Technical data

13773-001
8-20
Page 3
Figure 8-201
Airplane Weighing
30 Nov 2000
Weighing
Point
Scale
Reading
- Tare
= Net
Weight
X Arm = Moment
Left Main A =
Right Main A =
Nose Gear B =
Tot al
As Weighed
CG =
CG = Total Moment + Total Weight
Space below provided for additions or subtractions to as weighed condition.
Empty Weight CG =
Engine Oil (if oil drained)
15 lb at FS 79.3, Moment = 1176
Unusable Fuel 18.0 154.9 2788
Basic Empty Weight CG =
C.G. % MAC = 100 x(C.G. Inches - LEMAC)/MAC
= 100 x(C.G. Inches - 133.1)/47.7