Cessna Citation VI — Weight & Balance

This document outlines the operating limitations for the Cessna Citation VI (Model 525). It provides essential information regarding weight limitations, center-of-gravity limits, powerplant limitations, and other critical operational parameters necessary for safe flight operations. The manual is intended for pilots and maintenance personnel who require detailed knowledge of the aircraft's performance and operational constraints. It includes specific data on weight and balance, engine operating limits, and various speed limitations, ensuring that operators can comply with safety regulations and maintain optimal performance during flight.

• Maximum Design Ramp Weight: 10,700 lbs
• Maximum Takeoff Weight: 10,600 lbs
• Maximum Landing Weight: 9,800 lbs
• Engine Type: Williams International FJ44-1A Turbofan
• Maximum Operating Speed: 0.710 Mach above 30,500 ft