E6b Flight Computer Exercises File
The wind side is used to determine wind correction angle (WCA) and groundspeed (GS) by calculating the effect of wind on your true airspeed (TAS) and true course (TC). Practice Scenarios
The runway length is listed as 6,000 feet, which is roughly 1.14 Statute Miles. Convert 115 Statute Miles into Nautical Miles. Exercise 3.3: Convert 15∘C15 raised to the composed with power C
Your Pressure Altitude is 9,500 feet, OAT is -5°C, and your Indicated Airspeed is 135 knots. Find your Density Altitude and TAS. Answer Key & Explanations
Align the on the outer scale (A) with the 60 Rate Arrow on the inner scale (B). Locate the Time Enroute on the inner scale (B). e6b flight computer exercises
This utilizes the wind side of the E6B to determine your True Heading (TH) and Groundspeed (GS) given your True Course (TC), True Airspeed (TAS), Wind Direction (WD), and Wind Velocity (WV). Step-by-Step Wind Calculation Set the on the true index at the top.
Use the small internal "windows" on the calculator side to solve for environmental factors. Aviation Supplies & Academics
Look at the pencil dot to see how many degrees left or right it sits from the centerline. This is your Wind Correction Angle (WCA). The wind side is used to determine wind
Despite the prevalence of GPS and electronic flight bags (EFBs), the mechanical remains an essential tool for student pilots and a required subject for FAA knowledge tests. It is the ultimate backup, working without batteries or satellite signals.
Are you training for a (e.g., Private, Instrument, Commercial)?
WCA: +10° (Right), TH: 100°, GS: 118 knots. The wind is a direct right crosswind. This forces you to crab 10° to the right to maintain your track, slightly reducing your groundspeed. Exercise 3
How to solve: Set the Speed Index to 9.5. Locate 36 on the outer scale. Read the inner hour scale. Answer: 3 hours and 47 minutes. Section 2: Conversions and Corrections
Given: 75 statute miles (SM). Find: Nautical miles (NM).
) is used to determine Wind Correction Angle (WCA) and Groundspeed (GS). 1. Heading and Groundspeed Scenario A: True Course (TC): 090 raised to the composed with power True Airspeed (TAS): 125 knots 180 raised to the composed with power at 20 knots
Convert 75 Statute Miles (SM) to Nautical Miles (NM) . Fuel: Convert 40 Liters to US Gallons . Speed: Convert 150 knots to Miles per Hour (MPH) .