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• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ................................. Full Rich Weight .................................. 3400 LB
• Flaps .....................................0% (UP) Pressure Altitude .................. 4000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................98 Knots
Gradient............................639 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT - Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 101 911 867 823 781 834
2000 100 813 771 729 689 748
4000 98 720 679 639 600 665
6000 97 630 590 552 515 584
8000 96 544 505 468 433 507
10000 95 461 424 388 354 433
12000 94 381 346 312 279 361
14000 93 304 271 238 207 292
16000 92 231 199 168 139 226
2900
SL 101 1130 1078 1026 975 1039
2000 100 1015 965 915 867 937
4000 98 905 857 809 763 840
6000 97 800 753 708 664 746
8000 96 699 654 611 569 656
10000 95 603 560 518 478 570
12000 94 610 469 429 391 487
14000 93 422 382 344 308 407
16000 92 337 299 263 229 331
Figure 5-12
Revision A4
5-24 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Figure 5-13
Enroute Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• 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: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 10° C
• Mixture............................As Required Weight...................................3400 LB
• Flaps.....................................0% (UP) Pressure Altitude...................6000 FT
• Airspeed ...............Best Rate of Climb
Climb Airspeed..................... 97 Knots
Rate of Climb .....................1030 FPM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 101 1428 1414 1392 1366 1398
2000 100 1311 1292 1267 1238 1279
4000 98 1193 1170 1141 1108 1160
6000 97 1074 1046 1013 977 1041
8000 96 953 921 884 845 922
10000 95 830 794 754 712 803
12000 94 706 666 623 577 684
14000 93 581 537 490 441 565
16000 92 454 406 355 303 446
2900
SL 101 1761 1748 1726 1698 1732
2000 100 1629 1610 1584 1552 1596
4000 98 1494 1471 1441 1405 1461
6000 97 1359 1331 1296 1257 1326
8000 96 1222 1189 1151 1108 1191
10000 95 1084 1046 1004 958 1056
12000 94 945 902 855 806 921
14000 93 804 757 706 653 787
16000 92 662 610 556 499 653
Revision A4
P/N 13772-001 5-25
Cirrus Design Section 5
SR22 Performance Data
Enroute Rate of Climb Vs Density Altitude
Conditions:
• Power .................................................................................................... Full Throttle
• Mixture ......................................... Per Schedule - Section 4, Max Power Fuel Flow
• Flaps ...........................................................................................................0% (UP)
• Airspeed..................................................................................... Best Rate of Climb
1,000
2,000
3,000
4,000
5,000
6,000
7,000
8,000
9,000
10,000
11,000
12,000
13,000
14,000
15,000
16,000
17,000
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
3400 LB
2900 LB
Rate of Climb ~ Feet Per Minute
Figure 5-14
Revision A5 Density Altitude ~
Feet
5-26 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Figure 5-15
Time, Fuel and Distance to Climb
Factors:
• Taxi Fuel - Add 1.5 gallon for start, taxi, and takeoff.
• Temperature - Add 10% to computed values for each 10º C above standard.
• Fuel flow must be set to the placarded limit for all takeoffs and climbs.
　
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