CESSNA FR172N — Flight Manual
1 flight manual reference for the CESSNA FR172N.
Overview
Supplemental Airplane Flight Manual · 2012
This document is a Supplemental Airplane Flight Manual for the Cessna 172N, detailing modifications made under STC SA2196CE, which increases the gross weight to 2550 lbs. It is intended for pilots operating the Cessna 172N with specific engine modifications and provides essential information on limitations, procedures, and performance. The manual supplements the basic Airplane Flight Manual and should be used in conjunction with it for comprehensive operational guidance.
- Maximum certificated takeoff weight: 2550 lbs
- Engine model: O-360-A4A, A4M, A4N with 180 BHP at 2700 RPM
- Normal landing speed: 60-70 KIAS (Flaps Down)
- Emergency landing speed: 70 KIAS (Flaps Up)
- Cruise fuel consumption at 2550 lbs: 10.2 GPH at 2600 RPM
1 document