Cessna Citation CJ3 — Weight And Balance

This document provides critical operating limitations for the Cessna Citation VI (Model 525B), including weight limitations, center-of-gravity limits, and engine operating limits. It is intended for pilots and maintenance personnel to ensure safe operation of the aircraft. The document outlines maximum design weights for ramp, takeoff, landing, and zero fuel, as well as specific procedures for weight and balance calculations. Additionally, it includes important information regarding engine performance, temperature limits, and operational limits for various flight conditions. Compliance with these limitations is essential for maintaining airworthiness and safety during flight operations.

• Maximum Design Ramp Weight: 14,070 lbs
• Maximum Design Takeoff Weight: 13,870 lbs
• Maximum Design Landing Weight: 12,750 lbs
• Maximum Design Zero Fuel Weight: 10,510 lbs
• Maximum Operating Altitude: 45,000 feet