Determination should be made by using the following equation:
Ballast = Derived weight x (Required CG – Derived CG) ÷ Ballast Arm – Required CG
ACS:
AM.I.C.K9
AM.I.C.S2
AM.I.C.S3
AM.I.C.S15
Process/Skill Questions:
- Why would temporary ballast be used on an aircraft?
- What are the effects of an improper use of ballast?
- How does one determine proper ballast placement?
- How does one calculate ballast weight shift and determine the required weight location?
- How does one calculate the change needed to correct an out of balance condition?