World’s most popular E6B Calculator, aka CR, CRP-5

FLIGHT PLANNING TOOLKIT

E6B Calculator

2.0

Plan your heading, check performance, and convert units in one place.

Course, Ground Speed & Wind Correction

Wind Correction Angle—° —
True Heading—°
Magnetic Heading—°
Ground Speed— kt
Head/Tailwind—
Crosswind— kt —
Wind triangle; numeric results are provided alongside.
Air vectorGround vectorWind vector

Wind Direction & Speed (Inverse)

Wind Direction FROM—°
Wind Speed— kt

Flight Time for Distance & GS

Flight Time—

Crosswind Calculator

Use the same reference for runway and wind directions: both true or both magnetic.

Crosswind— kt —
Head/Tailwind—

True Airspeed (from CAS)

Correct IAS for instrument and position error using your aircraft handbook to obtain CAS. Subsonic compressibility is included.

Pressure Altitude—
ISA Temp—
True Air Speed—

Calibrated Airspeed (from TAS)

Calibrated Airspeed—

Density Altitude

Dry-air ISA model. Pressure altitude uses the approximate 1,000 ft per inHg correction.

Pressure Altitude—
ISA Temp—
Density Altitude—

Time – Speed – Distance

Choose what to calculate, then enter the other two values.

Result—

Fuel Consumption

Trip consumption only; add taxi, contingency and required reserves separately.

Trip Fuel— US gal

Dewpoint

Dewpoint—
* Magnus approximation over water (−45 to +60 °C)

Relative Humidity

Relative Humidity—%
* Magnus approximation over water (−45 to +60 °C)

Reciprocal Heading

Reciprocal—

VOR Radial & Bearing

Radial ↔ Bearing: 180° apart.

Temperature

Distance

Speed / Mach (ISA sea level)

Mach conversion assumes 15 °C. Local Mach varies with temperature.

Pressure

Area

Weight & Mass

Volume / Fuel

*Presets use typical densities; adjust for temperature/batch as needed.

Avgas ≈ 0.72 kg/L (6 lb/US gal)

Time Breakdown

Hours + minutes + seconds = total seconds.