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General| Manufacturer | Cessna |
|---|---|
| Model | 170 |
| Year | 1952 |
| Type | Light Aircraft |
| Horsepower | 145 hp |
| Seating Capacity | 4 |
| Engine | Continental C145-2 |
| Wingspan | 36 ft (11 m) |
| Height | 6 ft 7 in (2.01 m) |
| Max Takeoff Weight | 2, 200 lbs (998 kg) |
| Gross weight | 2, 200 lbs (998 kg) |
| Service ceiling | 15, 500 feet (4, 724 m) |
| Fuel Capacity | 42 gallons |
| Stall speed | 48 knots |
| Rate of climb | 690 ft/min |
Details the specific Cessna 170 models covered by this manual.
Welcomes the owner and outlines the manual's role in operating the aircraft.
Compares key specifications and features across different model years.
Identifies and describes the various instruments and controls on the panel.
Explains the fuel selector valve, specification, and grade requirements.
Details the schematic and components of the aircraft's electrical system.
Details the main landing gear, wheels, and tires.
Describes seats, cabin doors, baggage compartments, and utility shelf.
Outlines essential checks before engine start and during ground operation.
Covers normal and minimum run take-offs for landplanes and seaplanes.
Details normal landing procedures and stall speeds.
Lists critical performance and operational restrictions for the aircraft.
Explains center of gravity envelopes and loading graphs for balance.
Presents take-off, climb, and landing data for seaplane operations.
Outlines required inspections and their intervals.
Details the procedures for rigging ailerons, elevators, and rudder controls.
Covers maintenance for the metal propeller and landing gear components.
Shows the electrical wiring for the 1952 Cessna 170 model.
Illustrates the electrical wiring for the 1954 and 1955 Cessna 170 models.
Details the manufacturer's warranty for new aircraft.
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