E6b Flight Computer Exercises Verified Patched -

A sliding grid used to determine wind correction angles (WCA), true heading (TH), and ground speed (GS) based on wind direction/velocity and true airspeed (TAS).

The wind side of the E6B requires plotting with a pencil to determine how wind affects your heading and groundspeed. Exercise 4: Determining True Heading and Groundspeed True Course (TC): 090∘090 raised to the composed with power True Airspeed (TAS): 120 Knots Wind Direction/Speed: From 180∘180 raised to the composed with power at 20 Knots Step-by-Step E6B Execution: Set the Wind Direction ( 180∘180 raised to the composed with power ) under the "True Index" at the top.

Your aircraft burns fuel at a rate of 9.5 gallons per hour (GPH). The flight time is 2 hours and 20 minutes (140 minutes). How much fuel will you consume? e6b flight computer exercises verified

Runway 18 is in use. The reported wind is from 240° at 20 knots. Determine the headwind component and the crosswind component.

This article provides a comprehensive set of by real-world CFIs (Certified Flight Instructors). Each problem includes the steps to solve it and the correct answer. Let’s sharpen your skills. A sliding grid used to determine wind correction

These problems involve calculating the , True Heading (TH) , and Groundspeed (GS) based on True Course (TC), True Airspeed (TAS), Wind Direction, and Wind Speed. Exercise 1: Standard Crosswind Data: TC 125°, Wind 219° at 27 kts, TAS 145 kts. Steps: Set True Index to 125∘125 raised to the composed with power (True Course). Place wind dot (27 kts) relative to center. Slide grid to put wind dot on kts TAS line. Verified Results: Wind Correction Angle (WCA): +10∘positive 10 raised to the composed with power True Heading (TH): 135∘135 raised to the composed with power Groundspeed (GS): Exercise 2: Tailwind Challenge Data: TC 355°, Wind 220° at 44 kts, TAS 114 kts. Steps: Set True Index to 355∘355 raised to the composed with power (True Course). Mark wind direction ( 220∘220 raised to the composed with power ) and velocity ( kts) on top of the grid. Adjust grid to align wind dot with 114 TAS. Verified Results: Wind Correction Angle (WCA): -16∘negative 16 raised to the composed with power True Heading (TH): 339∘339 raised to the composed with power Groundspeed (GS): Exercise 3: Slow Airspeed/High Wind Data: TC 345°, Wind 210° at 15 kts, TAS 98 kts. Verified Results: Wind Correction Angle (WCA): +7∘positive 7 raised to the composed with power True Heading (TH): 352∘352 raised to the composed with power Groundspeed (GS):

Calculate the WCA: TH (248°) - TC (240°) = +8° (a right correction, meaning the wind dot must be on the right side). Your aircraft burns fuel at a rate of 9

A circular slide rule used for multiplication, division, and time-speed-distance-fuel calculations.

Fuel problems utilize the exact same mathematical logic as time/distance problems. The represents 60 minutes, aligned with the fuel burn rate (gallons per hour) on the outer scale. Verified Exercise 4: Total Fuel Burned

Airport elevation: 2,000 ft OAT: +30°C Altimeter setting: 29.92 inHg