CESSNA 210N — Weight & Balance
1 weight & balance reference for the CESSNA 210N.
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.
How many Weight & Balance documents does Sprinkle have for the CESSNA 210N?
Sprinkle has 1 Weight & Balance document on file for the CESSNA 210N.
What year is the CESSNA 210N Weight & Balance?
The CESSNA 210N Weight & Balance on file is dated 2019.
How many pages is the CESSNA 210N Weight & Balance?
The CESSNA 210N Weight & Balance runs 2 pages.
Where does Sprinkle's CESSNA 210N Weight & Balance come from?
This CESSNA 210N Weight & Balance was originally published by 1979cessna210.com and is hosted on Sprinkle with full text and specs.