Cirrus SR20 - Page 174

5-32 P/N 21399-004
Section 5 Cirrus Design
Performance Data SR20
Landing Distance Table - Flaps 0%
WEIGHT: 3050 LB
Speed over 50 Ft Obstacle: 87 KIAS
Flaps: 0%
Power: Idle
Runway: Dry, Level Paved Surface
Headwind: Subtract 10% per each 13
knots headwind.
Tailwind: Add 10% for each 2 knots tail-
wind up to 10 knots.
Runway Slope: Ref. Factors.
Dry Grass: Add 20% to Ground Roll
Wet Grass: Add 60% to Ground Roll
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~ °C
0 10 20 30 40 50 ISA
SL Grnd Roll
1185 1228 1272 1315 1358 1402
1250
Total 2971 3037 3105 3174 3243 3314 3071
1000 Grnd Roll 1229 1274 1319 1364 1409 1454
1287
Total 3038 3108 3179 3252 3325 3399
3130
2000 Grnd Roll 1274 1321 1368 1414 1461 1508
1326
Total 3109 3183 3258 3335 3412 3490 3191
3000 Grnd Roll 1322 1371 1419 1467 1516 1564
1366
Total 3185 3263 3342 3422 3504 3586
3256
4000 Grnd Roll 1372 1422 1472 1523 1573 1623 1408
Total 3265 3348 3431 3515 3601 3688
3323
5000 Grnd Roll 1424 1476 1528 1581 1633 1685
1451
Total 3351 3437 3525 3614 3704 3795 3395
6000 Grnd Roll 1479 1533 1587 1641 1695 1749
1495
Total 3441 3533 3625 3719 3814 3910
3470
7000 Grnd Roll 1536 1592 1648 1704 1760 1817
1542
Total 3537 3634 3731 3830 3930 4031
3548
8000 Grnd Roll 1595 1654 1712 1770 1829 1887
1590
Total 3640 3741 3844 3948 4053 4159
3631
9000 Grnd Roll 1658 1718 1779 1840 1900 1961
1641
Total 3748 3855 3963 4073 4183 4295
3718
10000 Grnd Roll 1723 1786 1849 1912 1975 2038
1693
Total 3863 3976 4090 4205 4322 4439
3809
Revision A1