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General| Manufacturer | Cessna |
|---|---|
| Model | 172N |
| Year | 1980 |
| Engine | Lycoming O-320-H2AD |
| Horsepower | 160 hp |
| Length | 27 ft 2 in |
| Useful Load | 850 lbs |
| Seating Capacity | 4 |
| Propeller | Fixed-pitch |
| Height | 8 ft 11 in |
| Maximum Takeoff Weight | 2, 450 lbs |
| Rate of Climb | 720 ft/min |
| Wingspan | 36 ft 1 in (11.0 m) |
| Empty Weight | 1, 450 lb (658 kg) |
| Range | 640 nautical miles |
Details specifications for engine, propeller, fuel, and oil systems.
Defines certificated weights, empty weights, useful load, and specific loadings.
Explains limitations and details critical airspeeds like Vne, Vno, Va, Vfe.
Specifies operating limits for the engine, propeller, and maximum weights.
Covers CG limits, approved maneuvers, load factors, and permissible operations.
Provides step-by-step procedures for engine failures and other emergencies.
Offers detailed explanations for critical emergency actions.
Covers engine failure, forced landings, cloud operations, and spin recovery.
Details preflight checks and step-by-step instructions for starting the engine.
Covers normal and short field takeoff techniques and enroute climb.
Details recommended procedures for cruising and various landing types.
Presents takeoff distances and cruise performance metrics.
Details fuel estimation and landing distance data.
Outlines weighing procedures and methods for balance calculations.
