Beechcraft G58 Baron — Flight Manual

This document serves as a Specification and Description manual for the Beechcraft Baron G58 aircraft, specifically for units TH-2453 and onward. It provides essential information regarding the aircraft's design, performance, and equipment, including details about the powerplant, standard equipment, and warranties. The manual is intended for general information and evaluation purposes, ensuring that users have access to the necessary specifications and operational guidelines for the Baron G58. It covers various aspects of the aircraft, including dimensions, performance metrics, structural design, systems, and avionics, making it a comprehensive resource for pilots and aviation enthusiasts.

• Maximum Ramp Weight: 5,524 lb (2,506 kg)
• Maximum Take-off Weight: 5,500 lb (2,495 kg)
• Range: 1,245 nm (2,306 km)
• Stall Speed (Flaps Down): 75 kt (139 km/h)
• Take-off Field Length: 2,300 ft (701 m)
• Landing Distance: 1,300 ft (396 m)
• Powerplant: Two Continental Motors IO-550-C engines, 300 horsepower each.