CESSNA 172P SKYHAWK — Performance Data

This document provides the performance specifications for the Cessna 172P Skyhawk, detailing critical performance metrics necessary for pilots and operators. It includes data on speed, climb rates, takeoff and landing distances, weight limits, fuel capacities, and engine specifications. The information is essential for flight planning and operational safety, ensuring pilots understand the aircraft's capabilities under various conditions. The performance figures are based on standard atmospheric conditions and are derived from documented flight tests. This manual is intended for pilots, flight instructors, and aviation enthusiasts seeking detailed operational data on the Cessna 172P.

• Maximum speed at sea level: 123 knots
• Rate of climb: 700 feet per minute
• Maximum takeoff weight: 2550 lbs
• Standard empty weight: 1433 lbs
• Usable fuel capacity: 40 gallons in standard tanks
• Ground roll for takeoff: 890 feet
• Service ceiling: 13,000 feet