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General| Manufacturer | Cessna |
|---|---|
| Model | TR182 |
| Year | 1979 |
| Engine | Lycoming O-540-L3C5D |
| Horsepower | 235 hp |
| Max Takeoff Weight | 3, 100 lbs |
| Seating Capacity | 4 |
| Maximum Speed | 174 knots |
| Fuel Capacity | 92 US gallons (348 liters) |
| Landing Gear | Tricycle, retractable |
| Wingspan | 36 ft |
| Propeller | Constant speed, 3-blade |
Specifies the maximum allowable weights for the airplane.
Defines operational airspeed limits.
Lists limitations related to the power plant.
Specifies weight limitations for the aircraft.
Defines the acceptable center of gravity range.
Outlines limitations on permitted maneuvers.
Lists limitations related to fuel usage.
Specifies the maximum certified operating altitude.
Details limitations related to flap usage.
Lists critical airspeeds for emergency procedures.
Procedures for engine failure scenarios.
Procedures for forced landing situations.
Procedures for handling fires.
Procedures for inadvertent icing encounters.
Procedures for landing gear malfunctions.
Procedures for electrical power system issues.
Lists critical speeds for normal operations.
Detailed steps for preflight inspection.
Detailed procedure for starting the engine.
Procedures before takeoff.
Procedures for enroute climb.
Procedures after landing.
Procedures for securing the airplane.
Performance data related to takeoff.
Performance data related to cruise.
Information on fuel requirements for flights.
Performance data related to landing.
Stall speeds under various conditions.
Data for takeoff distances.
