Module MOD-06 · 7 min · ACS PA.I.F

How CG Position Affects Handling

Weight, Balance and Aircraft Performancedraft — pending CFI review

Why this matters in flight: The same airplane flies very differently depending on where the CG sits. Understanding the trade-offs explains why the limits exist and why exceeding them is dangerous rather than merely inconvenient.

Center of gravity position is a balance between stability and controllability. A forward CG makes the airplane more stable — it wants to return to level flight — but the tail must pull down harder, which raises the stall speed, adds drag, and demands more elevator force to flare. Too far forward and there may not be enough elevator to hold the nose up at landing speed. An aft CG does the opposite: it makes the airplane lighter on the controls and more efficient, and it lowers the stall speed, but it reduces stability so the airplane is less willing to recover on its own. Too far aft and stall or spin recovery can become difficult or impossible. This is why the aft limit is the more safety-critical of the two and why the approved envelope must never be exceeded in either direction.

Key terms

Longitudinal stability
The pitch tendency of the airplane to return to trimmed flight.
Forward limit
The most forward CG allowing adequate elevator authority.
Aft limit
The most rearward CG at which the airplane remains safely controllable.

Summary

Forward CG = more stable, higher stall speed, heavier controls; aft CG = less stable, lower stall speed, harder recovery. Stay within both limits.

Quick check ▾

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What is one effect of loading an airplane with a more forward center of gravity?

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Sources

Every claim traces to a source — paraphrased knowledge elements pointing at the governing FAA publication; not yet verified against a retrieved source.

  • FAA-H-8083-3 (stability) Airplane Flying Handbook unverified
  • FAA-H-8083-3 (stability) Airplane Flying Handbook unverified
  • FAA-H-8083-1 Ch. 4 Aircraft Weight and Balance Handbook unverified

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