Cessna 414 Chancellor — Type Certificate

This document serves as the Type Certificate Data Sheet for the Cessna 414 Chancellor. It provides essential information regarding the aircraft's certification, specifications, and operational limitations. This data sheet is intended for use by pilots, maintenance personnel, and aviation enthusiasts who require detailed knowledge about the Cessna 414 Chancellor's design and performance characteristics. Key information includes weight limits, engine specifications, and safety regulations that must be adhered to during operation.

• Maximum takeoff weight: 5,000 lbs (2,268 kg)
• Maximum cruise speed: 200 knots (230 mph)
• Stall speed: 65 knots (75 mph)
• Service ceiling: 25,000 ft (7,620 m)
• Fuel capacity: 110 gallons (416 liters)