Cirrus Design Section 5
SR22 Performance Data
P/N 13772-004 5-19P/N 13772-004 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 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
3600
SL 108 769 730 691 653 635 701
2000 106 685 647 609 573 555
626
4000 104 603 567 531 496 479
554
6000 102 525 489 454 421 405
484
8000 101 448 414 381 349 333
415
10000 99 375 341 309 279 264
349
12000 98 303 271 241 211 197
285
14000 96 234 204 174 146 133
223
16000 94 168 138 110 84 71
163
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
Revision 1
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