N23678 is a member of the Cessna 172S fleet at Crosswinds Aviation.
Being a 2007 model, this particular aircraft has a WAAS enabled GPS, allowing LPV approaches.
N23678
| Make | Cessna | |
| Model | 172S | |
| Year | 2007 | |
| Category | Utility / Normal | |
| Span / Length / Height | 36 ft. 1 in. / 27 ft. 2 in. / 8 ft. 11 in. | |
| Permitted Operations | Day and Night VFR and IFR | |
| Panel | Garmin G1000 | |
| Engine | Lycoming IO-360-L2A (180hp @ 2700 RPM) | |
| Propeller Type | Fixed Pitch | |
| Gear Configuration | Fixed Tricycle w/ Steerable Nosewheel | |
| Body Construction | Sheet metal | |
| ADS-B | N/A |
| Model | Lycoming IO-360-L2A | |
| No. Cylinders | 4 | |
| Displacement | 360 cu. in. | |
| Output | 180hp @ 2700 RPM | |
| Fuel Delivery | Fuel Injection | |
| Propeller Type | Fixed Pitch | |
| Propeller Manufacturer | McCauley Propeller Systems |
| PFD / MFD | Garmin G1000 | |
| GPS | Garmin GIA 63W | |
| Transponder | Garmin GTX 33 | |
| Audio Panel | Garmin GMA 1347 | |
| COM 1 | Garmin GIA 63W | |
| NAV 1 | Garmin GIA 63W | |
| COM 2 | Garmin GIA 63W | |
| NAV 2 | Garmin GIA 63W | |
| Autopilot | Bendix King KAP 140 |
| Total Fuel Capacity | 56 Gallons | |
| Usable Fuel Capacity | 53 Gallons | |
| Fuel Type | 100LL | |
| Oil Quantity | 8 Qts. |
| Max Ramp Weights | Normal: 2558 lbs. Utility: 2208 lbs. |
|
| Max Takeoff Weights | Normal: 2550 lbs. Utility: 2200 lbs. |
|
| Max Landing Weight | Normal: 2550 lbs. Utility: 2200 lbs. |
|
| Aircraft Specific Basic Empty Weight & Arm | 1750.4 lbs. @ 41.77 in. | |
| Max Useful Load | Normal: 807.6 lbs. Utility: 449.6 lbs. |
|
| Useful Load w/ Full Usable Fuel | Normal: 489.6 lbs. Utility: 131.6 lbs. |
|
| Baggage Capacities | Area A: 120 lbs. Area B: 50 lbs. *Max A + B is 120 lbs* |
| Climb Speeds | ||
| Cruise Climb | 80 KIAS | |
| Best Rate Climb – Flaps Up (VY) | Sea Level: 74 KIAS 10,000 Ft.: 72 KIAS |
|
| Best Angle Climb – Flaps Up (VX) | Sea Level: 74 KIAS 10,000 Ft.: 72 KIAS |
|
| Landing Speeds | ||
| Normal Landing | Flaps Up: 70 KIAS Flaps Full: 65 KIAS |
|
| Go Around Climb – Flaps 20 | 60 KIAS | |
| Max Demonstrated Crosswind Component | 15 KTS | |
| Airspeed Limitations | ||
| Never Exceed Speed (VNE) | 163 KIAS | |
| Max Structural Cruising Speed (VNO) | 129 KIAS | |
| Maneuvering Speeds (VA) | 1900 lbs.: 90 KIAS 2200 lbs.: 98 KIAS 2550 lbs.: 105 KIAS |
|
| Max Flap Extended Speed – Flaps 10 (VFE) | 110 KIAS | |
| Max Flap Extended Speed – Flaps 10 – Full (VFE) | 85 KIAS | |
| Clean Stall Speeds (VS) | 48 KIAS | |
| Landing Stall Speeds (VS0) | 40 KIAS | |
| Glide Ratio | 1.6 NM / 1000 ft. @ 68 KIAS | |
| Max Demonstrated Crosswind Component | 15 KTS | |
| Max Cruise Speed / Fuel Burn | 125 KTAS / 11.1 gph (8,000 ft. @ 20c Below Std. temp @ 2700 RPM) | |
| Service Ceiling | 14,000 ft. | |
| Sea Level Climb @ Max T/O Weight & 20c. | 710 fpm (Flaps Cruise @ 74 KIAS) | |
| Wing Loading | 14.7 lbs./sq. ft. (Max T/O Weight) | |
| Power Loading | 14.2 lbs./hp (Max T/O Weight) |
