Climb Gradient Explained: ft/NM, Percent and Feet per Minute

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Instrument departures, missed approaches and some visual departures specify a minimum climb gradient. The chart might say “Minimum climb of 350 ft per NM to 3,000” or show 4.5% in an RNAV procedure. Your vertical speed indicator shows feet per minute. This guide explains what a climb gradient means, how to convert it, and how to check whether your aircraft can meet it before you take off.

For a quick conversion, use our Climb Gradient Calculator.

Climb gradient vs rate of climb

A climb gradient is height gained per distance travelled over the ground. It is expressed in feet per nautical mile (ft/NM) or as a percentage. A rate of climb is height gained per unit of time, normally feet per minute (ft/min or fpm).

Obstacles are fixed to the ground, so procedure designers use gradient. The aircraft, however, delivers a rate of climb. The link between them is ground speed: the faster you cross the ground, the faster you must climb to stay above the same slope.

The formulas

  • Rate of climb (ft/min) = gradient (ft/NM) × ground speed (kt) ÷ 60
  • Gradient (ft/NM) = rate of climb (ft/min) × 60 ÷ ground speed (kt)
  • Percent to ft/NM: multiply by 60.76 (because 1 NM = 6,076 ft)
  • ft/NM to percent: divide by 60.76

A handy approximation: 1% is about 60 ft/NM, so 3.3% is about 200 ft/NM.

The standard 200 ft/NM

Unless a procedure states otherwise, both US TERPS and ICAO PANS-OPS assume an aircraft climbs at least 200 ft/NM (about 3.3%) after takeoff. That assumption gives obstacle clearance on standard departures. Where obstacles or airspace need more, a higher gradient is published along with the altitude to which it applies.

Gradient90 kt120 kt150 kt180 kt
200 ft/NM (3.3%)300400500600
300 ft/NM (4.9%)450600750900
400 ft/NM (6.6%)6008001,0001,200
500 ft/NM (8.2%)7501,0001,2501,500

Values are rates of climb in ft/min at each ground speed.

Checking your aircraft can make it

  1. Find the requirement on the departure procedure, including the altitude it applies to.
  2. Estimate ground speed in the climb. Start with the climb airspeed, convert to true airspeed for the altitude and temperature with our True Airspeed Calculator, then apply the wind.
  3. Convert the gradient to ft/min at that ground speed.
  4. Compare with the flight manual rate of climb for the actual weight, pressure altitude and temperature. On a hot day at a high airfield, climb performance can fall a long way; check the density altitude first.
  5. Keep a margin. Book figures are for a new aircraft flown precisely. Turbulence, a slightly rough engine or a less than perfect speed all eat into them.

Worked example

A departure requires 380 ft/NM to 4,000 ft. You will climb at 90 KIAS, which is about 96 KTAS at the altitudes involved, with a 10 kt headwind. Ground speed is about 86 kt.

Required rate of climb = 380 × 86 ÷ 60 = 545 ft/min. If the flight manual shows only 500 ft/min at today’s weight and temperature, you cannot meet the gradient. Options include waiting for cooler air, reducing weight, using a different departure or climbing in a published climb-in-holding pattern if one exists.

Headwind and tailwind

A headwind reduces ground speed, so the same rate of climb produces a steeper gradient over the ground. That is why aircraft take off into wind. A tailwind does the opposite and can turn a comfortable departure into a marginal one.

Descent works the same way

The same maths applies to descents. A 3° glidepath is about 318 ft/NM, which gives the familiar rule of thumb of descent rate ≈ ground speed × 5. Our Descent Rate Calculator handles the reverse case.

Related tools and guides

For training and general information. Use approved aircraft performance data and current published procedures for flight.

Sources and further reading

Sources checked November 2026. Rules differ between countries and change over time: for real flights, use the current publications of the authority that applies to you, your aircraft flight manual and your operator’s procedures.

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