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Downloaded from http://www.everyspec.com NAVAL 011B50 USAF TO 11B50 USCG TO 11B50 ARMY TM 55150034223 JOINT SERVICE TECHNICAL MANUAL AIRCRAFT WEIGHT AND BALANCE SUPERSEDE NOTICE. This manual supersedes

How to fill out aircraft weight and balance

How to fill out aircraft weight and balance:

1. Obtain the aircraft's empty weight: This is typically found in the aircraft's documentation or you can get it from the aircraft maintenance records.
2. Determine the weight of the fuel on board: Measure or estimate the amount of fuel in the aircraft's tanks and convert it to weight using the specific gravity of the fuel.
3. Calculate the weight of the occupants: Add up the weight of all individuals on board the aircraft, including the pilot, co-pilot, passengers, and any crew members.
4. Determine the weight of the cargo: If there is any cargo or baggage on the aircraft, measure or estimate its weight and include it in the calculations.
5. Calculate the total weight: Add up the empty weight, fuel weight, occupant weight, and cargo weight to get the total weight of the aircraft.
6. Determine the arm (moment) for each weight component: The arm is the horizontal distance from a reference point (usually the datum point) to the center of gravity of the weight component. Consult the aircraft's weight and balance manual or charts to find the arm for each component.
7. Compute the moment for each weight component: Multiply the weight of each component by its corresponding arm to get the moment. The moment is calculated using the formula Moment = Weight x Arm.
8. Calculate the total moment: Add up the moments of all weight components to get the total moment.
9. Determine the empty weight center of gravity (CG): The empty weight CG is usually provided in the aircraft's weight and balance manual. It is the point where the airplane would balance if it were empty. Consult the manual to find the empty weight CG location.
10. Calculate the loaded weight center of gravity (CG): Use the total weight and total moment to determine the loaded weight CG. The loaded weight CG position is found using the formula CG = Total Moment / Total Weight.
11. Plot the loaded weight CG on the weight and balance graph: Use the provided graph or worksheet to plot the loaded weight CG position. This will show if the aircraft is within its acceptable CG limits.

Who needs aircraft weight and balance?

1. Pilots: It is essential for pilots to understand and calculate aircraft weight and balance to ensure the safe operation and performance of the aircraft. They need to know the weight limits and the distribution of weight to maintain stability and control during flight.
2. Aircraft operators: Companies or individuals that own or operate aircraft are responsible for ensuring compliance with weight and balance requirements. They need to maintain accurate records of the aircraft's weight and balance to fulfill regulatory obligations and ensure the safety of the flight.
3. Aviation authorities: Regulatory bodies, such as the Federal Aviation Administration (FAA), require aircraft operators to comply with weight and balance regulations. They may conduct inspections and audits to ensure that aircraft are operated within safe weight limits and that proper weight and balance calculations are performed.

For pdfFiller’s FAQs

What is aircraft weight and balance?

Aircraft weight and balance refers to the distribution of weight and center of gravity within an aircraft to ensure safe operation and performance.

Who is required to file aircraft weight and balance?

Pilots, aircraft owners, and operators are required to file aircraft weight and balance.

How to fill out aircraft weight and balance?

Aircraft weight and balance is typically filled out using specific forms provided by the aviation authority or aircraft manufacturer.

What is the purpose of aircraft weight and balance?

The purpose of aircraft weight and balance is to ensure the safety, stability, and performance of the aircraft during flight.

What information must be reported on aircraft weight and balance?

Information such as the weight of the aircraft, distribution of weight, and center of gravity position must be reported on aircraft weight and balance.

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