6-4
P/N 13772-005
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
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
