True Airspeed Calculator

Calculate true airspeed (TAS) from indicated airspeed, altitude, and temperature for accurate flight planning.

Calculator

Flight Parameters

Speed shown on airspeed indicator
Altitude corrected to standard pressure (29.92 inHg)
Current outside air temperature

Results

True Airspeed (TAS)
Calibrated Airspeed (CAS)
IAS corrected for instrument errors
TAS - IAS Difference:
Speed Ratio:
Calculation: TAS = CAS × √(ρ₀/ρ)
Where ρ₀ is sea level density and ρ is density at altitude

About True Airspeed

What is True Airspeed?

True Airspeed (TAS) is the actual speed of an aircraft through the air mass. It differs from Indicated Airspeed (IAS) due to altitude and temperature effects on air density.

Why is TAS Important?

TAS is essential for navigation, fuel planning, and flight time calculations. GPS ground speed equals TAS when there's no wind component.

Key Factors

  • Higher altitude = Higher TAS (lower air density)
  • Higher temperature = Higher TAS (lower air density)
  • At sea level in standard conditions: TAS ≈ IAS

Aviation Standards

  • Standard temperature: 15°C at sea level
  • Standard lapse rate: -2°C per 1000 ft
  • Calibrated airspeed assumes minimal instrument error

Quick Reference

At 5,000 ft: TAS ≈ IAS + 8%
At 10,000 ft: TAS ≈ IAS + 17%
At FL350: TAS ≈ IAS + 94%

True Airspeed Regulatory Requirements

FAA Requirements (United States)

14 CFR 91.117 - Aircraft Speed

Establishes maximum operating speeds for aircraft operations in controlled airspace, based on indicated airspeed which must be converted to true airspeed for navigation purposes.

14 CFR 91.159 - VFR Cruising Altitude

Requires pilots to maintain appropriate VFR cruising altitudes, where true airspeed calculations are essential for flight planning and fuel consumption estimates.

AC 00-45H - Aviation Weather Services

Provides guidance on using atmospheric data for flight planning, emphasizing the importance of true airspeed in wind triangle calculations.

EASA Requirements (Europe)

SERA.6001 - VMC Visibility and Distance from Cloud Minima

Requires pilots to maintain specific flight conditions where true airspeed calculations affect compliance with visibility and cloud clearance requirements.

SERA.5005(f) - Pre-flight Action

Pilots must determine estimated times en route and fuel requirements, calculations that depend on accurate true airspeed computations.

Navigation Applications

Wind Triangle Solutions

  • Ground speed calculations for flight planning
  • Wind correction angle determinations
  • Fuel consumption estimates
  • Time en route calculations

Performance Planning

  • Optimal altitude selection
  • Range and endurance planning
  • Approach speed calculations
  • Emergency descent planning

Professional Best Practices

Calculation Accuracy

  • Use current altimeter setting
  • Account for temperature variations
  • Verify pressure altitude readings
  • Cross-check with GPS ground speed

Flight Planning

  • Calculate TAS for each flight segment
  • Factor in altitude changes
  • Consider temperature deviations
  • Update calculations en route

Safety Considerations

  • Maintain adequate fuel reserves
  • Monitor actual vs. planned speeds
  • Account for changing conditions
  • Use conservative estimates