PA-28-181 Takeoff Performance Calculator
Indicated Altitude (ft)
↺
0
8000
QNH (hPa)
↺
950
1050
Outside Air Temp (°C)
↺
-40
40
Aircraft Mass (kg)
↺
930
1160
Wind Type
Headwind
Tailwind
Wind Speed (knots)
↺
0
20
Safety Factor
↺
1
2
Ground Roll (0ft) Computations
1. Pressure Altitude
2. Density Altitude
3. Base Distance
4. Weight Correction Delta
5. Dist. After Weight Adj.
6. Wind Correction Delta
50ft Obstacle Computations
3. Base Distance
4. Weight Correction Delta
5. Dist. After Weight Adj.
6. Wind Correction Delta
Final Distances
Ground Roll
To Clear 50ft
Calculate