5-10 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Weight and Balance Procedure
The following is a step-by-step guide to determine that an air-
craft with a given load is within and remains within the gross
weight and center of gravity limitations. Check that the pro-
posed aircraft is within CG limits at the operational zero fuel or
wing bending weight. This ensures that the aircraft remains
within limits as fuel is burned.
The following page numbers apply to Learjet 35A/36AAFM 102
and are only approximate for the 019 and 108 AFMs.
Action Where
Record manufacturer’s
empty weight and moment/
1,000 from aircraft weighing
record
AFM, Weight and Balance, page
1, or aircraft records
Enter payload weights and
moment
AFM Payload Moments Charts,
Weight and Balance, 25-33A
Enter fuel weights and
moments
AFM Fuel Moments Charts,
Weight and Balance, 14-17
Aircraft CG Takeoff Weight
and Moment
AFM CG Limits Chart, Weight and
Balance, 10-13
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