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Calcimator

Emergency Descent Calculator

Emergency descent time, distance, and time of useful consciousness for rapid decompression scenarios.

About this calculator

This calculator times an emergency descent — the kind flown after a rapid decompression, engine fire, or smoke in the cabin — and checks whether you can get down before hypoxia takes over. Descent time is simply the altitude to lose divided by your target vertical speed, and horizontal distance covered is derived from groundspeed times that same descent time, so a faster VSI shortens both the time aloft and the ground track consumed. True airspeed is estimated from indicated airspeed using the standard approximation that TAS runs about 2% higher than IAS per 1,000 feet, evaluated at the average of your start and target altitudes, then reduced by any headwind to get groundspeed.

The calculator also reports time of useful consciousness (TUC) — the rough window of useful cognitive function without supplemental oxygen — using widely-cited altitude bands (roughly 15–20 seconds above FL400, down to 30+ minutes below 15,000 ft), and flags whether your planned descent completes before that window closes. If a bank angle is entered it also computes turn radius for a turning descent, though the vertical-speed target itself is assumed constant through the turn rather than degrading with bank. Oxygen duration comes from a rough D-cylinder approximation (about 0.07 liters of gas per PSI) divided by your selected flow rate — treat both the TUC bands and this oxygen figure as planning approximations, not certified duration data, since actual TUC varies with individual physiology and activity level, and cylinder capacity varies by hardware.

Inputs

ft
ft
psi

Results

Descent time (min)

3.8

Time of useful consciousness (sec)

210

Descent time (sec)225
Horizontal distance (NM)15.2
Groundspeed (kts)243
True airspeed (kts)243
Turn radius (NM)0
O2 remaining (min)63
Completes before TUC (1=Yes)0
How to Use This Calculator
  1. Enter your current altitude (ft) and target altitude (ft) for the emergency descent.
  2. Set the planned descent rate (fpm) and indicated airspeed (kts) during the descent.
  3. Enter headwind component (kts) and bank angle if turning during descent.
  4. Review time to descend (minutes and seconds), horizontal distance covered (NM), and groundspeed.
  5. Compare time of useful consciousness (TUC) to descent time for rapid decompression emergencies.

How the result changes with Current altitude (ft)

Current altitude (ft)Descent time (min)Time of useful consciousness (sec)
12,5000.699,999
18,7502.21,800
37,5006.945
60,00012.518

What each input means

Current altitude (ft)
Altitude when emergency descent begins.
Target altitude (ft)
Safe altitude to descend to (typically 10,000 ft or MEA).
Descent rate (fpm)
Target vertical speed for the emergency descent.
Indicated airspeed (kts)
Airspeed during the descent (below Vne/Vmo).
Headwind (kts, neg=tail)
Headwind component. Negative = tailwind.
Bank angle (degrees)
Bank angle if executing a turning descent.
O2 pressure (PSI)
Remaining supplemental oxygen cylinder pressure.
O2 flow rate (L/min)
Oxygen flow rate in liters per minute.

What each result means

Descent time (min)
Time required to reach the target altitude.
Descent time (sec)
Descent time in seconds for comparison with TUC.
Time of useful consciousness (sec)
Approximate TUC at the starting altitude without supplemental O2.
Horizontal distance (NM)
Ground distance covered during the descent.
Groundspeed (kts)
Estimated groundspeed during descent.
True airspeed (kts)
TAS corrected for altitude.
Turn radius (NM)
Turn radius if banked (0 = wings level).
O2 remaining (min)
Supplemental oxygen duration at current flow rate.
Completes before TUC (1=Yes)
1 if descent completes within time of useful consciousness.

How this is calculated

Worked example, using the default values

  1. Identify Input Parameters
    4 parameters
    Current altitude (ft) = 25000, Target altitude (ft) = 10000, Descent rate (fpm) = 4000, Indicated airspeed (kts) = 180 = 8 input(s) provided
  2. Calculate Descent time
    Descent time = altitudeLoss / descentRateFpm
    3.8 = 3.8
  3. Calculate Time of useful consciousness
    Time of useful consciousness = Infinity
    210 = 210
  4. Calculate Descent time
    Descent time = descentTimeMin * 60
    225 = 225
  5. Calculate Horizontal distance
    Horizontal distance = (groundspeedKts / 60) * descentTimeMin
    15.2 = 15.2

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 does the calculator use average altitude instead of current altitude for the TAS conversion?

True airspeed's increase over indicated airspeed depends on air density, which changes continuously as you descend from your current altitude toward the target. Using the midpoint of the two altitudes for the 2%-per-1,000-ft TAS correction gives a single representative airspeed for the whole descent rather than the (too-high) starting-altitude value, though groundspeed and distance are still an approximation of a continuously changing quantity.

Does entering a bank angle change how fast I descend?

No. The calculator assumes you hold your entered descent rate constant regardless of bank angle — bank angle is only used to compute turn radius during the maneuver. In reality, banking reduces the vertical component of lift, so holding the same vertical speed while turning typically takes added power or a steeper pitch than a wings-level descent.

What happens if descent time exceeds time of useful consciousness?

The "Completes before TUC" output switches to 0, flagging that your descent rate and starting altitude combination would leave you without reliable cognitive function before reaching breathable air, absent supplemental oxygen. In that case the practical response is a steeper descent rate (within structural and airspeed limits) and getting oxygen on immediately.

How is oxygen duration estimated, and why might it be off for my equipment?

The calculator converts remaining cylinder pressure to liters using a rough 0.07-liters-per-PSI factor typical of a D-cylinder, then divides by your selected flow rate. Actual cylinder volume varies by size and manufacturer, so treat this as a ballpark figure and cross-check against your aircraft's actual oxygen duration chart or placard.

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