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Weight & Balance

Why weight & balance

Definition

Every flight has two independent limits, not one: the airplane must be at or under its maximum gross weight, AND its center of gravity must fall inside the approved envelope. An airplane can be comfortably under gross and still be dangerously out of balance.

Explanation

Weight affects performance — an overloaded airplane takes more runway, climbs worse, and stalls faster. Balance affects control and stability — where the weight sits front-to-back sets how the airplane handles and how it recovers from a stall or spin. This is the payoff of the Module 2 stability lesson: weight and balance is how you confirm the CG is where the designer needs it, on every single flight.

Figure 10-3. Determining moment.
Figure 10-3 · FAA-H-8083-25C, Pilot's Handbook of Aeronautical Knowledge (p. 250)

Why it matters

Loading is one of the few safety items entirely in your control before you ever start the engine. Getting it wrong can make an airplane that flies fine on paper unsafe.

A DPE might ask

  • What two limits does weight and balance confirm?
  • Can an airplane be within gross weight but still unsafe to fly? How?
The vocabulary

Definition

Weight and balance has a small, precise vocabulary. The datum is a reference line the manufacturer picks; an arm is the distance from the datum to something; a moment is weight times arm; and the center of gravity is the total moment divided by the total weight — the balance point of the loaded airplane.

Explanation

Empty weight is the airplane with all fluids but no people, bags, or usable fuel; useful load is max gross minus empty weight, and payload is what's left after fuel. Usable fuel weighs about 6 pounds per gallon (avgas). You get your airplane's empty weight, arm, and moment from the current weighing recorded in the POH equipment list — not the sample figures in the handbook.

TermWhat it means
Datum The reference line the manufacturer measures everything from (often the firewall or spinner).
Arm The distance from the datum to an item's location, in inches.
Moment Weight × arm. It measures the turning effect of a weight about the datum.
Center of gravity (CG) Total moment ÷ total weight — the balance point of the loaded airplane.
Empty / useful load Empty weight is the airplane with fluids but no payload or usable fuel; useful load = max gross − empty weight.

Why it matters

Every W&B computation is just these terms applied in a table. Get the vocabulary and the math is bookkeeping.

A DPE might ask

  • Define datum, arm, moment, and CG.
  • What's the difference between empty weight, useful load, and payload?
The CG envelope

Definition

The CG envelope is the approved region of center of gravity versus weight — the shape your loaded point must fall inside. It captures both limits at once: the top is max gross weight, and the sides are the forward and aft CG limits.

Explanation

Where the CG sits changes how the airplane flies. A forward CG makes it more stable but gives heavier controls, a higher stall speed, and a harder flare. An aft CG makes it less stable and twitchier, and — most importantly — degrades stall and spin recovery, which is why the aft limit is the more dangerous one to exceed. Real POH envelopes are sometimes plotted against moment (as here) or slope with weight; this course's calculator uses the simpler conservative box, and using the most-restrictive forward limit is always safe.

Figure 10-8. CG moment envelope.
Figure 10-8 · FAA-H-8083-25C, Pilot's Handbook of Aeronautical Knowledge (p. 252)

Why it matters

Reading the envelope is how you turn a computed CG into a go/no-go decision. The aft limit especially is a hard safety boundary.

A DPE might ask

  • What does the CG envelope show?
  • Compare the effects of a forward vs an aft CG.
Compute it

Definition

Computing weight and balance is a table: list every item (the empty airplane, front seats, rear seats, baggage, fuel), write each one's weight and arm, multiply to get each moment, add up the weights and the moments, and divide the total moment by the total weight to get the CG. Then check the total against max gross and the CG against the envelope.

Explanation

The calculator below does exactly that with your airplane's numbers. Enter what you're carrying and it computes each moment, the totals, and the CG, then plots your point on the envelope and tells you whether you're within limits. Fill in your airplane's constants (empty weight, arms, limits) in My Aircraft first.

Why it matters

Doing the computation for real — with your airplane — is what turns W&B from a formula into a habit you trust.

A DPE might ask

  • Walk me through a weight and balance computation.
  • How do you find the CG from the moments and weights?
Out of limits

Definition

Exceeding either limit is a real hazard. Overweight erodes performance and structural margin; an out-of-CG loading degrades handling — and an aft-CG loading can leave the airplane barely recoverable from a stall or spin even when it isn't overweight.

Explanation

Overloaded, the airplane needs more runway, climbs poorly, stalls at a higher speed, and has less structural reserve. Too far aft, it's unstable and its stall/spin recovery is degraded; too far forward, it's nose-heavy with heavy controls, a higher stall speed, and maybe not enough elevator to flare. The fix is always the same: reduce or redistribute the load — move weight, offload baggage, or adjust fuel — until both weight and CG are legal.

Out of limitsWhat happens
Overweight Longer takeoff roll, reduced climb, higher stall speed, less structural margin — the book numbers no longer apply.
CG too far aft Less stable and twitchy in pitch, and dangerously degraded stall/spin recovery. The more hazardous limit to exceed.
CG too far forward Nose-heavy: heavier controls, higher stall speed, and you may run out of elevator to flare.
The fix Reduce or redistribute the load (move or offload weight, adjust fuel) until both weight and CG are within limits.

Why it matters

Knowing WHICH way you're out of limits tells you how the airplane will misbehave and how to fix it before you fly.
Common error

A common misconception is that staying under max gross weight means you're safe to fly. You can be well under gross and still outside the CG envelope — an aft-CG loading with light fuel and rear-seat passengers is the classic trap. Always check BOTH the weight and the CG.

Your airplane is 200 lb under max gross, but the CG is 0.5 in aft of the aft limit. Is it safe to fly as loaded?

A DPE might ask

  • What are the effects of being overweight? Of an aft CG? A forward CG?
  • How do you correct an out-of-limits loading?
Weight & balance wrap

Definition

Weight and balance is a pre-flight habit, not a one-time calculation. Do it for the airplane as you'll actually load it, and remember that burning fuel moves the CG — so you check both takeoff and landing.

Explanation

Use your airplane's current empty weight and arm from the most recent weighing in the POH equipment list, not the sample numbers in the handbook, because equipment changes shift them. The numbers you saved in My Aircraft feed the calculator — keep them current, and re-run the numbers whenever the loading is unusual. Confirm both limits, every flight.

Weight & balance habitDetail
Two limits, every flight Confirm total weight ≤ max gross AND CG inside the envelope — being under gross is not enough.
Takeoff and landing Fuel burn shifts the CG, so check both ends of the flight.
Use current data Use your airplane's current empty weight/arm from the latest weighing in the POH equipment list — not the sample in the book.
Your profile The numbers you saved in My Aircraft feed the calculator — keep them current.

Why it matters

The pilots who get caught out are the ones who assumed a loading was fine. A two-minute computation is the whole defense.

A DPE might ask

  • Why check weight and balance for both takeoff and landing?
  • Where do you get your airplane's empty weight and arm?
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