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1000 Grnd Roll 997 1034 1070 1067 1143 1045
Total 2018 2065 2113 2161 2210 2079
2000 Grnd Roll 1034 1072 1110 1148 1186 1076
Total 2066 2116 2166 2217 2268 2121
3000 Grnd Roll 1073 1112 1151 1191 1230 1108
Total 2117 2169 2222 2275 2329 2164
4000 Grnd Roll 1113 1154 1195 1236 1142
Total 2170 2225 2281 2337 2209
5000 Grnd Roll 1156 1198 1240 1283 1177
Total 2227 2285 2343 2402 2256
6000 Grnd Roll 1200 1244 1288 1332 1214
Total 2287 2348 2409 2471 2306
7000 Grnd Roll 1246 1292 1337 1251
Total 2351 2415 2479 2358
8000 Grnd Roll 1295 1342 1389 1291
Total 2418 2485 2553 2412
9000 Grnd Roll 1345 1394 1444 1331
Total 2490 2560 2631 2470
10000 Grnd Roll 1398 1449 1373
Total 2565 2639 2529
March 2010
Information Manual 6-1
Cirrus Design Section 6
SR20 Weight and Balance
Section 6
Weight and Balance
Table of Contents
Introduction .....................................................................................6-3
Airplane Weighing Form .................................................................6-6
Airplane Weighing Procedures .......................................................6-7
Weight & Balance Record .............................................................6-10
Loading Instructions......................................................................6-12
Center of Gravity Limits ................................................................6-14
Weight & Balance Loading Form ..................................................6-15
Loading Data.................................................................................6-16
Moment Limits...............................................................................6-17
Equipment List ..............................................................................6-18
March 2010
6-2 Information Manual
Section 6 Cirrus Design
Weight and Balance SR20
Intentionally Left Blank
March 2010
Information Manual 6-3
Cirrus Design Section 6
SR20 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.
March 2010
6-4 Information Manual
Section 6 Cirrus Design
Weight & Balance SR20
Figure 6-1
FS
350.2"
BUTTOCK LINE (BL)
200
150
100
50
BL 0.0
50
100
150
200
SR20_FM06_1031A
LBL 210.9"
RBL 87.7"
Typical LBL
MAC 48.4"
RBL 66.3"
LBL 66.3"
LBL 77.3"
BL 0.0"
RBL 77.3"
RBL 210.9"
LEMAC
FS 132.9"
STATION
FUSELAGE
(FS)
WL
165.5"
FS
157.5"
220
350
300
250
200
150
100
0.0
50
50
WL100
150
WATER LINE (WL)
FS
38.3"
Reference Datum located at
fuselage station 0.0".
NOTE
FS
55.6"
FS
222.0"
FS
100.0"
Airplane Dimensional Data
March 2010
Information Manual 6-5
Cirrus Design Section 6
SR20 Weight & Balance
SR20_FM06_1021A
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
March 2010
6-6 Information Manual
Section 6 Cirrus Design
Weight & Balance SR20
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 26.4 153.95 4064
Basic Empty Weight CG=
　
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