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FAA-H-8083-1B

Aircraft Weight and Balance Handbook (WBH)

The Aircraft Weight and Balance Handbook (FAA-H-8083-1B) is a free FAA publication covering weight and balance principles, calculations, and their effects on aircraft performance. It explains how to compute center of gravity, use CG envelopes, and understand the consequences of improper loading. Essential for all pilots. Download it at no cost from FAA.gov.

Why This Document Matters

Weight and balance is one of the most critical safety topics in aviation. An aircraft loaded outside its approved weight or CG limits may be uncontrollable. The Weight and Balance Handbook is the FAA's dedicated resource for mastering these calculations. While the PHAK covers weight and balance in one chapter, this handbook goes much deeper—covering the computational method, graph method, CG shift formulas, and the effects of loading on performance. Weight and balance problems appear on every pilot knowledge test, and DPEs expect you to demonstrate proper calculations during the checkride.

Chapter-by-Chapter Guide

What each section covers and the key topics to study

1

Chapter 1: Weight and Balance Overview

Importance of weight and balance, terminology, and regulatory requirements.

Key Topics

Weight and balance terminologyRegulatory requirementsSafety implications
2

Chapter 2: Weight and Balance Fundamentals

Definitions of empty weight, useful load, arm, moment, datum, and center of gravity.

Key Topics

Empty weightUseful loadArm and datumMoment calculationsCenter of gravity
3

Chapter 3: Weighing the Aircraft

Procedures for weighing aircraft and establishing an accurate empty weight.

Key Topics

Weighing proceduresLevel positionEquipment list
4

Chapter 4: Weight and Balance Calculations

Computational method, graph method, and table method for determining CG.

Key Topics

Computational methodGraph methodCG envelopeLoading examples
5

Chapter 5: Effects of Weight on Performance

How weight affects takeoff, climb, cruise, stall speed, and landing performance.

Key Topics

Takeoff distance vs. weightStall speed increase with weightManeuvering speed changesLanding distance

Study Tips

  • Practice weight and balance calculations by hand until you can do them confidently. You will be given a scenario on your checkride and expected to compute CG.
  • Understand the difference between forward CG (more stable, higher stall speed) and aft CG (less stable, lower stall speed, potentially dangerous).
  • Memorize the formula: CG = Total Moment / Total Weight. Also know the weight-shift formula: CG change = (weight shifted x distance shifted) / total weight.
  • Always check weight and balance for both takeoff AND landing conditions. Fuel burn changes the CG position during flight.
  • On the knowledge test, read weight and balance problems carefully. Common traps include using the wrong fuel weight (avgas is 6 lbs/gal, not 8) and confusing arm with moment.

Frequently Asked Questions

Is the Weight and Balance Handbook free?

Yes, it is a free PDF available from FAA.gov.

How much does aviation fuel weigh?

Aviation gasoline (avgas 100LL) weighs 6 pounds per gallon. Jet-A fuel weighs approximately 6.7 pounds per gallon. These values are important for weight and balance calculations.

What happens if CG is too far aft?

An aft CG beyond limits reduces stability and can make the aircraft uncontrollable. In extreme cases, the nose pitches up uncontrollably and the pilot cannot recover. Aft CG is generally more dangerous than forward CG.

Do I need this if weight and balance is already in the PHAK?

The PHAK covers the basics in one chapter. The Weight and Balance Handbook provides much more detail, including multiple calculation methods, real-world examples, and an in-depth discussion of how weight affects every aspect of performance. It is recommended for thorough preparation.

Quick Facts

Document ID
FAA-H-8083-1B
Last Updated
2023
Cost
Free
Publisher
FAA

Applies To

StudentPrivateInstrumentCommercialCFIATP
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Aircraft Weight and Balance Handbook (FAA-H-8083-1B) is an official FAA publication available at FAA.gov

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