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Calcimator

VFR Flight Planner Calculator

Route planning with wind correction, groundspeed, time enroute, and fuel estimates.

About this calculator

This calculator runs the classic VFR time/speed/distance/wind problem for a single leg. It first finds the angle between the wind's direction and your intended true course, then splits the reported wind into a headwind component (wind speed times the cosine of that angle) and a crosswind component (wind speed times the sine), the same trigonometric breakdown every private pilot learns for runway wind analysis. The wind correction angle — how many degrees you must crab into the wind to track your course — comes from the arcsine of crosswind divided by true airspeed, and that angle is added to or subtracted from your course to produce the heading to fly, depending on which side the wind is pushing from.

Groundspeed here is calculated as a simplified true-airspeed-minus-headwind figure rather than the full vector triangle (which would use the Pythagorean relationship between TAS, crosswind, and groundspeed); for typical light-aircraft wind angles this simplification is close enough for flight planning, but it will run a little optimistic in strong, highly-quartering winds. Flight time, enroute fuel, and reserve fuel follow directly from groundspeed and your entered burn rate, with the VFR reserve defaulting to the FAA's 30-minute day minimum set by 14 CFR 91.151 (bump it to 45 for the regulation's night VFR minimum). Because no magnetic variation input exists, the "heading to fly" output is a true heading — you'll still need to apply your local variation and any known compass deviation before flying it.

Inputs

Results

Groundspeed (kts)

110

Flight time (min)

65.5

Headwind component (kts)0
Crosswind component (kts)15
Wind correction angle (deg)7.8
Heading to fly (deg)352.2
Enroute fuel (gal)9.3
Total fuel (gal)13.5
Fuel cost ($)$87.90

Figures current as of 2026. Source: 14 CFR 91.151 (Fuel requirements for flight in VFR conditions)

How to Use This Calculator
  1. Enter route distance (NM), true airspeed (kts), wind speed (kts), and wind direction (degrees).
  2. Set your true course (degrees) and fuel burn (GPH).
  3. Enter fuel reserve requirement (minutes) and current fuel price per gallon.
  4. Review groundspeed, flight time, head/crosswind components, wind correction angle, and required fuel.
  5. Use the wind correction angle to compute your magnetic heading before flight.

How the result changes with True airspeed (kts)

True airspeed (kts)Groundspeed (kts)Flight time (min)
5555130.9
838386.7
16516543.6
27527526.2

What each input means

Distance (NM)
Leg distance in nautical miles.
True airspeed (kts)
True airspeed at planned cruise altitude.
Wind speed (kts)
Reported or forecasted wind speed.
Wind direction (degrees)
Direction wind is coming FROM (0-360).
True course (degrees)
Desired true course over the ground.
Fuel burn (GPH)
Expected cruise fuel consumption.
VFR reserve (min)
VFR day reserve is 30 min; VFR night is 45 min.
Fuel price ($/gal)
Cost per gallon for fuel cost estimate.

What each result means

Groundspeed (kts)
Estimated groundspeed after wind correction.
Flight time (min)
Estimated enroute time for the leg.
Headwind component (kts)
Positive = headwind, negative = tailwind.
Crosswind component (kts)
Perpendicular wind component for landing considerations.
Wind correction angle (deg)
Crab angle needed to maintain course.
Heading to fly (deg)
True course adjusted for wind correction.
Enroute fuel (gal)
Fuel burned for the enroute portion.
Total fuel (gal)
Enroute + reserve fuel.
Fuel cost ($)
Estimated fuel cost for the leg.

How this is calculated

Worked example, using the default values

  1. Identify Input Parameters
    4 parameters
    Distance (NM) = 120, True airspeed (kts) = 110, Wind speed (kts) = 15, Wind direction (degrees) = 270 = 8 input(s) provided
  2. Calculate Groundspeed
    Groundspeed = max(1, tasKts - headwindComponent)
    110 = 110
  3. Calculate Flight time
    Flight time = flightTimeHrs * 60
    65.5 = 65.5
  4. Calculate Headwind component
    0 = 0
  5. Calculate Crosswind component
    15 = 15

Figures and sources

Engine last updated . Checked against 3 independently-derived tests — how we verify calculators. Built by Paul Gunder, a software engineer, not a licensed financial, medical, or legal professional.

Frequently Asked Questions

Why isn't the "heading to fly" output my magnetic heading?

The calculator only has your true course as an input — there's no magnetic variation field — so the corrected heading it outputs is a true heading. You still need to apply your local magnetic variation, and any known compass deviation, to get the heading to actually fly by compass or heading indicator.

How accurate is the simplified groundspeed calculation compared to the full wind triangle?

Groundspeed here is true airspeed minus the headwind component, a linear approximation rather than the exact vector solution (which combines TAS, crosswind, and groundspeed via the Pythagorean relationship). For typical light-aircraft wind angles the difference is small, but in strong, highly-quartering winds this method reports a slightly higher groundspeed than the true vector triangle would.

Why does the wind correction angle use arcsine instead of a full triangle solution?

Wind correction angle is the arcsine of the crosswind component divided by true airspeed, the standard approximation pilots use for mental math and the one most cross-country planning references teach. It pairs with the same simplified groundspeed method above, so both outputs stay internally consistent even though neither is the exact vector-triangle answer.

What's the difference between the VFR reserve default and what I should use at night?

The calculator defaults to 30 minutes, matching the VFR day fuel reserve requirement set by 14 CFR 91.151, but you can change the reserve-minutes input directly — bump it to 45 minutes for night VFR flights, which is the higher regulatory minimum that section of the FARs sets for after dark.

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