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4000 Grnd Roll 1147 1239 1335 1434 1537 1211
50 ft 1745 1876 2011 2151 1914 1836
5000 Grnd Roll 1263 1364 1469 1579 1693 1313
50 ft 1914 2057 2206 2359 2101 1985
6000 Grnd Roll 1392 1503 1619 1739 1865 1424
50 ft 2101 2258 2421 2589 2307 2147
7000 Grnd Roll 1534 1657 1785 1546
50 ft 2307 2479 2658 2324
8000 Grnd Roll 1692 1828 1969 1679
50 ft 2535 2725 2922 2516
9000 Grnd Roll 1868 2018 2174 1825
50 ft 2788 2997 3213 2727
10000 Grnd Roll 2064 2229 1984
50 ft 3068 3298 2956
Revision 01: 08-26-09
30 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
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 extreme caution.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
• 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 ISA
3050
SL 89 678 621 568 518 581
2000 88 587 532 481 433 504
4000 87 500 447 398 351 430
6000 86 416 365 318 274 358
8000 85 336 287 241 199 289
10000 84 259 212 224
2500
SL 88 957 880 808 741 826
2000 87 841 767 698 634 729
4000 86 730 659 593 531 636
6000 85 624 555 492 545
8000 84 522 456 396 459
10000 83 425 362 377
Revision 01: 08-26-09
11934-S37 31 of 56
Cirrus Design Section 9
SR20 Supplements
Takeoff Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude for unit time expended
expressed in Feet per Minute.
• 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 .................................................................................................................50%
• Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3050
SL 89 905 862 817 771 828
2000 88 807 761 712 663 734
4000 87 707 657 606 554 639
6000 86 607 553 499 444 545
8000 85 504 447 390 333 450
10000 84 401 341 356
2500
SL 88 1256 1201 1144 1086 1158
2000 87 1136 1077 1017 955 1044
4000 86 1014 952 888 824 929
6000 85 892 825 758 815
8000 84 768 698 627 701
10000 83 643 569 587
Revision 01: 08-26-09
32 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Enroute 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 extreme caution.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
　
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