The back of the E6B is used for wind vector solutions to find your Wind Correction Angle (WCA) Groundspeed (GS)
Align the under 9.5 (read as 95) on the Outer Scale.
Wind drift changes your aircraft's path, requiring heading corrections to stay on course. Exercise 4: True Heading and Ground Speed : True Course (TC): 090° True Airspeed (TAS): 120 knots Wind: From 180° at 25 knots Manual Step : Set the wind direction (180°) under the True Index. Mark 25 knots up from the center grommet.
Set the wind direction () at the True Index index line. e6b+flight+computer+exercises+verified
Fuel problems use the same scales as time-speed-distance but replace speed with fuel burn rate (GPH). www.aeropartner.se
Fuel management is critical for flight safety. Always double-check your consumption rates. Exercise 2.1: Fuel Burned
Find the Density Altitude pointer within that same window window frame. Read the scale value pointed to by the arrow. : 6,800 Feet Quick Reference Answer Key Given Parameters Target Metric Verified Verification Value 1.1 35 NM, 14 Min Groundspeed 150 KTS 1.2 112 NM, 125 KTS Time En Route 54 Min 1.3 9.5 GPH, 140 Min Fuel Burned 22.2 GAL 2.1 TC 090°, TAS 120, Wind 180° @ 25KTS Heading / GS 102° TH / 117 KTS GS 3.1 Statue Miles 51.8 SM 3.2 5,000 PA, +20°C OAT Density Altitude 6,800 FT Share public link The back of the E6B is used for
: Your aircraft burns fuel at a rate of 9.5 gallons per hour (GPH). Your flight duration is 2 hours and 20 minutes (140 minutes). How much fuel will you consume? E6B Execution :
Observe the wind mark drift to determine the wind correction angle (WCA).
Look at the (the large black triangle labeled "60" on the inner scale). Mark 25 knots up from the center grommet
. Because the wind is pushing you from the right, you must steer into it. Subtract 12∘12 raised to the composed with power from your course (or read the left-hand scale). True Heading is 078∘078 raised to the composed with power ( ), and Groundspeed is 117 knots . Conversions and Altitudes Exercise 5: True Airspeed (TAS) and Density Altitude Problem: Pressure Altitude: 6,000 feet Outside Air Temperature (OAT): +15∘Cpositive 15 raised to the composed with power C Indicated Airspeed (IAS): 110 knots Find: Density Altitude and True Airspeed Verified Solution:
a list of "verified exercises," tasks designed to prove that the E6B was more than an antique. looked at the first problem: Calculate the Ground Speed and Wind Correction Angle. True Course: 090 raised to the composed with power True Airspeed (TAS): 180 raised to the composed with power
Master the E6B Flight Computer: Verified Exercises and Practice Guide
Align the "60" index (the rate arrow) on the inner scale with on the outer scale. on the inner scale. Read the value directly across on the outer scale. 50 Nautical Miles (NM) Exercise 2: Flight Time Your destination is away and your ground speed is . What is your Time En Route (ETE)? Verification: Align the rate arrow with on the outer scale. on the outer scale. Read the inner scale value. 1 hour and 38 minutes (98 minutes). Phase 2: Fuel Consumption
: Open the FUEL menu, select BURN , enter 12.5 for rate and 02:15 for duration. Verified Answer : 28.1 gallons. Wind Correction and Heading