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Cessna 172M N80168 Weight and Balance

CESSNA 172M SKYHAWK · Weight And Balance

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Overview

This document provides the weight and balance information for the Cessna 172M aircraft, specifically for the serial number 17265986. It includes details about the maximum gross weight, center of gravity (CG) calculations, and the distribution of weight among various occupants and baggage areas. The document is intended for pilots and ground crew to ensure that the aircraft is loaded within safe limits before flight. It emphasizes the importance of calculating the takeoff weight and understanding the implications of weight distribution on aircraft performance.

  • Max gross weight: 2300 lbs
  • Weight distribution includes pilot, co-pilot, and two rear passengers
  • Center of gravity calculations are essential for safe flight operations

Document

Source

Originally published by wingsflightschool.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
·
2020
Pages
·
1
File size
·
344 KB
Publisher
·
wingsflightschool.com
About this document
What is the Cessna 172M N80168 Weight and Balance?

The Cessna 172M N80168 Weight and Balance is a weight and balance for the CESSNA 172M SKYHAWK, dated 2020.

How many pages is the Cessna 172M N80168 Weight and Balance?

The copy of the Cessna 172M N80168 Weight and Balance on file runs 1 pages.

Where does the Cessna 172M N80168 Weight and Balance come from?

This copy of the Cessna 172M N80168 Weight and Balance was originally published by wingsflightschool.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Cessna 172M N80168 Weight and Balance published?

The Cessna 172M N80168 Weight and Balance — the CESSNA 172M SKYHAWK weight and balance on file — is dated 2020.

Documentation completeness
5/7

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In this document

Weight and Balance Summary

The document outlines the maximum gross weight for the Cessna 172M as 2300 lbs. It details the weight distribution among the pilot, co-pilot, rear passengers, and baggage areas, which is crucial for maintaining the aircraft's center of gravity within safe limits.

Weight Distribution

The weight distribution includes the airplane itself, pilot, co-pilot, and two rear passengers, with specific weights assigned to each. The total moment and arm measurements are provided to assist in calculating the center of gravity.

Takeoff and Landing Weights

The takeoff weight is calculated by summing the weights of all occupants and baggage, subtracting the flight fuel. The document also mentions the landing weight, which is critical for ensuring compliance with safety regulations.

Safety notes

  • Ensure the aircraft is loaded within the specified weight limits to maintain safety during flight.

Full document text

Date: PIC: Max gross weight 2300 CG Baggage area 1 Cessna 172M N80168 Weight and Balance S/N 17265986 Moment Arm Weight Item Airplane Pilot Co-pilot Rear pax 1 Rear pax 2 1466.5 39.44 37 37 73 73 95 57842.38 Safety 123 48 48 Baggage area 2 Fuel Take Off Weight Checklist Landing weight Max gross 2300 Less Flight fuel Last update: 30SEP20 Flight plan Weather Glasses Fuel Maps & charts Approaches