CESSNA P-210 Pressurized Centurion II — Specifications

This document provides specifications for the Cessna P210R Pressurized Centurion, a single-engine aircraft known for its pressurized cabin and performance capabilities. It is designed for pilots and aviation enthusiasts seeking detailed information about the aircraft's engine, fuel capacity, weights, and performance metrics. The specifications include critical data such as engine model, fuel requirements, weight limits, and performance characteristics, making it a valuable reference for operational planning and understanding the aircraft's capabilities.

• Engine Model: Continental TSIO-520-CE, 6 cylinders, 325 HP
• Fuel Capacity: 90 gallons (120 gallons with long-range tanks)
• Takeoff Weight: 4,100 lbs; Landing Weight: 3,900 lbs
• Max Structural Cruising Speed: 167 KIAS
• Stall Speed Clean: 65 knots; Stall Speed Landing Configuration: 55 knots
• Best Rate of Climb: 1,150 FPM; Service Ceiling: 25,000 ft