AIRPLANE WEIGHING FORM
DATA
A = B = A - B =
CG = Total Moment ÷ Total Weight
WEIGHING EQUIPMENT
Scale Number: Cal Due Date:
SCALE READING
Position Weight (lb) Arm Moment
Left Main
Right Main
Nose
Total As Weighed:
Adjustments (+/-): Weight (lb) Arm Moment
Totals:
Empty Weight:
(Including Undrainable Fluids
and Full Oil)
Plus Drainable Unusable Fuel:
Basic Empty Weight:
Table 6-1 – Airplane Weighing Form