E6b+flight+computer+exercises+verified [exclusive] -

Your engine burns 8.5 gallons per hour (GPH). You have a flight time of 2 hours and 15 minutes. Calculate total fuel required.

Atmospheric pressure and temperature change how your instruments read. You must calculate True Airspeed ( TAScap T cap A cap S ) and Density Altitude for accurate navigation. Exercise 3.1: True Airspeed (TAS) Pressure Altitude = , Outside Air Temperature (OAT) = +15∘Cpositive 15 raised to the composed with power C , Indicated Airspeed (IAS) = Find: True Airspeed Locate the Airspeed/Altitude window on the computer. Rotate the dial to align +15∘Cpositive 15 raised to the composed with power C with a pressure altitude of IAScap I cap A cap S ) on the inner scale. Read the outer scale directly above it to find . Exercise 3.2: Density Altitude Given: Pressure Altitude = +30∘Cpositive 30 raised to the composed with power C Find: Density Altitude In the Airspeed/Altitude window , align +30∘Cpositive 30 raised to the composed with power C Look at the Density Altitude window arrow. Read the value indicated by the arrow: . 4. Wind Vector Problems (The Wind Side) The wind side of the E6B calculates your True Heading ( THcap T cap H ) and Groundspeed ( GScap G cap S ) by accounting for wind drift. Exercise 4.1: Heading and Groundspeed Given: True Course (TC) = 090∘090 raised to the composed with power 180∘180 raised to the composed with power Find: True Heading (TH) and Groundspeed (GS) Rotate the azimuth dial to place the wind direction ( 180∘180 raised to the composed with power ) at the True Index .

Rotate the inner disc until the air temperature (+15°C) aligns with the pressure altitude (6,500 ft).

Used for determining wind correction angle, groundspeed, and true airspeed (TAS). Verified E6B Flight Computer Exercises e6b+flight+computer+exercises+verified

WCA = +8° (Right), TH = 098°, GS = 133 kts. Exercise 4: True Airspeed Calculation

Verification method: Plot wind vector (240/22) from grommet. Rotate to TC 270°. Slide TAS 110 under grommet; read WCA and GS at wind dot.

These verified exercises target five mission-critical calculations: Your engine burns 8

Set the inner circle '10' pointer to the GPH rate (85 on the outer scale).

You wouldn't train for a marathon with a broken watch. Similarly, you need a .

Find 85 (representing 8.5) on the outer scale and align it with the black . Convert 2 hours and 20 minutes into total minutes: Find 140 on the middle scale (represented by 14). Read the value directly above it on the outer scale: 19.8. The verified fuel burn is 19.8 gallons . The Wind Side: True Heading and Groundspeed Rotate the dial to align +15∘Cpositive 15 raised

Indicated Altitude is 9,000 ft, OAT is +10°C, Calibrated Airspeed (CAS) is 120 knots. Calculate TAS.

Burn rate 9.5 GPH. Flight time 2 hours 20 minutes. Fuel needed?