Aircraft Weight & Balance Calculator
SI
Imp
Imperial
Inputs
View results
Empty weight
Basic empty weight from the aircraft records.
lb
Empty arm
Basic empty-weight arm.
in
Pilot/front-seat weight
lb
Pilot/front-seat arm
in
Passenger/rear-seat weight
lb
Passenger/rear-seat arm
in
Fuel weight
lb
Fuel arm
in
Baggage weight
lb
Baggage arm
in
Forward CG limit
in
Aft CG limit
in
Results
Default result
Edit inputs
Loaded weight
2,130
lb
Pass
Also computed
Loaded CG arm
Pass
43.88
in
Total moment
93,470
lb·in
Forward-limit margin
8.88
in
Aft-limit margin
3.12
in
Method notes
2 notes
Uses total moment = sum(weight * arm) and CG arm = total moment / total weight.
This is a station-arithmetic screen only. Use the current aircraft weight-and-balance records, approved envelope and loading instructions.
Powered by MachineCalcs ↗