Aviation & Pilots
Weight and balance, crosswind and density altitude.
6 tools
- Aircraft Weight and Balance CalculatorEstimate aircraft weight and balance from pilot-entered data.
- Crosswind Component CalculatorEstimate crosswind component from pilot-entered data.
- Density Altitude CalculatorEstimate density altitude from pilot-entered data.
- Flight Fuel Burn CalculatorEstimate flight fuel burn from pilot-entered data.
- Cessna 172S Weight and Balance CalculatorCessna 172S historical N21767 historical example: empty weight 1718.2 lb at 41.07 in. Fuel arm 48 in; front 37, rear 73, baggage 95 in. Forward CG interpolates from 35 to 41 inches above 1950 lb; maximum 2550 lb. These records must not replace your aircraft's approved POH.
- Piper Cherokee PA-28-161 Weight and Balance CalculatorPiper Cherokee PA-28-161 historical N3044N historical example: empty weight 1464.69 lb at 85.95 in. Fuel arm 95 in; front 80.5, rear 118.1, baggage 142.8 in. Forward CG interpolates from 83 to 87 inches above 1950 lb; maximum 2325 lb. These records must not replace your aircraft's approved POH.