CESSNA 414 — Weight And Balance

This document provides a revised weight and balance and equipment list for the Cessna 414 aircraft, specifically for the aircraft identified as N414TRIP. It outlines the weight changes due to various equipment additions and modifications, including pilot and passenger seating, catering storage, baggage, and fuel loads. The document is essential for pilots and operators to ensure compliance with weight limits and to maintain safe operational parameters during flight. It includes critical weight data such as zero fuel weight, computed takeoff weight, and center of gravity calculations, which are vital for flight planning and safety.

• Original weight: 4,851.05 lbs
• Total weight after modifications: 6,760.10 lbs
• Max ramp weight: 6,800 lbs
• Max takeoff weight: 6,765 lbs
• Max landing weight: 6,430 lbs
• Max zero fuel weight: 6,165 lbs
• Required fuel burn to land at max landing weight: 335 lbs (approx. 58 gallons)