N1327N is a member of the Cessna 172S fleet at Crosswinds Aviation.
This particular aircraft has a Garmin GTX 345 transponder installed. As a result, not only does this enable ADS-B Out and In, but it also allows weather, traffic, position, and attitude data to be sent to ForeFlight and Garmin Pilot via Bluetooth connectivity.
For more information on Garmin Connext, please take a look at their brochure.
| Make | Cessna | |
| Model | 172S | |
| Year | 2006 | |
| 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 | In / Out |
| 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 63 | |
| Transponder | Garmin GTX 345 | |
| Audio Panel | Garmin GMA 1347 | |
| COM 1 | Garmin GIA 63 | |
| NAV 1 | Garmin GIA 63 | |
| COM 2 | Garmin GIA 63 | |
| NAV 2 | Garmin GIA 63 | |
| 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 | 1747.4 lbs. @ 41.56 in. | |
| Max Useful Load | Normal: 802.6 lbs. Utility: 452.6 lbs. |
|
| Useful Load w/ Full Usable Fuel | Normal: 484.6 lbs. Utility: 134.6 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) |
