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General| Manufacturer | Cessna |
|---|---|
| Model | 150 |
| Type | Light aircraft |
| First Flight | September 12, 1957 |
| Engine | Continental O-200-A |
| Horsepower | 100 hp |
| Height | 8 ft 6 in (2.59 m) |
| Service Ceiling | 14, 000 ft (4, 300 m) |
| Rate of Climb | 670 ft/min (3.4 m/s) |
| Gross Weight | 1, 600 lb (726 kg) |
| Seating Capacity | 2 |
| Maximum Speed | 124 mph |
| Fuel Capacity | 26 gallons |
| Stall Speed | 48 mph |
Aircraft gross weight specifications.
Aircraft speed performance data.
Flight range capabilities of the aircraft.
Rate of climb performance at sea level.
Maximum altitude the aircraft can operate.
Aircraft take-off performance metrics.
Aircraft landing performance metrics.
Approximate empty weight of the aircraft.
Aircraft baggage capacity.
Wing loading specification in pounds per square foot.
Power loading specification in pounds per horsepower.
Total fuel capacity for standard and long range tanks.
Total oil capacity for the engine.
Specifications for the aircraft propeller.
Specifications of the aircraft engine.
Pre-flight exterior inspection procedures.
Checks to perform before engine start.
Procedures for starting the aircraft engine.
Standard procedure for aircraft take-off.
Procedures for high-performance take-off.
Standard procedure for climbing the aircraft.
Description of the aircraft's fuel system.
Operation and maintenance of the fuel strainer drain.
Function and indication of the ammeter.
Aircraft electrical protection systems.
Operation of optional landing lights.
Operation of optional flashing beacon.
Engine warm-up procedures before take-off.
Procedure for checking the magneto system.
Performing full throttle checks before take-off.
Data related to aircraft climb performance.
Recommended airspeeds for climbing.
Procedures for normal aircraft landings.
Procedures for landing in short fields.
Procedures for landing in crosswind conditions.
Approved flight operations and certifications.
Permitted maneuvers in the utility category.
Procedures for handling the airplane on the ground.
Steps for securely tying down the aircraft.
Daily maintenance and servicing tasks for the aircraft.
Procedures for fueling the aircraft's tanks.
Maintenance and draining of the fuel strainer.
Procedures for adding engine oil.
Method for checking the engine oil level.
Maintenance tasks required every 50 hours of operation.
Maintenance tasks required every 100 hours of operation.
Maintenance tasks required every 500 hours of operation.
Maintenance tasks performed as needed.
Description of optional long range fuel tanks.
Information on the winterization kit.
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