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Glossary

Arm

Learn what arm means in aircraft weight and balance. Discover how to measure arm, calculate moments, and ensure your CG stays within limits for safe flight.

Arm is the horizontal distance between a reference point (called the datum) and a specific location on an aircraft. It is measured in inches and used to calculate the aircraft's weight and balance.

How It Works#

Every aircraft has a datum, an imaginary vertical plane fixed by the manufacturer. All arm measurements start from this point. A location forward of the datum has a negative arm. A location aft of the datum has a positive arm.

You multiply an item's weight by its arm to get its moment. Moment is simply the turning force that item exerts around the datum. Add up all the moments and all the weights, then divide one by the other. The result tells you where the aircraft's center of gravity (CG) sits.

The CG must fall within a range the manufacturer defines. That range is called the CG envelope. If the CG lands outside it, the aircraft may be unsafe to fly.

Example in Aviation#

A pilot is loading a Cessna 172 for a cross-country flight. The front seats have an arm of 37 inches. The rear baggage compartment has an arm of 95 inches. The pilot places 50 lbs of gear in the baggage compartment. That gear produces a moment of 4,750 inch-pounds, pulling the CG aft. The pilot checks the final CG against the approved envelope in the Pilot's Operating Handbook (POH) before departure.

Why It Matters#

Getting the arm values wrong leads to an incorrect CG calculation. An aircraft loaded with the CG too far aft becomes unstable and difficult to recover from a stall. One loaded too far forward requires excessive back-pressure to rotate and may not flare properly on landing.

Arm is not just a number on a form. It is the foundation of every weight and balance calculation a pilot makes. Understanding it helps you load the aircraft safely every time.

Key Takeaways#

  • Arm is the distance, in inches, from the datum to any given point on the aircraft.
  • Forward of the datum is a negative arm; aft of the datum is a positive arm.
  • Multiply weight by arm to get moment.
  • Moments are summed and divided by total weight to find the CG location.
  • The CG must stay within the manufacturer's approved envelope for safe flight.

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