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Center of Gravity Limits ................................................................6-14
Weight & Balance Loading Form ..................................................6-15
Loading Data.................................................................................6-16
Moment Limits...............................................................................6-17
Equipment List ..............................................................................6-18
Revision A3
6-2 P/N 13772-001
Section 6 Cirrus Design
Weight and Balance SR22
Intentionally Left Blank
Revision A3
P/N 13772-001 6-3
Cirrus Design Section 6
SR22 Weight & Balance
Introduction
This section describes the procedure for establishing the basic empty
weight and moment of the airplane. Sample forms are provided for
reference. Procedures for calculating the weight and moment for
various operations are also provided. A comprehensive list of all
equipment available for this airplane is included at the back of this
section.
It should be noted that specific information regarding the weight, arm,
moment, and installed equipment for this airplane as delivered from
the factory can only be found in the plastic envelope carried in the
back of this handbook.
It is the responsibility of the pilot to ensure that the airplane is loaded
properly.
Reissue A
6-4 P/N 13772-001
Section 6 Cirrus Design
Weight & Balance SR22
Figure 6-1
230.0
WL
165.5
FS
350.2
FS
222.0
FS
157.5
FS
38.3
FS
FS 100.0
55.6
(FS)
STATION
FUSELAGE
NOTE
Reference datum located at
fuselage station 0.0.
MAC 47.7"
50.0
100.0
150.0
200.0
50.0
100.0
150.0
230.0
LEMAC
FS 133.1
RBL 87.7
Typical LBL
RBL 63.1
LBL 63.1
RBL 77.3
BL 0.0
LBL 77.3
RBL 229.5
LBL 229.5
200.0
50.0
150.0
WL 100.0
100.0
50.0
0.0
150.0
200.0
250.0
300.0
350.0
BUTTOCK LINE (BL)
BL 0.0
WATER LINE (WL)
SR22_FM06_1439
Airplane Dimensional Data
Reissue A
P/N 13772-001 6-5
Cirrus Design Section 6
SR22 Weight & Balance
SR22_FM06_1440A
Spirit Level
LONGITUDINAL LEVELING
LATERAL LEVELING
Spirit Level
Straight
Edge
Door Sill Door Sill
Spacer
Block
Straight Edge Straight Edge
Spacer
Block
Figure 6-2
Airplane Leveling
Revision A2
6-6 P/N 13772-001
Section 6 Cirrus Design
Weight & Balance SR22
Figure 6-3
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 18.0 154.9 2788
Basic Empty Weight CG=
SR22_FM06_1441
x
WL 100.0
y
A
B
FS 100.0 FS 145.0
A = x + 100
B = A - y
y = ____________ Measured
x = ____________ Measured
REF DATUM
FS 0.0
Airplane Weighing Form
Revision A2
P/N 13772-001 6-7
Cirrus Design Section 6
SR22 Weight & Balance
Airplane Weighing Procedures
A basic empty weight and center of gravity were established for this
airplane when the airplane was weighed just prior to initial delivery.
However, major modifications, loss of records, addition or relocation of
equipment, accomplishment of service bulletins, and weight gain over
time may require re-weighing to keep the basic empty weight and
center of gravity current. The frequency of weighing is determined by
the operator. All changes to the basic empty weight and center of
gravity are the responsibility of the operator. Refer to Section 8 for
specific servicing procedures.
1. Preparation:
a. Inflate tires to recommended operating pressures.
b. Service brake reservoir.
c. Drain fuel system.
d. Service engine oil.
e. Move crew seats to the most forward position.
f. Raise flaps to the fully retracted position.
g. Place all control surfaces in neutral position.
h. Verify equipment installation and location by comparison to
equipment list.
2. Leveling (Figure 6-2):
a. Level longitudinally with a spirit level placed on the pilot door
　
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