Crosswind Component Calculator for Pilots
Calculate crosswind and headwind from wind direction, speed, and runway. Includes gust components, opposite runway, aircraft limit check, and clock method tip.
Direction wind is coming FROM (0–360°)
How to Use This Calculator
- 1
Select your wind speed unit
Choose kts (knots), mph, km/h, or m/s. All calculations adjust automatically. Most aviation weather reports (METAR/ATIS) use knots.
- 2
Enter wind direction and speed
Enter the wind direction in degrees true (0–360°) as reported on ATIS or METAR. Enter the steady wind speed. Wind direction is the direction the wind is blowing FROM — 270° means wind from the west.
- 3
Enter gust speed if applicable
If ATIS reports a gust (e.g. '15G22') enter the gust speed (22). The calculator shows both steady and gust crosswind components side by side.
- 4
Enter your runway
Enter the runway number (01–36) or the exact magnetic heading. Runway 27 = 270° heading. The calculator also shows the opposite runway automatically.
- 5
Enter aircraft crosswind limit (optional)
Enter your aircraft's demonstrated crosswind component from the POH/AFM. The calculator shows a green/yellow/red status — green = within limits, yellow = above 75% of limit, red = exceeds limit.
What Each Value Means
- Crosswind Component (kts / mph / km/h / m/s)
- The portion of wind acting perpendicular to the runway centerline. Calculated as wind speed × sin(angle between wind direction and runway heading). A crosswind from the right is positive; from the left is negative. This is the component that causes lateral drift and requires crab angle or wing-low correction.
- Headwind Component (kts / mph / km/h / m/s)
- The portion of wind acting parallel to the runway. Calculated as wind speed × cos(angle between wind direction and runway heading). Positive = headwind (into your face); negative = tailwind (behind you). A headwind increases effective airspeed and shortens ground roll; a tailwind does the opposite.
- Demonstrated Crosswind Component (kts)
- The maximum crosswind in which the aircraft manufacturer has demonstrated the aircraft can be safely controlled. Listed in the Pilot's Operating Handbook (POH) / Airplane Flight Manual (AFM). It is not a structural limit but an operational guideline. Many pilots treat it as a hard limit; regulations allow exceeding it with appropriate pilot experience and conditions.
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