W&B · Chapter 2
W&B 2-1
Page 2-1
This reproduces published FAA reference text for study. It does not replace the current official FAA publication or regulation.
Introduction Weight and balance in aircraft is based on the law of the lever. This chapter discusses the application of the law of the lever and its applications relative to locating the balance point of a beam or lever on which various weights are located or shifted. The chapter also discusses the documentation pertaining to weight and balance that is furnished by the Federal Aviation Administration (FAA) and aircraft manufacturers. Weight and Balance Theory Chapter 2
Retrieved from ecfr.gov on July 18, 2026.