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Liftoff Speed.......................... 69 KIAS
Obstacle Speed .................... 75 KIAS
Takeoff Ground Roll ..............1685 FT
Dist. over 50' Obstacle ..........2380 FT
March 2010
Information Manual 5-19
Cirrus Design Section 5
SR20 Performance Data
Takeoff Distance
WEIGHT = 3000 LB
Speed at Liftoff = 68 KIAS
Speed over 50 Ft. Obstacle = 75 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 1287 1390 1497 1608 1724 1446
50 ft 1848 1988 2132 2282 2437 2064
1000 Grnd Roll 1412 1526 1643 1766 1893 1564
50 ft 2022 2175 2333 2497 2666 2226
2000 Grnd Roll 1552 1676 1805 1940 2079 1692
50 ft 2214 2381 2555 2734 2920 2402
3000 Grnd Roll 1706 1842 1985 2132 2286 1831
50 ft 2426 2609 2799 2996 3200 2593
4000 Grnd Roll 1877 2027 2183 2346 2515 1983
50 ft 2660 2861 3069 3285 3509 2802
5000 Grnd Roll 2066 2231 2404 2583 2769 2149
50 ft 2919 3139 3368 3605 3850 3029
6000 Grnd Roll 2276 2458 2648 2845 3050 2329
50 ft 3205 3447 3698 3959 4228 3276
7000 Grnd Roll 2509 2710 2919 2528
50 ft 3522 3788 4064 3547
8000 Grnd Roll 2768 2990 3221 2744
50 ft 3872 4165 4469 3841
9000 Grnd Roll 3056 3301 3555 2980
50 ft 4261 4583 4917 4160
10000 Grnd Roll 3376 3646 3241
50 ft 4691 5046 4514
Figure 5-9
Sheet 1 of 2
March 2010
5-20 Information Manual
Section 5 Cirrus Design
Performance Data SR20
Figure 5-9
Takeoff Distance
WEIGHT = 2500 LB
Speed at Liftoff = 65 KIAS
Speed over 50 Ft Obstacle = 70 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 813 878 946 1016 1090 912
50 ft 1212 1303 1398 1496 1597 1350
1000 Grnd Roll 892 964 1038 1116 1196 986
50 ft 1326 1426 1529 1636 1747 1457
2000 Grnd Roll 980 1059 1141 1226 1314 1067
50 ft 1451 1561 1674 1791 1912 1572
3000 Grnd Roll 1078 1164 1254 1348 1445 1156
50 ft 1590 1709 1834 1962 2095 1697
4000 Grnd Roll 1185 1281 1380 1483 1590 1253
50 ft 1743 1874 2010 2151 2297 1835
5000 Grnd Roll 1305 1410 1519 1632 1750 1358
50 ft 1912 2056 2205 2360 2520 1985
6000 Grnd Roll 1438 1553 1673 1798 1928 1473
50 ft 2098 2256 2421 2590 2766 2140
7000 Grnd Roll 1585 1712 1845 1599
50 ft 2305 2479 2659 2324
8000 Grnd Roll 1749 1889 2035 1737
50 ft 2534 2725 2923 2517
9000 Grnd Roll 1931 2085 2247 1887
50 ft 2787 2997 3216 2727
10000 Grnd Roll 2133 2304 2050
50 ft 3068 3299 2986
Sheet 2 of 2
March 2010
Information Manual 5-21
Cirrus Design Section 5
SR20 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.
• 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 ................................. Full Rich Weight .................................. 3000 LB
• Flaps ...........................................50% Pressure Altitude .................. 1750 FT
• Airspeed............... Best Rate of Climb
Climb Airspeed .....................85 Knots
Gradient............................491 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
3000
SL 85 678 621 568 518 581
2000 85 587 532 481 433 504
4000 84 500 447 398 351 430
6000 83 416 365 318 274 358
8000 82 336 287 241 199 289
10000 82 259 212 224
2500
　
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