Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-19P/N 13772-005 5-19
Enroute Climb Gradient
• Note •
Climb Gradient values shown are the gain in altitude for the horizontal
distance traversed expressed as Feet per Nautical Mile.
For operation in air colder than this table provides, use the coldest (left-most)
data shown.
For operation in air warmer than this table provides, use extreme caution.
Conditions:
•Power....................................................................................................Full Throttle
•Mixture............................................................Maintain Fuel Flow in GREEN ARC
•Flaps..........................................................................................................0% (UP)
•Airspeed....................................................................................................120 KIAS
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~°C
-40 -20 0 20 40 50 ISA
3600
S.L. 120 931 798 679 571 473 427
597
2000 120 866 740 627 524 430 386
569
4000 120 804 685 577 480 390 349
542
6000 120 746 632 530 438 353 313
516
8000 120 690 583 486 398 317 279
490
10000 120 638 536 444 360 284 248
466
12000 120 588 491 404 325 252 218
442
14000 120 541 449 367 292 222 190
419
16000 120 497 410 332 260 195 164
397
18000 120 455 373 299 231 169 139
376
20000 120 415 337 267 203 144 117
356
22000 120 390 245 119 9
306
24000 120 280 147 32
230
25000 120 229 102
194
2900
S.L. 120 1173 998 856 736 629 579
765
2000 120 1083 932 806 695 594 546
744
4000 120 1012 878 763 657 559 511
725
6000 120 953 831 722 619 521 472
706
8000 120 903 787 680 578 478 428
685
10000 120 856 743 636 531 428 377
662
12000 120 808 695 585 478 371 318
634
14000 120 757 642 528 416 305 250
601
16000 120 701 581 463 346 230 173
562
18000 120 637 512 388 266 146 86
517
20000 120 564 433 303 176 51
465
22000 120 482 344 209 77
405
24000 120 389 245 105
337
25000 120 339 192 49
300
Original Issue