Performance Data for Cessna 210 Centurion
Cessna 210 Centurion · Performance Data
Overview
This document provides performance data specifically for the Cessna 210 Centurion. It is designed for pilots and aviation enthusiasts who require detailed information about the aircraft's capabilities, including speed, range, fuel consumption, and other critical performance metrics. The data is essential for flight planning and operational efficiency, ensuring that pilots can make informed decisions based on the aircraft's performance characteristics. The document is structured to present the information clearly and concisely, allowing for quick reference during pre-flight preparations and in-flight operations.
- Maximum takeoff weight: 3,600 lbs (1,633 kg)
- Maximum cruise speed: 160 knots (184 mph or 296 km/h)
- Range: 800 nautical miles (1,540 km)
- Fuel consumption: 15 gallons per hour (56.8 liters per hour)
- Rate of climb: 1,000 feet per minute (5.08 m/s)
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Aircraft Specifications
The Cessna 210 Centurion features a high-wing design with a maximum takeoff weight of 3,600 lbs (1,633 kg). It is powered by a Lycoming IO-540-U4A5 engine, providing 300 horsepower. The aircraft has a wingspan of 36 feet 0 inches (10.97 m) and a length of 27 feet 2 inches (8.28 m).
Performance Metrics
The Cessna 210 Centurion has a maximum cruise speed of approximately 160 knots (184 mph or 296 km/h) at 75% power. The stall speed in landing configuration is around 55 knots (63 mph or 102 km/h). The aircraft has a range of approximately 800 nautical miles (1,540 km) with standard fuel reserves.
Fuel Consumption
At a cruise power setting, the Cessna 210 Centurion consumes about 15 gallons per hour (56.8 liters per hour). This consumption rate can vary based on weight, altitude, and environmental conditions.
Climb Performance
The aircraft has a rate of climb of approximately 1,000 feet per minute (5.08 m/s) at sea level under standard conditions. This performance allows for efficient ascent to cruising altitude.
Landing and Takeoff Distances
The takeoff distance over a 50-foot obstacle is approximately 1,800 feet (549 m), while the landing distance over the same obstacle is about 2,200 feet (671 m). These distances are critical for evaluating suitable airfields.
Safety notes
- Ensure weight and balance calculations are completed before flight.
- Monitor fuel levels to avoid running out during flight.