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General| Engine | Continental TSIO-520-R |
|---|---|
| Horsepower | 310 hp |
| Max Takeoff Weight | 4, 000 lbs |
| Fuel Capacity | 92 gallons |
| Cruise Speed | 195 knots |
| Wingspan | 36 ft |
| Rate of Climb | 1, 000 ft/min |
Defines operational speeds like VNE, VNO, VA, VFE, VLO, VLE, and their significance.
Details engine manufacturer, model, power ratings, and operating limits.
Specifies maximum ramp, takeoff, and landing weights for the aircraft.
Defines the allowable center of gravity range for safe operation.
Outlines approved maneuvers for the normal category aircraft.
Details fuel tank capacities, usable fuel, and grade requirements.
Immediate action items for various emergencies like engine failures, fires, and forced landings.
Elaboration on operational checklists for specific emergencies like engine failure and forced landings.
Detailed checks for general condition, controls, and systems before flight.
Procedures for starting the engine and ground movement.
Procedures for normal, short field, and crosswind takeoffs.
Procedures for climb, cruise, descent, and landing.
Details takeoff distances and corrections for various conditions.
Guidance on selecting cruising altitude and power settings for optimal performance.
Estimation of total fuel requirements for the flight based on performance data.
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