CIRRUS DESIGN SR20, Pilot Operating Handbook, Page: 152 / 508

5-34 P/N 11934-003
Section 5 Cirrus Design
Performance Data SR20
Figure 5-20
Landing Distance
WEIGHT = 2900 LB
Speed over 50 Ft Obstacle = 75 KIAS
Flaps - 100% · Idle · Dry, Level Paved
Surface
Headwind: Subtract 10% per each
13 knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 40% to Ground Roll
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 ISA
SL Grnd Roll 962 997 1032 1067 1102 1014
50 ft 1972 2017 2063 2109 2156 2040
1000 Grnd Roll 997 1034 1070 1067 1143 1045
50 ft 2018 2065 2113 2161 2210 2079
2000 Grnd Roll 1034 1072 1110 1148 1186 1076
50 ft 2066 2116 2166 2217 2268 2121
3000 Grnd Roll 1073 1112 1151 1191 1230 1108
50 ft 2117 2169 2222 2275 2329 2164
4000 Grnd Roll 1113 1154 1195 1236 1142
50 ft 2170 2225 2281 2337 2209
5000 Grnd Roll 1156 1198 1240 1283 1177
50 ft 2227 2285 2343 2402 2256
6000 Grnd Roll 1200 1244 1288 1332 1214
50 ft 2287 2348 2409 2471 2306
7000 Grnd Roll 1246 1292 1337 1251
50 ft 2351 2415 2479 2358
8000 Grnd Roll 1295 1342 1389 1291
50 ft 2418 2485 2553 2412
9000 Grnd Roll 1345 1394 1444 1331
50 ft 2490 2560 2631 2470
10000 Grnd Roll 1398 1449 1373
50 ft 2565 2639 2529
Revision A5