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• Flaps...........................................................................................................0% (UP)
• 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 96 650 589 533 481 549
2000 96 560 502 448 398 474
4000 95 474 418 367 319 402
6000 94 392 338 289 244 332
8000 93 313 216 214 171 265
10000 92 237 188 200
12000 91 164 118 139
14000 90 95 51 80
2500
SL 93 846 777 712 652 728
2000 93 741 674 612 554 640
4000 92 640 576 516 461 555
6000 91 543 482 425 473
8000 91 451 392 337 395
10000 90 363 306 320
12000 89 279 224 248
14000 88 198 147 180
Revision 01: 08-26-09
11934-S37 33 of 56
Cirrus Design Section 9
SR20 Supplements
Enroute Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• 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.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps .......................................................................................................... 0% (UP)
• 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 96 1007 949 890 830 905
2000 96 868 808 748 688 775
4000 95 756 693 630 567 671
6000 94 642 576 510 445 566
8000 93 527 458 389 321 462
10000 92 411 339 357
12000 91 294 218 252
14000 90 175 97 148
2500
SL 93 1231 1175 1117 1058 1132
2000 93 1109 1050 988 926 1016
4000 92 987 923 858 793 900
6000 91 863 796 727 785
8000 91 738 667 595 670
10000 90 612 537 555
12000 88 484 405 440
14000 88 355 273 325
Revision 01: 08-26-09
34 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Time, Fuel and Distance to Climb
Factors:
• Taxi Fuel - Add 1 gallon for start, taxi, and takeoff.
• Temperature - Add 10% to computed values for each 10º C above standard.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture....................................................................................................... Full Rich
• Fuel Density...........................................................................................6.0 LB/GAL
• Weight ........................................................................................................3050 LB
• Winds................................................................................................................Zero
• Climb Airspeed ...............................................................................................Noted
Press
Alt
FT
OAT
(ISA)
°C
Climb
Speed
KIAS
Rate Of
Climb
FPM
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
Fuel
U.S. Gal
Distance
NM
SL 15 96 880 0.0 0.0 0
1000 13 96 828 1.3 0.3 2
2000 11 96 775 2.4 0.6 4
3000 9 95 723 3.8 1.0 6
4000 7 95 671 5.2 1.3 8
5000 5 95 618 6.7 1.7 11
6000 3 94 566 8.4 2.0 14
7000 1 94 514 10.3 2.4 17
8000 -1 93 462 12.3 2.9 21
9000 -3 93 409 14.6 3.3 25
10000 -5 92 357 17.2 3.8 29
11000 -7 92 305 20.3 4.4 35
12000 -9 91 252 23.8 5.0 41
13000 -11 91 200 28.3 5.8 49
14000 -13 90 148 34.0 6.8 60
Revision 01: 08-26-09
11934-S37 35 of 56
Cirrus Design Section 9
SR20 Supplements
Balked Landing Climb Gradient
　
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