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General| Manufacturer | Piper Aircraft Corporation |
|---|---|
| Model | Cherokee Lance PA-32R-300 |
| Engine | Lycoming IO-540-K1G5 |
| Horsepower | 300 hp |
| Seating Capacity | 6 |
| Maximum Takeoff Weight | 3, 600 lb (1, 633 kg) |
| Type | Single-engine piston aircraft |
| Propeller | Constant speed, 3-blade |
| Length | 27 ft 9 in |
| Empty Weight | 2, 150 lb (975 kg) |
| Useful Load | 1, 450 lb (658 kg) |
| Service Ceiling | 15, 000 ft |
Specific speed limitations for safe operation.
Detailed checklists for various emergencies.
Detailed procedure for landing without engine power.
Checklist for preflight and ground operations.
Procedures for starting the engine.
Procedures for approach and landing.
Importance of weight and CG.
Method for determining weight and balance for flight.
Description of the engine and propeller.
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