CESSNA 172M — Flight Manual

This Supplemental Airplane Flight Manual is specifically designed for the Cessna 172M, detailing modifications made under FAA STC SA2196CE. The manual outlines the operational parameters and limitations for aircraft modified to increase the maximum takeoff weight to 2550 lbs and restrict flap travel to 30 degrees. It includes essential information for pilots regarding engine specifications, performance data, emergency procedures, and weight and balance considerations. The manual is crucial for ensuring safe operations of the modified aircraft and is approved by the FAA, making it a reliable reference for pilots and aviation enthusiasts alike.

• Maximum certificated takeoff weight: 2550 lbs
• Engine: Lycoming O-360 series, 180 BHP at 2700 RPM
• Flap travel limited to 30 degrees
• Normal category flight load factors: +3.8g, -1.52g
• Emergency landing approach speed: 71-83 MPH IAS with flaps down