Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-19P/N 13772-002 5-19
Enroute Climb Gradient
• Note •
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
Fuel flow must be set to the placarded limit for all takeoffs and climbs.
Cruise climbs or short duration climbs are permissible at best power as long
as altitudes and temperatures remain within those specified in the table.
For operation in air colder than this table provides, use coldest data shown.
For operation in air warmer than this table provides, use extreme caution.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps .......................................................................................................... 0% (UP)
• Airspeed .....................................................................................Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 50 ISA
3400
SL 101 911 867 823 781 760 834
2000 100 813 771 729 689 669
748
4000 99 720 679 639 600 581
665
6000 98 630 590 552 515 497
584
8000 97 544 505 468 433 416
507
10000 96 461 424 388 354 338
433
12000 95 381 346 312 279 264
361
14000 94 304 271 238 207 193
292
16000 93 231 199 168 139 125
226
2900
SL 101 1130 1078 1026 975 951
1039
2000 100 1015 965 915 867 843
937
4000 99 905 857 809 763 741
840
6000 98 800 753 708 664 642
746
8000 97 699 654 611 569 548
656
10000 96 603 560 518 478 458
570
12000 95 610 469 429 391 372
487
14000 94 422 382 344 308 290
407
16000 93 337 299 263 229 212
331
Reissue A
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