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Test Figures

How to Read FAA Test Figures: Weight and Balance and Performance Charts

Aviator IQ Editorial TeamUpdated September 23, 20269 min read
An FAA aeronautical chart showing airspace, frequencies, and terrain
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Figure questions are mechanical, not conceptual

The most common thing students say about the written is some version of this: I understand the concepts, but I keep missing the figure and chart questions. That gap is real, and it is almost never a theory problem. It is a reading problem.

Trace the wrong answers and they cluster in the same few places: an entry value pulled from the wrong line of the scenario, a graph entered on the wrong axis, a value read straight off the nearest printed line instead of interpolated between two of them, or a dense table scanned into the wrong row. None of those are gaps in what weight and balance or density altitude mean. They are slips in how the figure was read.

It is also harder than it used to be. The FAA knowledge test is delivered on a computer through PSI, and the figures now live in an on-screen supplement rather than a printed booklet you could hold up to the light and trace with a finger. The image can be low-resolution, the reference lines are thinner on a screen, and you cannot lay a pencil across the graph. The fix is a method you run the same way every time, so the reading stops depending on how clean the picture happens to look.

The universal method for any figure

Every figure question, weight and balance or performance, yields to the same sequence. Run all of it, in order, even when a step feels obvious. The steps you skip are the ones the trap answers are built around.

Run these eight steps on every figure question
  1. 1Separate given from asked. Read the question once for what the figure hands you and once for what it wants back. Circle the units on the answer, because that is what you are solving for.
  2. 2Pull the correct entry value from the scenario. Most misses happen here. Match each number to the right variable, and watch for pressure altitude versus indicated altitude, or gross weight versus empty weight.
  3. 3Enter the graph on the correct axis. Confirm which axis is your starting variable before you draw anything. Charts usually start at the bottom or left edge.
  4. 4Follow the reference and guide lines exactly. Track the curved or angled reference lines the chart provides. Turn where they turn, and do not cut a straight line across a curved family of lines.
  5. 5Interpolate between the printed lines. Your value almost never lands on a labeled line. Estimate its position between the two nearest lines rather than snapping to the closer one.
  6. 6Carry the value across to the answer axis. Move from your interpolated point to the output scale, keeping your line square to the axes.
  7. 7Convert units if the answer scale asks for it. Feet versus meters, knots versus miles per hour, pounds versus gallons. Convert before you compare to the choices.
  8. 8Sanity-check the magnitude. Ask whether the number is even plausible. A takeoff roll of 40 feet or a CG far outside the envelope means you read something wrong, so go back before you commit.

Weight and balance: loading graph plus CG envelope

A weight and balance problem is two figures working together. A loading graph or a table turns each load into a moment, and a center of gravity envelope tells you whether the totals land in a legal box. The whole thing rests on one relationship.

The two relationships behind every W and B problem
weight × arm = momentDo that for every station, add up the weights and the moments, then:CG = total moment / total weight

The arm is the distance of a station from the datum. Compute a moment for each station, the empty airplane, the front seats, the rear seats, the fuel, the baggage, then total both columns and divide. The result is a single weight and a single CG. Plot that one point on the envelope. If it falls inside the envelope, the airplane is loaded legally. If it falls outside, it is not, no matter how reasonable each individual load looked.

Worked example (illustrative numbers, not from any FAA figure)
These figures are made up to show the method. Read your own values off the actual test figure.Empty airplane: 1,500 lb × 38.0 in = 57,000 in-lbFront seats: 340 lb × 37.0 in = 12,580 in-lbRear seats: 170 lb × 73.0 in = 12,410 in-lbFuel: 240 lb × 48.0 in = 11,520 in-lbBaggage: 50 lb × 95.0 in = 4,750 in-lbTotal the two columns:total weight = 1,500 + 340 + 170 + 240 + 50 = 2,300 lbtotal moment = 57,000 + 12,580 + 12,410 + 11,520 + 4,750 = 98,260 in-lbCG = 98,260 / 2,300 = 42.7 in aft of datumNow plot 2,300 lb at 42.7 in on the envelope and confirm the point sits inside it.

One thing to expect on the real figures: many FAA loading graphs and CG envelopes are scaled in moment index, meaning moment divided by 1,000, to keep the numbers small. Read the axis label and stay consistent. The scaling does not change your answer, because that same factor cancels out when you divide moment by weight to get the CG.

Performance charts: the entry values and the missed interpolation

Performance charts all follow the same enter, turn, read pattern. What separates a right answer from a wrong one is using the correct entry values and interpolating the one place students routinely read straight off a printed line. Here is what to enter, and the interpolation to watch, for the four you will meet most.

ChartEntry valuesThe interpolation students miss
Density altitudePressure altitude and outside air temperatureTemperature between the printed isotherms, not the nearest one
Takeoff or landing distancePressure altitude, temperature, weight, then wind and runway slopeWeight and wind between the guide lines, applied in the given order
Crosswind componentWind speed and the angle between wind and runwayThe angle between the printed radial lines (for example 30 and 45 degrees)
Cruise power tablePressure altitude, RPM or manifold pressure, and temperatureAltitude between two tabulated rows, not just the closest row
What each chart asks you to enter and the interpolation that trips people up. Values on the real test come from the figure supplied.

Two ordering habits matter across all of them. Correct for pressure altitude and temperature before you read a distance, never after. And when a chart lists adjustments, weight, then wind, then runway surface, apply them in that stated order, because the guide lines are drawn to be followed in sequence.

Interpolation, the simple version

Interpolation sounds like math and is really just splitting the difference. Your value sits somewhere between two printed lines. Find what fraction of the way it is between them, and move the output by that same fraction.

The one interpolation formula you need
value = low + fraction × (high − low)where the fraction is how far your input sits between the two printed lines.
Tiny worked example (illustrative numbers)
A chart prints takeoff distance at 2,000 lb (1,000 ft) and 2,400 lb (1,400 ft). Your weight is 2,300 lb. How far between the two lines is that?fraction = (2,300 − 2,000) / (2,400 − 2,000) = 300 / 400 = 0.75value = 1,000 + 0.75 × (1,400 − 1,000)value = 1,000 + 0.75 × 400 = 1,000 + 300 = 1,300 ftThree-quarters of the way up in weight, three-quarters of the way up in distance. That is all interpolation is.

Reading the on-screen figure supplement

The fix is reps with worked solutions

Method plus repetition is what turns figure questions from the category you dread into reliable points. You do not need to read more theory. You need to run the eight steps on figure after figure until the sequence is automatic, checking each answer against a worked solution so you catch the exact step where a miss happened. The Private Pilot practice test serves figure questions with the figure shown inline and a step-by-step explanation on every answer, so you drill the reading method with the picture right there and see precisely where a trace went wrong.