Cirrus Design Section 5
SR20 Performance Data
P/N 21399-004 5-17P/N 21399-004 5-17
Takeoff Climb Gradient
• Note •
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
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 ............................................................................................ Set per Placard
• Flaps .................................................................................................................50%
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 50 ISA
3050
SL 89 678 621 568 518 494 581
2000 88 587 532 481 433 410
504
4000 87 500 447 398 351 330
430
6000 86 416 365 318 274 253 358
8000 85 336 287 241 199 179
289
10000 84 259 212
224
2500
SL 88 957 880 808 741 710 826
2000 87 841 767 698 634 604
729
4000 86 730 659 593 531 503
636
6000 85 624 555 492
545
8000 84 522 456 396
459
10000 83 425 362
377
Revision A1
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