Aircraft Selection
Choose your aircraft model
Load example showing significant KIAS vs KTAS difference at high altitude
Cessna 150
C150
Empty Weight
1100 lbs
Max Gross
1600 lbs
Vs Clean
42 KIAS
Vs0 Landing
38 KIAS
Weight & Configuration
Set aircraft weight and flap position
lbs
Atmospheric Conditions
Set altitude and temperature
ft
°C
Pressure Altitude
0 ft
Density Altitude
0 ft
Maneuvering Parameters
Set bank angle for accelerated stall
°
Important Safety Information
Stall speeds are calculated using aerodynamic formulas and aircraft performance data. Always refer to your aircraft's POH for official stall speeds. Bank angles above 45° significantly increase stall speed and should be avoided in normal operations.