 100 KIAS after takeoff |
| 15 deg | 165 KIAS max | Normal takeoff and initial approach |
| 30 deg | 130 KIAS max | Reduced takeoff distance and landing approach |
| 40 deg | 130 KIAS max | Normal landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | Pratt and Whitney Canada PT6E-67XP (PC-12 NGX, MSN 2001 and up) |
| Max ITT (takeoff) | 850 degC |
| Max ITT (max climb) | 825 degC |
| Max ITT (cruise) | 820 degC |
| Max ITT (start) | 1,000 degC, time limited to 5 sec |
| Max torque | 44.84 psi (23.92 psi below 1,000 prop RPM) |
| Ng limit | 104% |
| Np limit | 1,700 RPM |
| Oil pressure | 90-135 psi; 60 psi minimum below 23.92 psi torque; below 60 psi stop the engine |
| Oil temperature | 15-110 degC for takeoff; 105-110 degC limited to 10 min |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Ramp Weight | 10,495 lb (4,760 kg) |
| Max Takeoff Weight | 10,450 lb (4,740 kg) |
| Max Landing Weight | 9,921 lb (4,500 kg) |
| Max Zero Fuel Weight | 9,039 lb (4,100 kg) |
| Fuel (usable) | 402 US gal, 2,703.6 lb (1,521.5 litres) |
| Oil capacity | 3.6 US gal (13.6 litres) total |
| Max altitude (engine inlet limit) | 30,000 ft |
| Max demonstrated crosswind | 30 kts flaps 0, 25 kts flaps 15, 20 kts flaps 30, 15 kts flaps 40 |