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Cessna 172 S – Weight & Balance Work Sheet

CESSNA 172S Skyhawk · Weight And Balance

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Overview

This document is a Weight & Balance Work Sheet specifically for the Cessna 172S Skyhawk, dated July 17, 2015. It serves as a reference for pilots and ground crew to calculate the weight and center of gravity (CG) of the aircraft. The sheet includes essential data such as the Basic Empty Weight, fuel capacity, and various weight categories including pilot, passengers, and baggage. It emphasizes the importance of consulting the Pilot's Operating Handbook (POH) for accurate weight and balance calculations. The document is structured to guide users through the calculation process, ensuring safe operation within the aircraft's weight limits.

  • Basic Empty Weight: 1,702.8 lbs
  • Usable Fuel: 48.00 lbs
  • Taxi Fuel: 8.0 lbs
  • Weight calculation includes pilot, passengers, and baggage
  • Always consult the POH for accurate Weight & Balance calculations

Document

Source

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

View original at meowmeow.info

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Document details

Type
·
Weight And Balance
Year
·
2015
Pages
·
1
File size
·
420 KB
Publisher
·
meowmeow.info
About this document
What is the Cessna 172 S – Weight & Balance Work Sheet?

The Cessna 172 S – Weight & Balance Work Sheet is a weight and balance for the CESSNA 172S Skyhawk, dated 2015.

How many pages is the Cessna 172 S – Weight & Balance Work Sheet?

The copy of the Cessna 172 S – Weight & Balance Work Sheet on file runs 1 pages.

Where does the Cessna 172 S – Weight & Balance Work Sheet come from?

This copy of the Cessna 172 S – Weight & Balance Work Sheet was originally published by meowmeow.info and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Cessna 172 S – Weight & Balance Work Sheet published?

The Cessna 172 S – Weight & Balance Work Sheet — the CESSNA 172S Skyhawk weight and balance on file — is dated 2015.

Documentation completeness
5/7

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In this document

Weight Calculation

The Weight Calculation section provides a formula to determine the Takeoff Weight and CG. It starts with the Basic Empty Weight of 1,702.8 lbs and includes additional weights for front pilots, rear passengers, and baggage areas. The Zero Fuel Weight is calculated before adding usable fuel to determine the Ramp Weight.

Center of Gravity (CG) Limits

This section outlines the importance of maintaining the center of gravity within specified limits. The document indicates that the center of gravity for pilots and passengers should be positioned on adjustable seats for average occupants, with forward and aft limits provided in parentheses.

Fuel Management

The Fuel Management section details the usable fuel amount of 48.00 lbs and includes a deduction for taxi fuel of 8.0 lbs. This information is crucial for calculating the Takeoff Weight and Landing Weight, ensuring that the aircraft is within safe operational limits.

Safety notes

  • Always ensure the aircraft is within weight and balance limits before flight.
  • Consult the POH for specific weight and balance procedures.

Full document text

Cessna 172 S – Weight & Balance Work Sheet This sheet is for reference only; always consult with the aircraft POH and documented Weight & Balance. * Pilot or passenger center of gravity on adjustable seats positioned for average occupant. Numbers in parentheses indicate forward and aft limits of occupant center of gravity range. ** Arm measured to the center of the areas shown. N513WF as of 7/17/2015 WEIGHT x ARM = MOMENT Basic Empty Weight 1,702.8 41.11 70,005.54 + Front Pilots * + Rear Passengers 73.00 + Baggage Area 1 ** + Baggage Area 2 ** = Zero Fuel Weight + Usable Fuel 48.00 = Ramp Weight - Taxi Fuel 8.0 48.00 = Takeoff Weight / CG - Fuel Burn 48.00 = Landing Weight / CG

All CESSNA 172S Skyhawk weight and balance