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General| Manufacturer | Cessna |
|---|---|
| Engine | Continental IO-360-K |
| Horsepower | 195 hp |
| Max Takeoff Weight | 2, 550 lbs |
| Length | 27 ft 2 in |
| Service Ceiling | 16, 000 ft |
| Seating Capacity | 4 |
| Landing Distance | 1, 335 ft |
| Model | R172K |
| Propeller | McCauley constant speed |
| Empty Weight | 1, 600 lbs |
| Fuel Capacity | 52 gallons |
| Cruise Speed | 122 knots |
Airspeed limitations and their operational significance.
Specifications and limits for the aircraft's power plant.
Procedures for engine failure during takeoff and flight.
Procedures for landing without engine power or with reduced power.
Procedures for emergency landing on water.
Procedures for engine, electrical, cabin, and wing fires.
Procedures for encountering icing conditions.
Takeoff distances for various conditions and weights.
Performance data for cruise flight at different altitudes and temperatures.
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