N122VS is Crosswinds Aviation’s Cirrus SR22.
The fastest aircraft in the Crosswinds fleet, N122VS is able to cruise at 183 KTAS. This aircraft is also equipped with a TKS Anti-Ice system, allowing flight into known icing being allowed under certain situations.
Given its speed and FIKI capabilities, N122VS is great for when you need to get somewhere fast or when icing is in the cards.
| Make | Cirrus | |
| Model | SR22 | |
| Year | 2014 | |
| Category | Normal | |
| Span / Length / Height | 38.3 ft. / 26.0 ft. / 8.9 ft. | |
| Permitted Operations | Day and Night VFR and IFR | |
| Panel | Garmin G1000 Perspective | |
| Engine | Continental IO-550-N | |
| Propeller Type | Constant Speed | |
| Gear Configuration | Fixed Tricycle w/ Castering Nosewheel | |
| Body Construction | Composite | |
| ADS-B | Out |
| Model | Continental IO-550-N | |
| No. Cylinders | 6 | |
| Displacement | 550 cu. in. | |
| Output | 310hp @ 2700 RPM | |
| Fuel Delivery | Fuel Injection | |
| Propeller Type | Constant Speed | |
| Propeller Manufacturer | Hartzell |
| PFD / MFD | Garmin G1000 Perspective | |
| GPS | Garmin GIA 63W | |
| Transponder | Garmin GTX 33 | |
| Audio Panel | Garmin GMA 350 | |
| COM 1 | Garmin GIA 63W | |
| NAV 1 | Garmin GIA 63W | |
| COM 2 | Garmin GIA 63W | |
| NAV 2 | Garmin GIA 63W | |
| Autopilot | Garmin GFC 700 |
| Total Fuel Capacity | 94.5 Gallons | |
| Usable Fuel Capacity | 92.0 Gallons | |
| Fuel Type | 100LL | |
| Oil Quantity | 8 Qts. |
| Max Takeoff Weight | 3600 lbs. | |
| Aircraft Specific Basic Empty Weight & Arm | 2432 lbs. @ 139.9 in. | |
| Max Useful Load | 1168 lbs. | |
| Useful Load w/ Full Usable Fuel | 616 lbs. | |
| Baggage Capacities | 130 lbs. |
| Climb Speeds | ||
| Cruise Climb | 110 KIAS | |
| Best Rate Climb – Flaps Cruise (VY) | 108 KIAS | |
| Best Angle Climb – Flaps Cruise (VX) | 88 KIAS | |
| Landing Speeds | ||
| Normal Landing – Flaps 100% | 80 KIAS | |
| Go Around Climb – Flaps 50% | 80 KIAS | |
| Max Demonstrated Crosswind Component | 21 KTS | |
| Airspeed Limitations | ||
| Never Exceed Speed (VNE) | 205 KIAS | |
| Max Structural Cruising Speed (VNO) | 176 KIAS | |
| Operating Maneuvering Speeds (VA) | 140 KIAS | |
| Max Flap Extended Speed – 50% (VFE) | 150 KIAS | |
| Max Flap Extended Speed – 100% (VFE) | 110 KIAS | |
| Clean Stall Speeds (VS) | 74 KIAS | |
| Landing Stall Speeds (VS0) | 64 KIAS | |
| Glide Ratio (Windmilling Propeller) | 8.8:1 (1.45 NM / 1000 ft.) 92 KIAS |
|
| Max Demonstrated Crosswind Component | 21 KTS | |
| Max Cruise Speed / Fuel Burn | 183 KTAS / 18.6 gph (8,000 ft. Std. Temp. @ 78% Power) | |
| Max Operating Altitude | 17,500 ft. | |
| Sea Level Climb (Cruise) @ Max T/O Weight & Std. Temp. | 1251 fpm (Flaps Cruise @ 108 KIAS) | |
| Sea Level Climb (Takeoff) @ Max T/O Weight & Std. Temp. | 1270 fpm (Flaps 50% @ 97 KIAS) | |
| Wing Loading | 24.8 lbs./sq. ft. | |
| Power Loading (Max Power) | 11.4 lbs./hp |
Airplane Flight Manual and Weight and Balance sheet coming soon
