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General| Manufacturer | Beechcraft |
|---|---|
| Model | Baron G58 |
| Horsepower | 300 hp each |
| Length | 29 ft 10 in (9.09 m) |
| Wingspan | 37 ft 10 in (11.53 m) |
| Seating Capacity | 6 |
| Avionics | Garmin G1000 NXi |
| Maximum Speed | 202 knots (232 mph, 374 km/h) |
| Rate of Climb | 1, 700 ft/min (8.6 m/s) |
| Fuel Capacity | 194 gallons |
| Service Ceiling | 20, 688 feet |
Lists operational airspeed limits (VNE, VNO, VA, VFE, VLO/VLE, VMCA, VSO, VX, VY) and their respective speeds.
Details engine limitations including number, manufacturer, model, type, operating limits, and starter procedures.
Specifies maximum takeoff, landing, and ramp weights, as well as maximum baggage compartment weights.
Outlines minimum airspeeds and ambient temperatures for deicing boot operation, and limitations for severe icing conditions.
Provides procedures for engine failure, including controllability, climb performance, and securing the engine.
Details procedures for engine fires occurring on the ground or in flight, including shutdown steps.
Outlines the procedure for an emergency descent, including airspeed and flap settings.
Covers specific system emergencies like electrical smoke/fire, alternator failure, and load shedding.
Provides instructions for attempting an in-flight engine restart.
Details procedures for one-engine-inoperative landings and gear-up landings.
Outlines the critical checks and procedures to be performed during the engine runup before takeoff.
Provides methods to determine maximum takeoff weight for positive one-engine-inoperative climb at liftoff.
Covers ice accumulation intensity, effects on performance, and procedures for exiting icing conditions.
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