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tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll
Wet Grass: Add 60% to Ground Roll
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 1082 1121 1161 1200 1240 1141
50 ft 2244 2298 2352 2408 2464 2325
1000 Grnd Roll 1122 1163 1204 1245 1286 1175
50 ft 2298 2355 2412 2470 2529 2372
2000 Grnd Roll 1163 1206 1248 1291 1334 1210
50 ft 2356 2415 2476 2537 2598 2422
3000 Grnd Roll 1207 1251 1295 1339 1384 1247
50 ft 2417 2479 2543 2607 2672 2473
4000 Grnd Roll 1252 1298 1344 1390 1436 1285
50 ft 2481 2547 2614 2681 2749 2528
5000 Grnd Roll 1300 1348 1395 1443 1490 1324
50 ft 2550 2619 2689 2759 2831 2585
6000 Grnd Roll 1350 1399 1449 1498 1547 1365
50 ft 2622 2694 2768 2842 2917 2644
7000 Grnd Roll 1402 1453 1504 1556 1607 1408
50 ft 2698 2775 2852 2930 3008 2707
8000 Grnd Roll 1456 1509 1563 1616 1669 1452
50 ft 2779 2860 2941 3022 3105 2773
9000 Grnd Roll 1513 1569 1624 1679 1735 1497
50 ft 2865 2949 3035 3121 3207 2841
10000 Grnd Roll 1573 1630 1688 1746 1803 1545
50 ft 2956 3045 3134 3225 3316 2914
June 2007
Information Manual 6-1
Cirrus Design Section 6
SR22 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
June 2007
6-2 Information Manual
Section 6 Cirrus Design
Weight and Balance SR22
Intentionally Left Blank
June 2007
Information Manual 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.
June 2007
6-4 Information Manual
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
June 2007
Information Manual 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
June 2007
6-6 Information Manual
Section 6 Cirrus Design
Weight & Balance SR22
Figure 6-3
Airplane Weighing Form
Weighing
Point
Scale
Reading - Tare = Net Weight X Arm = Moment
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(47)
