Weight and Balance - Cessna 210N / Sn 210-63828

CESSNA TURBO 210L · Weight And Balance

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Overview

This document provides the weight and balance information for the Cessna 210N, specifically for serial number 210-63828. It includes details on the aircraft's maximum weight, center of gravity (CG) range, and various weight adjustments based on equipment changes. The document is intended for pilots and maintenance personnel who need to ensure the aircraft is within safe operating limits for weight and balance. It outlines the empty weight, useful load, and adjustments made to the aircraft's configuration, providing critical data for flight planning and safety.

Max Takeoff Weight: 4000 lbs
Empty Weight: 2493.7 lbs
New Useful Load: 1506.3 lbs
CG Range: FWD 37.0 in, AFT 53.0 in
Total Weight after adjustments: 2943.5 lbs

Document

Source

Originally published by jaxnfc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Weight And Balance
Year: 2021
Pages: 1
File size: 42 KB
Publisher: jaxnfc.com

About this document

What is the Weight and Balance - Cessna 210N / Sn 210-63828?

The Weight and Balance - Cessna 210N / Sn 210-63828 is a weight and balance for the CESSNA TURBO 210L, dated 2021.

How many pages is the Weight and Balance - Cessna 210N / Sn 210-63828?

The copy of the Weight and Balance - Cessna 210N / Sn 210-63828 on file runs 1 pages.

Where does the Weight and Balance - Cessna 210N / Sn 210-63828 come from?

This copy of the Weight and Balance - Cessna 210N / Sn 210-63828 was originally published by jaxnfc.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Weight and Balance - Cessna 210N / Sn 210-63828 published?

The Weight and Balance - Cessna 210N / Sn 210-63828 — the CESSNA TURBO 210L weight and balance on file — is dated 2021.

Documentation completeness

4/7

Most owners only have the POH. Here's the essential set for the CESSNA TURBO 210L.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More CESSNA TURBO 210Lmanuals & documents

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In this document

Weight and Balance Summary

The document summarizes the weight and balance for the Cessna 210N, indicating a maximum takeoff weight of 4000 lbs. The center of gravity (CG) range is specified as forward at 37.0 inches and aft at 53.0 inches. The empty weight is recorded at 2460.2 lbs with a CG of 44.2 inches.

Weight Adjustments

The document details weight adjustments made to the aircraft, including the removal of a radio box weighing 1.0 lb and the addition of an audio stack weighing 5.0 lbs, along with rear seat and belts weighing 29.5 lbs. These adjustments result in a new empty weight of 2493.7 lbs and a new CG of 44.8 inches.

Total Weight Calculation

After accounting for the adjustments, the total weight of the aircraft is calculated to be 2943.5 lbs with a CG of 44.8 inches. The moment is calculated at 111,698.64.

Full document text

Weight and Balance Cessna 210N / Sn 210-63828 Previous Weight and Balance Dated 28 July, 2020 Max Weight 4000LBS CG Range FWD 37.0 AFT 53.0 Item Weight ARM MOMENT Empty Weight 2460.2 CG 44.2 108712.14 Remove A< Radio Box 1.0 Lbs 138” -138 ADD Audio Stack 5.0 40” +200 Rear Seat & Belts 29.5 101” +2979.5 TOTAL 2943.5 CG 44.8 111,698.64 Max T/O Weight 4000 New Empty Weight 2493.7 New Empty Weight CG 44.8 New Useful Load 1506.3 Gilbert Wood A&P/IA 3444134 Date: 10/1/2021

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