Aviation & Data Analysis Nat
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Aviation Calculators
EO ACC Logic
Data Analysis & Plotting
Percentage Difference
TOFP Plotter
Wind Components
Runway Heading (°)
Wind Direction (°)
Wind Speed (kts)
Calculate
Enter values to calculate.
Airspeed Conversion
Pressure Altitude (ft)
OAT (°C)
CAS / IAS (kts)
Calculate
Enter values to calculate.
Pressure Altitude
Indicated Altitude / Field Elevation (ft)
QNH (hPa)
Calculate
Enter values to calculate.
Engine Out Acceleration Height Logic
ACCSEG(2) (ft)
ACCSEG(7) (ft)
Runway Slope (%)
TOD (m)
OAT (°C)
Runway Elevation (ft)
Standard EO ACC Height (ft)
Runway Condition
Dry
Wet
Enter values to calculate.
Illustration
Dataset 1
Add Point
Dataset 2
Add Point
Interpolation
New X Value
On Dataset
Dataset 1
Dataset 2
Method
Linear
Exponential
Interpolate
Result will be shown here.
Display Options
Show Dataset 1
Show Dataset 2
Regression Analysis
Include Regression
Analyze Dataset 1
Analyze Dataset 2
Linear Model
Exponential Model
Show Residual Plot
Show Residual Histogram
Residual Plot
Residual Histogram
Value 1 (Reference)
Value 2 (New Value)
Calculate
Percentage Change
Change from Value 1 to Value 2.
Symmetric Difference
Difference relative to the average.
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