Load example showing significant KIAS vs KTAS difference at high altitude
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.