Cessna 414 Chancellor — Weight And Balance

This document provides an in-depth overview of the Cessna 414A Chancellor, detailing its performance characteristics, specifications, and operational capabilities. It is intended for pilots and aviation enthusiasts interested in understanding the aircraft's features, modifications, and operational guidelines. The Cessna 414A is a pressurized twin-engine aircraft known for its spacious cabin and versatility in various flight conditions. The document highlights the aircraft's engine specifications, performance metrics, and modifications available through RAM Aircraft, which enhance its capabilities. Additionally, it discusses the aircraft's handling characteristics, operational costs, and market positioning, making it a valuable resource for potential buyers and current owners alike.

• Maximum takeoff weight: 6,750 lbs
• Fuel capacity: 213.4 gallons (204 gallons usable)
• Rate of climb at sea level: 1,580 fpm
• Cruise speed at 75% power: 221 knots
• Engine power: 310 hp per engine