Cirrus DESIGN SR22T - Airplane Weighing Form

6-4 P/N 13772-003
Section 6 Cirrus Design
Weight and Balance Data SR22T
Airplane Weighing Form
Weighing
Point
Scale
Reading
- Tare = Net Weight X Arm = Moment
L Main A=
R Main A=
Nose B=
Total
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 78.4, moment = 1176
Unusable Fuel 15.0 154.9 2324
Basic Empty Weight CG=
Figure 6-1
SR22_FM06_2540
x
WL 100.0
y
A
B
FS 100.0 FS 142.5
A = x + 100
B = A - y
y = ____________ Measured
x = ____________ Measured
REF DATUM
FS 0.0
Original Issue