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50 ft 1710 1837 1970 2107 2248 1851
3000 Grnd Roll 1224 1322 1424 1530 1640 1312
50 ft 1883 2024 2169 2320 2476 2010
4000 Grnd Roll 1354 1463 1575 1693 1814 1430
50 ft 2076 2231 2392 2558 2730 2185
5000 Grnd Roll 1500 1620 1746 1875 2009 1560
50 ft 2291 2462 2640 2823 3013 2377
6000 Grnd Roll 1663 1796 1935 2078 2228 1704
50 ft 2532 2721 2917 3120 3330 2590
7000 Grnd Roll 1846 1994 2147 2307 2473 1862
50 ft 2801 3010 3227 3452 3684 2824
8000 Grnd Roll 2052 2216 2387 2564 2748 2038
50 ft 3103 3335 3575 3823 4080 3083
9000 Grnd Roll 2284 2466 2656 2853 3058 2233
50 ft 3442 3698 3965 4240 4526 3370
10000 Grnd Roll 2544 2748 2959 3179 3407 2449
50 ft 3822 4107 4403 4709 5026 3687
Figure 5-9
Sheet 1 of 2
June 2007
5-20 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-9
Takeoff Distance
WEIGHT = 2900 LB
Speed at Liftoff = 70 KIAS
Speed over 50 Ft Obstacle = 74 KIAS
Flaps - 50% · Takeoff Pwr · Dry Paved
Headwind: Subtract 10% for each 12
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll.
Wet Grass: Add 30% to Ground Roll.
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 605 654 704 757 811 679
50 ft 958 1029 1103 1180 1259 1066
1000 Grnd Roll 668 721 777 835 895 738
50 ft 1053 1131 1212 1297 1383 1155
2000 Grnd Roll 737 796 857 921 989 802
50 ft 1158 1244 1334 1426 1522 1253
3000 Grnd Roll 815 880 948 1018 1092 873
50 ft 1275 1370 1469 1570 1676 1361
4000 Grnd Roll 901 973 1048 1126 1207 952
50 ft 1408 1510 1619 1731 1847 1479
5000 Grnd Roll 998 1078 1161 1248 1337 1088
50 ft 1552 1667 1787 1911 2039 1610
6000 Grnd Roll 1107 1195 1287 1383 1483 1134
50 ft 1714 1842 1974 2111 2253 1753
7000 Grnd Roll 1229 1327 1429 1535 1646 1239
50 ft 1896 2037 2184 2335 2492 1912
8000 Grnd Roll 1366 1475 1588 1706 1829 1356
50 ft 2100 2257 2419 2587 2760 2087
9000 Grnd Roll 1520 1641 1767 1899 2035 1486
50 ft 2329 2503 2682 2868 3061 2281
10000 Grnd Roll 1683 1828 1969 2115 2267 1630
50 ft 2586 2779 2978 3185 3399 2495
Sheet 2 of 2
June 2007
Information Manual 5-21
Cirrus Design Section 5
SR22 Performance Data
Takeoff 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 extreme caution.
Conditions: Example:
• Power .............................. Full Throttle Outside Air Temp.......................20° C
• Mixture ...................... Set per Placard Weight .................................. 3400 LB
• Flaps ...........................................50% Pressure Altitude .................. 4000 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................89 Knots
Gradient............................654 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 91 939 896 853 811 864
2000 90 834 793 75.2 711 770
4000 89 734 694 654 615 680
6000 88 638 600 561 524 594
8000 87 546 509 472 436 510
10000 86 458 422 387 353 431
2900
SL 91 1172 1122 1070 1019 1083
2000 90 1049 1000 950 902 972
4000 89 931 884 836 790 867
6000 88 818 773 727 683 766
8000 87 711 667 623 581 669
10000 86 608 566 524 484 576
Figure 5-10
June 2007
5-22 Information Manual
Section 5 Cirrus Design
Performance Data SR22
Figure 5-11
Takeoff Rate of Climb
• Note •
• Rate-of-Climb values shown are change in altitude for unit time expended
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.
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(41)
