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MSFS 2024 · General Aviation
Cirrus SR22 Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vr | 73-76 KIAS | Rotation, flaps 50% |
| Vr (Short Field) | 73 KIAS | Obstacle speed 84 KIAS |
| Vx | 88 KIAS | Best angle climb, SL and 10,000 ft |
| Vy | 108 KIAS | Best rate climb SL (99 at 10,000 ft) |
| Enroute Climb | 110-120 KIAS | Normal, flaps up |
| Vg | 92 KIAS | Best glide, all weights, 8.8:1 |
| Vo | 140 KIAS | Operating maneuvering (3,600 lb) |
| Vfe (50%) | 150 KIAS | Max flaps 50% |
| Vfe (100%) | 110 KIAS | Max flaps 100% |
| Vpd | 140 KIAS | Max demonstrated CAPS deployment |
| Vno | 176 KIAS | Max structural cruise |
| Vne | 205 KIAS | Never exceed |
| Vs0 | 64 KIAS | Stall, landing config (white arc) |
| Vs1 | 74 KIAS | Stall, flaps up (green arc) |
| Vref | 79 KIAS | Short field approach, flaps 100% |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | FULL FORWARD - approx 2,700 RPM |
| Taxi | 1,000 RPM max (hard surface) |
| Run-Up | 1,700 RPM |
| Idle | 600-750 RPM |
| Climb | Full power, fuel flow at top of green arc |
| Cruise | 55-85% power |
| Cruise Best Power | 75 degF rich of peak EGT (75% power or less) |
| Cruise Best Economy | 50 degF lean of peak EGT (65% power or less) |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| 0% (UP) | Any | Cruise / normal climb |
| 50% | <= 150 KIAS | All takeoffs / approach |
| 100% (Full) | <= 110 KIAS | Normal landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | Continental IO-550-N, 310 HP @ 2,700 RPM |
| Max RPM | 2,700 |
| Max Oil Temp | 240 degF (116 degC) |
| Min Oil Temp for Takeoff | 75 degF (24 degC) |
| Oil Pressure | 10 psi min / 100 psi max |
| Oil Quantity | 6 qt min, 7 qt for extended flights, 8 qt max |
| Max Power Fuel Flow (SL) | 27.1 GPH |
| Starter Duty Cycle | 10 sec crank / 20 sec cooling |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Takeoff Weight | 3,600 lbs (1,633 kg) |
| Max Zero Fuel Weight | 3,400 lbs (1,542 kg) |
| Max Baggage | 130 lbs (59 kg) |
| Fuel Capacity | 94.5 gal total / 92.0 gal usable |
| Max Glide Ratio | 8.8:1 (14.5 NM from 10,000 ft AGL) |
| Max Demonstrated Crosswind | 21 kts |
| Turbulent Air Penetration | 140 KIAS at 3,600 lb |
| CAPS Deployment Altitude | No minimum set; 2,000 ft AGL advised |
| CAPS Descent Rate | Less than 1,700 fpm (approx 13 ft drop) |
| Magneto Drop Limit | 150 RPM max / 75 RPM differential |