MSFS 2024 · General Aviation
Cessna Citation X (FlightFX) Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vmo | 270 KIAS below 8,000 ft / 350 KIAS above 8,000 ft | Manual splits VMO by altitude. Current entry lists only 350 KIAS. |
| Mmo | M0.92 | Max operating Mach. Typical cruise M0.88 |
| Vr | 116-134 KIAS | Typical range at maximum takeoff weight |
| V1 / V2 | Per FMS takeoff data page | V-speeds are not populated to the PFD until flaps are in the T/O position (15) |
| Vfe (Slats / Flaps 5 deg) | 250 KIAS | Max flap extension speed |
| Vfe (Flaps FULL) | 180 KIAS | Max flap extension speed |
| Vlo / Vle | 210 KIAS | Max gear operating and max gear extension speed |
| Approach Speed (Flaps MID, MLW) | 147 KIAS | At maximum landing weight |
| Approach Speed (Flaps DN, MLW) | 136 KIAS | At maximum landing weight |
| Climb Speed | 300 KIAS below FL300 / M0.80 above FL300 | Recommended climb speed |
| Rough Air Penetration | 300 KIAS below FL300 / M0.9 above FL300 | - |
| Max Crosswind Component | 25 knots | - |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | TO/MC detent - FADEC controlled |
| Climb | CLB detent |
| Cruise | CRU detent or as required |
| Descent | Idle or as required |
| Anti-Ice Check (before takeoff) | Approximately 40 percent N1 for 2-3 minutes, then idle |
| Cross-Bleed Start | Opposite engine adjusted to maintain 30 PSI minimum start pressure, approximately 55 percent N1 |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| UP | Any | Cruise / Climb |
| Slats / Flaps 5 deg | 250 KIAS max | Slat and initial flap extension |
| T/O (15) | Per placard | Takeoff - V-speeds only populate to the PFD at this setting |
| MID | Per placard | Approach - 147 KIAS approach speed at MLW |
| DN / FULL | 180 KIAS max | Landing - 136 KIAS approach speed at MLW |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | Rolls-Royce AE 3007C, around 6,700 lbf each (AE 3007C1) |
| Max N1 | As per FADEC control limits |
| Max ITT | Around 857 degC |
| Generator Load Limit | 400 amps per generator |
| APU Ammeter | 400 A max on ground / 200 A max in flight |
| APU DC Volts (start) | 22 volts minimum |
| Start Duct Pressure | At least 30 PSI |
| Fuel Introduction | Throttle to IDLE by 10 percent N2 RPM |
| Thrust Reversers | Idle by 65 KIAS |
| Bypass Ratio / Fan | Approximately 5:1, 44 inch fan |
KEY NUMBERS
| Parameter | Value |
|---|---|
| MTOW | 36,100 lbs (16,374 kg) |
| MRW | 36,400 lbs (16,510 kg) |
| MLW | 31,800 lbs (14,424 kg) |
| MZFW | 24,400 lbs (11,067 kg) |
| Typical Empty Weight | Around 21,000 lbs (9,525 kg) |
| Max Fuel Imbalance | 400 lbs intentional |
| Max Operating Altitude | 51,000 ft |
| Typical Cruise | Mach 0.88 |
| Range | Around 3,100 nmi (standard conditions) |
| Takeoff Distance (MTOW, SL, ISA) | Around 5,140 ft |
| Landing Distance (MLW, SL, ISA) | Around 3,500 ft |
| Minimum Flight Crew | 2 (pilot and co-pilot) |
| Avionics | Integrated HP2000 avionics suite |