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General| Manufacturer | Cessna |
|---|---|
| Model | 152 |
| Year | 1979 |
| Type | Light Aircraft |
| Engine | Lycoming O-235-L2C |
| Horsepower | 110 hp |
| Wingspan | 33 ft 4 in (10.16 m) |
| Height | 8 ft 6 in (2.59 m) |
| Maximum Takeoff Weight | 1, 670 lb (757 kg) |
| Cruise Speed | 107 knots (123 mph, 198 km/h) |
| Empty Weight | 1, 081 lb (490 kg) |
| Useful Load | 589 lb (267 kg) |
| Stall Speed (Flaps Down) | 43 knots (49 mph, 80 km/h) |
| Seating Capacity | 2 |
| Range | 415 nmi (477 mi, 768 km) |
| Service Ceiling | 14, 700 ft |
| Rate of Climb | 715 ft/min (3.6 m/s) |
Provides checklists for engine failure during takeoff, immediately after takeoff, and during flight.
Outlines procedures for emergency landings with and without engine power, and ditching.
Provides takeoff distance data based on conditions like altitude, temperature, and wind.
Details cruise performance, including true airspeed, fuel flow, and altitude considerations.
Explains how to use loading graphs and envelopes to ensure proper loading and CG.
Details the Lycoming O-235-L2C engine, its accessories, and control systems.
Explains the 28-volt DC system, battery, alternator, master switch, and related components.
Specifies approved fuel types and usage, including unleaded/leaded automotive gasoline.
