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Manufacturer | Cessna |
---|---|
Model | 150M |
Year | 1977 |
Engine Type | Continental O-200-A |
Horsepower | 100 hp |
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) |
Length | 24 ft 1 in |
Fuel Capacity | 26 US gal (98 L) |
Propeller | Fixed Pitch |
Service Ceiling | 14, 000 ft (4, 267 m) |
Maximum speeds and cruise performance details.
Ground roll and obstacle clearance distances.
Ground roll and obstacle clearance distances.
Stall speeds with flaps up and down.
Maximum allowable weight for takeoff and landing.
Takeoff, landing, and baggage weight limits.
Maximum permissible airspeeds for various operations.
Engine and propeller operating limits.
Maximum weight limits for takeoff and landing.
Recommended airspeeds for emergency flight.
Procedures for engine failure during takeoff and flight.
Procedures for landing without engine power.
Procedures for handling fires during start and in flight.
Steps to take for engine fire in flight.
Procedures for electrical fires.
Procedures for inadvertent icing encounters.
Troubleshooting rough engine operation.
Troubleshooting magneto malfunctions.
Actions for low oil pressure indications.
Issues with the electrical power system.
Recommended airspeeds for normal flight phases.
Walk-around inspection checklist.
Engine starting checklist.
Pre-takeoff checks and procedures.
Takeoff procedures.
Standard takeoff procedure.
Takeoff for short fields.
Landing procedures.
Standard landing procedure.
Landing on short fields.
Procedures for performing spins.
Takeoff distance calculation.
Cruise performance and range.
Landing distance estimation.
Takeoff distances based on conditions.
Landing distances based on conditions.
Calculating weight and balance.
Envelope for acceptable CG.
Graphical representation of CG limits.
Layout and function of instruments.
Description of the aircraft engine.
Description of the fuel system.
Description of the electrical system.