Cirrus SR22 - Moment Limits

Cirrus Design Section 6
SR22 Weight and Balance Data
P/N 13772-004 6-11P/N 13772-004 6-11
Moment Limits
Use the following chart or table to determine if the weight and moment
from the completed Weight and Balance Loading Form (Figure 6-3)
are within limits.
Weight
LB
Moment/1000 Weight
LB
Moment/1000
Minimum Maximum Minimum Maximum
2200 304 326 2950 414 437
2250 311 333 3000 422 444
2300 318 341 3050 430 452
2350 326 348 3100 438 459
2400 333 355 3150 445 467
2450 340 363 3200 453 474
2500 347 370 3250 461 481
2550 354 378 3300 469 489
2600 362 385 3350 477 496
2650 369 392 *3400 484 504
2700 375 400 3450 494 511
2750 383 407 3500 501 519
2800 390 415 3550 508 526
2850 398 422 3600 515 533
2900 406 430
*NOTE: Maximum zero fuel weight.
Figure 6-5
SR22_FM06_3551
Moment/1000
Weight - Pounds
300 350 400 450 500 550
2000
2200
2400
2600
2800
3000
3200
3400
3600
Max Zero Fuel
Airplane
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