Weight & Balance
Luggage Area 1 is located immediately behind the pilot/co-pilot seats.
Luggage Area 2 is behind area 1 from where the fuselage starts to narrow to
the rear bulkhead.
You may find the conversion tools below useful. They work both ways.
Quick Calculator can be used to do quick sums e.g. input expression: 10*14+5 will give an answer of 145.
G-BJDW Weight & Balance
Complete the fields below to calculate the total aircraft weight and moment.
Two values are given: that with the fuel on board, and that with no fuel.
Good practice states that you should perform these calculations to ensure the aircraft remains within limits at the end of your flight as well as at the start.
Please note the definitive reference to use for Weight & Balance calculations is the aircraft manual and latest official aircraft weigh data. Anglian Flight Centres can not be held responsible for the accuracy of the information presented here, although this has been checked.
Data used for this page originates from aircraft weighing report dated 1st April 2005.
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G-BJDW Check the calculated results against the loading graph at the bottom of this page (shown after you click 'calculate') to ensure you are within the CofG envelope for your planned type of flight. Alternatively, use the printable W&B graph to plot manually. Text highlighted in red indicates a warning. |
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| Item | Value | Arm |
| Aircraft basic weight | ||
| Pilot weight | ||
| Co-pilot weight | ||
| Fuel on board | ||
| Rear Passenger 1 weight | ||
| Rear Passenger 2 weight | ||
| Luggage Area 1 weight | ||
| Luggage Area 2 weight | ||
| Calculated Results | Take-off Values | Zero Fuel Values |
| Total Weight | ||
| Total Arm | ||
| Total Moment | ||
For a printable graph to plot manually, click here