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Required Climb Rate from Gradient (the AIM Table, Live)

A departure says 'minimum 350 ft/nm': enter it with your ground speed and get the VSI number you must beat — the AIM 5-2-9 table as a calculator.

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Required rate of climb (ft/min)
0
At 75 kt GS it would be (ft/min)
0
At 120 kt GS it would be (ft/min)

The table's quiet lesson: slowing down lowers the required rate. If the airplane can't make the number at cruise-climb speed, Vy — or even Vx — may still satisfy the gradient. Ground speed is the lever.

Formula

required ft/min = gradient (ft/nm) × GS (kt) / 60
References: FAA AIM 5-2-9 (instrument departure climb gradients); FAA TERPS Order 8260.3 (departure-procedure gradient basis)

⚠️ For planning and education only. Weight & balance must be computed from YOUR aircraft's actual empty weight, arm and current equipment list, and verified against the POH/AFM envelope before flight.

A departure says 'minimum 350 ft/nm': enter it with your ground speed and get the VSI number you must beat — the AIM 5-2-9 table as a calculator.

About Required Climb Rate from Gradient (the AIM Table, Live)

The chart demands feet per mile; your VSI reports feet per minute; the AIM's conversion table bridges them at fixed speeds — this calculator does it at yours, exactly. Enter the published gradient and your climb ground speed for the VSI target you must sustain, with two reference speeds shown so the core insight is unmissable: the required rate scales with how fast you cross the miles.

How to use Required Climb Rate from Gradient (the AIM Table, Live)

  1. 1Enter — sensible defaults are pre-filled so you see a worked result immediately.
  2. 2Read the live results: .
  3. 3Check the "With your numbers" line to see the formula required ft/min = gradient (ft/nm) × GS (kt) / 60 substituted step by step.
  4. 4Adjust inputs (or flip the unit toggle) until the scenario matches yours, then copy or share the result.

Why use Required Climb Rate from Gradient (the AIM Table, Live)?

  • Instant, free and private — every calculation runs in your browser, nothing is uploaded
  • Built on the published formula required ft/min = gradient (ft/nm) × GS (kt) / 60 with sources cited on the page
  • The table's quiet lesson: slowing down lowers the required rate. If the airplane can't make the number at cruise-climb speed, Vy — or even Vx — may still satisfy the gradient. Ground speed is the lever.
  • Switch units, tweak any input and watch every result update live

Frequently asked questions

Where do these required gradients come from?+

TERPS obstacle evaluation: when terrain or towers penetrate the standard 40:1 departure surface (152 ft/nm, protected by requiring 200), the procedure publishes the steeper gradient that clears them — '410 ft/nm to 8,400' — sometimes with a low-close-in obstacle note besides. The number is the mountain's geometry translated into your contract.

Can I just climb at Vx and ignore the math?+

Vx maximizes gradient through the air — necessary but not sufficient. The requirement is over the ground: a tailwind on departure dilutes even a Vx climb's ft/nm (and density altitude erodes the rate itself). Compute the required fpm at your actual GS, compare with honest aircraft performance at today's weight and DA — that comparison is the go/no-go, not the speed choice alone.

What if my aircraft can't meet a published gradient IFR?+

Then that departure isn't available to you as published: wait for better climb conditions (cooler, lighter), use a different runway/procedure, or — where offered — the 'diverse vector area' or a visual-climb-over-airport (VCOA) option designed for exactly this. Taking off anyway and 'climbing in the hold' improvises terrain separation that the procedure was built to guarantee.

Does the 200 ft/nm standard apply to VFR flight too?+

Legally no — VFR terrain avoidance is see-and-avoid. Practically, the same physics kills: a high-DA VFR departure toward rising terrain wants exactly this computation with the terrain's own gradient (our obstacle-departure tool computes it). Instrument paperwork aside, ft/nm-versus-terrain is universal aviation arithmetic.

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