CIRRUS DESIGN 2220, Pilot Operating Handbook

Page: 185 / 334

C
IRRUS
D
ESIGN
S
ECTION
5: P
ERFORMANCE
D
ATA
SR20 L
ANDING
D
ISTANCE
P/N 11934-005 5-39
Landing Distance Table - Flaps 50%
Weight: 3150 lb (1429 kg)
Speed over 50 ft Obstacle: 82 KIAS
Flaps: 50%
Power: Idle
Runway: Dry, Level, Paved
Headwind: Subtract 10% per each 13
knots headwind.
Tailwind: Add 10% per each 2 knots
tailwind up to 10 knots.
Runway Slope: Refer to list of 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 Gnd Roll 1029 1066 1104 1141 1179 1217 1085
Total 2704 2768 2833 2899 2966 3033 2800
1000 Gnd Roll 1067 1106 1145 1184 1223 1262 1117
Total 2768 2836 2904 2974 3044 3115 2856
2000 Gnd Roll 1106 1147 1187 1228 1268 1309 1151
Total 2837 2908 2980 3053 3127 3202 2915
3000 Gnd Roll 1148 1190 1232 1274 1316 1358 1186
Total 2909 2984 3060 3137 3216 3295 2977
4000 Gnd Roll 1191 1234 1278 1322 1365 1409 1222
Total 2987 3066 3146 3227 3309 3392 3042
5000 Gnd Roll 1236 1281 1327 1372 1417 1462 1259
Total 3069 3152 3236 3322 3408 3496 3111
6000 Gnd Roll 1283 1330 1377 1424 1471 1518 1298
Total 3156 3243 3332 3422 3513 3605 3183
7000 Gnd Roll 1333 1382 1431 1479 1528 1577 1338
Total 3248 3340 3434 3529 3624 3721 3258
8000 Gnd Roll 1385 1435 1486 1537 1587 1638 1380
Total 3346 3443 3542 3642 3742 3844 3338
9000 Gnd Roll 1439 1492 1544 1597 1650 1702 1424
Total 3450 3553 3656 3761 3867 3974 3421
10,000 Gnd Roll 1496 1550 1605 1660 1715 1769 1469
Total 3560 3668 3778 3888 4000 4112 3509
Reissue A