CESSNA 210N — Weight And Balance
1 weight and balance reference for the CESSNA 210N.
Overview
Loading Summary · 2019
This document provides a detailed weight and balance summary for the Cessna 210N, specifically for aircraft N611TM. It includes information on ramp, takeoff, and landing weights, as well as center of gravity (CG) calculations. The document is intended for pilots and ground crew to ensure safe loading and compliance with weight limits. It outlines the maximum allowable weights and the distribution of weight across various sections of the aircraft, which is critical for maintaining stability and performance during flight.
- Maximum ramp weight: 3,800 lbs
- Current ramp weight: 2,324.6 lbs
- Center of gravity (CG) range: 37 to 53 inches, current CG: 42.6 inches
- Front seats capacity: 450 lbs
- Total weight distribution includes various sections with specific weight limits.
1 document