CESSNA 172H — Flight Manual

This document is a Supplemental Airplane Flight Manual for the Cessna 172 P, specifically for aircraft modified under STC SA2196CE, which allows for an increased maximum gross weight of 2550 lbs. It is intended for pilots operating this modified aircraft and provides essential information regarding limitations, procedures, and performance data that supplements the basic Airplane Flight Manual. The manual includes critical operational data such as engine specifications, weight limits, airspeed indicators, and emergency procedures, ensuring safe and efficient operation of the aircraft under the new configuration. The manual is FAA approved and must be used in conjunction with the original Pilot Operating Handbook.

• Maximum certificated takeoff weight: 2550 lbs.
• Engine: O-360 series, 180 BHP at 2700 RPM.
• Normal climb-out speed: 75-85 KIAS.
• Emergency landing speed: 70 KIAS (flaps up), 65 KIAS (flaps down).
• Maximum landing weight: 2550 lbs.