Aviation & Aeronautics
Basic

True Airspeed (rule of thumb)

Quick estimate: true airspeed increases about 2% per 1000 ft of altitude above indicated airspeed.

Formula

TAS≈IAS+(IAS×0.02×alt1000)TAS \approx IAS + (IAS \times 0.02 \times \tfrac{alt}{1000})

Variables

TASTrue airspeed
IASIndicated airspeed
altAltitude (ft)

Example

IAS 100 kt at 5000 ft: TAS ≈ 100 + 100×0.02×5 = 110 kt

How it works

Indicated airspeed is what the cockpit instruments show, but at higher altitudes the air is thinner, so the airplane must move faster through the air to produce the same aerodynamic effects. This rule of thumb estimates that increase by adding about 2% of IAS for every 1,000 ft of altitude, giving a quick mental conversion from IAS to TAS. It is only an approximation, but it is useful because the density of air generally decreases with altitude in a way that makes true speed rise steadily above indicated speed.

When to use it

Use this for quick flight-planning estimates when you need a rough TAS from IAS and altitude without a flight computer or detailed performance tables. It is most helpful in basic navigation, cross-country planning, and sanity-checking airspeed at moderate altitudes.

Worked example, step by step

Given: IAS = 140 kt, altitude = 8,000 ft Step 1: Convert altitude to thousands of feet: 8,000 ÷ 1,000 = 8 Step 2: Find the correction: 140 × 0.02 × 8 = 22.4 kt Step 3: Add the correction to IAS: TAS ≈ 140 + 22.4 = 162.4 kt Final answer: TAS ≈ 162 kt (rounded)

Common mistakes to avoid

  • Using altitude in feet directly instead of dividing by 1,000 first
  • Treating the result as exact instead of an estimate
  • Using this rule at very high altitudes or in unusual temperature conditions without checking more accurate data

Did You Know?

True airspeed rises above indicated airspeed with altitude — roughly 2% per 1,000 feet as the air thins.

Share this formula

Reviewed & maintained by the FormulaWon editorial teamLast reviewed September 2026