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General| Manufacturer | Cessna |
|---|---|
| Model | 150 COMMUTER |
| Year | 1976 |
| Type | Light Aircraft |
| Engine | Continental O-200-A |
| Horsepower | 100 hp |
| Wingspan | 33 ft 4 in (10.16 m) |
| Height | 8 ft 6 in (2.59 m) |
| Maximum Takeoff Weight | 1, 600 lb (726 kg) |
| Rate of Climb | 670 ft/min (3.4 m/s) |
| Seating Capacity | 2 |
| Service Ceiling | 14, 000 ft |
| Fuel Capacity | 26 US gal (22 imp gal; 98 L) |
Maximum takeoff and landing weights.
Critical airspeed limits and their operational significance.
Limits for the engine and its components.
Maximum certificated takeoff and landing weights.
Restrictions on fuel types and capacities.
Critical airspeeds for emergency scenarios.
Procedures for engine failure during takeoff or flight.
Steps for emergency landing with or without power.
Procedures for handling engine or cabin fires.
Critical speeds for normal flight phases.
Detailed checklist for preflight aircraft inspection.
Procedures for starting the aircraft engine.
Checklist for actions before takeoff.
Checklist for actions before landing.
Procedures for a standard landing.
Techniques for landing in crosswind conditions.
Performance data for takeoff operations.
Performance data for cruise flight.
Performance data for landing operations.
Stall speeds under various conditions.
Data on takeoff distances required.
Data on aircraft climb rates.
Data on climb performance.
Detailed cruise performance data.
Charts showing flight range based on fuel.
Charts showing flight endurance based on fuel.
Data on landing distances required.
Procedures for calculating weight and balance.
Chart for acceptable CG limits.
Chart showing CG limits for safe operation.
Description and operation of the ELT system.
Description of the transponder and altitude encoder.
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