Title: Determine location and amount of ballast needed to stay within the weight and balance envelope.
Course: Aviation Maintenance Technology II (20114-II) > Section: Demonstrating Aircraft Weight and Balance Procedures

Determination should be made by using the following equation:

Ballast = Derived weight x (Required CG – Derived CG) ÷ Ballast Arm – Required CG

Process/Skill Questions:

- Why would temporary ballast be used on an aircraft?
- What are the effects of improper use of ballast?