Conversion Tools

Icing Conditions Structural & Induction Icing Determination
Structural Icing
NONE
Induction / Engine Icing
NONE
Visible Moisture -
Mach (approx) -
TAT / Leading Edge -
RAM Rise -
Enter cloud top altitude, aircraft altitude, SAT, and IAS to determine icing conditions.
SAT / TAT Static & Total Air Temperature
°C
Edit to compute TAT
°C
Edit to compute SAT
-
TAT − SAT
Formula: TATK = SATK × (1 + 0.2M²) - assumes recovery factor K=1
Alternate Minimums Statute Mile Fraction Calculator
SM
SM
Required Alternate Visibility
-

Enter values as fractions (e.g. 3/4, 1 1/4) or decimals.

ISA Temperature Deviation
ISA Standard
-
ISA Deviation
-

Enter actual temperature and pressure altitude to compute ISA deviation.

Temperature

Edit either field to update the other.

Fuel Weight
Pounds
-
Kilograms
-
Endurance Fuel / Burn Rate
Endurance
-
Decimal Hours
-

Enter total fuel and burn rate to compute endurance.

Altimeter Setting

ISA standard: 29.92 inHg = 1013.25 hPa

Pressure Altitude
Pressure Altitude
-
QNH Correction
-

Enter field elevation and current altimeter setting.

Density Altitude
Density Altitude
-
ISA Deviation
-

Enter pressure altitude and outside air temperature.

RVR / Visibility Runway Visual Range
FAA Equivalent
-
Calculated
-

Enter RVR in feet or meters to compute visibility in statute miles.

Distance
Speed
Mach Number
Static Air Temperature at cruise altitude
Speed of sound: -  |  Edit Mach or TAS to convert.
Altitude

1 ft = 0.3048 m  |  FL310 = 31,000 ft = 9,449 m

Weight

1 lb = 0.453592 kg