1976 Cessna 150M Standard, Commuter & Commuter II Airplane Pilot's Operating Handbook
Pilot's Operating Handbook for all Cessna 150M configurations including Standard, Commuter & Commuter II models. Publication DI055-13-RPC-750-9/83.
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Models Covered & Key Technical Specifications
1976 Cessna 150M Standard, Commuter & Commuter II Airplane Pilot's Operating Handbook
Pilot's Operating Handbook for all Cessna 150M configurations including Standard, Commuter & Commuter II models. Publication DI055-13-RPC-750-9/83.
- General Data: 109 knots sets the maximum indicated airspeed at sea level.
- Cruise Performance: For optimal cruising, 106 knots at 7000 ft is specified as the typical speed.
- Takeoff Performance: 735 ft is the ground roll required for takeoff with a 50-foot obstacle clearance.
- Landing Performance: 445 ft is the ground roll required for landing.
- Stall Speeds: 48 knots establishes the stall speed with flaps up and power off.
- Weight Specifications: 1600 lbs governs the maximum takeoff and landing weight Threshold.
Professional Workshop Service Manual & Technical Specifications
Practical Technical Assembly Manual: Cessna 150M Standard, Commuter & Commuter II Airplane Pilot's Operating Handbook (1976) Specification-Set
Engine-Type: Continental O-200-A // Engineering-Base: Airframe and Systems // Technical-Scope: Flight and operational procedures.
| Performance-Element | Rating | Framework |
|---|---|---|
| Maximum Speed | 109 knots | Sea Level |
| Cruise Speed | 106 knots | 7000 ft |
| Takeoff Ground Roll | 735 ft | Obstacle Cleared |
| Landing Ground Roll | 445 ft | Standard |
| Stall Speed (Flaps Up) | 48 knots | Power Off |
| Maximum Weight | 1600 lbs | Takeoff & Landing |
Repair data is categorized into:
- Aircraft Systems Descriptions
- Performance Specifications
- Airplane Handling, Service & Maintenance
- Limitations
- Emergency Procedures
Wiring diagrams are provided for the aircraft's electrical system, detailing component locations and connections. Fuel system procedures are documented for fuel management, including tank cross-feeding and capacity information. Adjustment procedures are detailed for flight controls and trim systems to ensure proper operation. Timing procedures are documented for engine starting and operation. Technical notes are provided for various systems, offering insights into their function and maintenance.
... documents weight and balance procedures for ensuring the aircraft operates within its center of gravity range for safe flight.
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