Cessna Citation Mustang — Flight Manual

This Flight Planning Guide is specifically designed for the Cessna Citation Mustang (Model 510). It provides essential performance data derived from the Aircraft Flight Manual and Operating Manual. The guide is intended for pilots and aviation professionals to assist in evaluating the aircraft's performance capabilities. It includes critical information on takeoff, climb, cruise, descent performance, and reserve fuel calculations, ensuring that users can make informed decisions during flight planning. The data presented is subject to change and should not replace the FAA-approved Aircraft Flight Manual or Operating Manual.

• Maximum Takeoff Weight: 8,645 lb (3,921 kg)
• Takeoff Distance at Sea Level (Flaps 15°): 3,110 ft (948 m)
• Rate of Climb (2 Engines): 3,010 ft/min (917 m/min)
• Cruise Speed at 35,000 ft: 332 KTAS
• VFR Fuel Reserve (Day): 291 lb