Cessna Aircraft Company Citation Bravo

This document serves as a checklist for the Cessna Citation II Bravo, a small business jet that was introduced in 1994 and certified in 1996. It provides essential information about the aircraft's history, design, performance, and operational capabilities. The checklist is intended for pilots and aviation enthusiasts, offering a comprehensive overview of the aircraft's specifications, performance metrics, and operational guidelines. Key features include details on the aircraft's engines, climb performance, cruise performance, and takeoff and landing distances, which are crucial for safe and efficient flight operations.

• Maximum takeoff weight: 14,800 lbs
• Rate of climb: 2,500 ft/min at sea level
• Maximum ceiling: 43,000 feet
• Takeoff distance (15° flaps): 3,210 feet
• Cruise speed at 33,000 feet: Mach 0.681