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Normally 9 lb at average moment of 1394.
– –
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-7
Weight and Balance Loading Form
Reissue A
6-16 P/N 13772-001
Section 6 Cirrus Design
Weight & Balance SR22
Figure 6-8
Loading Data
Use the following chart or table to determine the moment/1000 for fuel
and payload items to complete the Loading Form.
*130 lb Maximum **81 U.S. Gallons Usable
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Baggage
FS 208.0
Fuel
FS 154.9
Weight
LB
Fwd
Pass
FS 143.5
Aft
Pass
FS 180.0
Fuel
FS 154.9
20 2.87 3.60 4.16 3.10 260 37.31 46.80 40.27
40 5.74 7.20 8.32 6.20 280 40.18 50.40 43.37
60 8.61 10.80 12.48 9.29 300 43.05 54.00 46.47
80 11.48 14.40 16.64 12.39 320 45.92 57.60 49.57
100 14.35 18.00 20.80 15.49 340 48.79 61.20 52.67
120 17.22 21.60 24.96 18.59 360 51.66 64.80 55.76
140 20.09 25.20 (27.04)* 21.69 380 54.53 68.40 58.86
160 22.96 28.80 24.78 400 57.40 72.00 61.96
180 25.83 32.40 27.88 420 60.27 75.60 65.06
200 28.70 36.00 30.98 440 63.14 79.20 68.16
220 31.57 39.60 34.08 460 71.25
240 34.44 43.20 37.18 486** 75.28
0.00 20.0 40.0 60.0 80.0
SR22_FM06_1946
0
100
200
300
400
500
Moment/1000
Weight - Pounds
Loading Chart Fwd Pass
Fuel
Aft Pass
Baggage
100
Loading Data
Revision A1
P/N 13772-001 6-17
Cirrus Design Section 6
SR22 Weight & Balance
Moment Limits
Use the following chart or table to determine if the weight and moment
from the completed Weight and Balance Loading Form are within
limits.
• Caution •
Before landing, verify aircraft weight and moment do not fall in the
Landing Limitation Zone.
Weight
LB
Moment/1000 Weight
LB
Moment/1000
Minimum Maximum Minimum Maximum
2200 304 326 2850 398 422
2250 311 333 2900 406 430
2300 318 341 2950 414 437
2350 326 348 3000 421 444
2400 333 355 3050 429 452
2450 340 363 3100 437 459
2500 347 370 3150 444 467
2550 354 378 3200 452 474
2600 362 385 3250 460 481
2650 369 392 3300 467 489
2700 375 400 3350 475 496
2750 383 407 3400 483 504
2800 390 415
2000
2200
2400
2600
2800
3000
3200
3400
300 350 400 450 500 550
Moment/1000
Weight - Pounds
Landing Limitation
Figure 6-9
Moment Limits
Revision A8
6-18 P/N 13772-001
Section 6 Cirrus Design
Weight & Balance SR22
Equipment List
This list will be determined after the final equipment has been installed
in the aircraft.
Reissue A
P/N 13772-001 7-1
Cirrus Design Section 7
SR22 Airplane Description
Section 7
Airplane and Systems Description
Table of Contents
Introduction .....................................................................................7-5
Airframe ..........................................................................................7-6
Fuselage ......................................................................................7-6
Wings...........................................................................................7-6
Empennage .................................................................................7-7
Flight Controls .................................................................................7-8
Elevator System...........................................................................7-8
Aileron System...........................................................................7-10
Rudder System..........................................................................7-12
Trim Systems ................................................................................7-14
Pitch Trim Control System.........................................................7-14
Roll Trim Control System...........................................................7-14
Yaw Trim System.......................................................................7-15
Flight Deck Arrangement ..............................................................7-16
Instrument Panel........................................................................7-16
Center Console..........................................................................7-17
Flight Instruments .........................................................................7-21
Primary Flight Display................................................................7-21
　
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