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Climb Airspeed..................... 73 Knots
Rate of Climb ................... 733 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB - Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
2900
SL 75 905 845 785 724 800
2000 74 789 726 662 598 691
4000 73 671 604 538 471 581
6000 72 552 482 412 - 471
8000 71 432 359 286 - 362
10000 70 310 234 - - 252
2500
SL 75 1142 1076 1009 942 1026
2000 74 1011 942 872 801 904
4000 73 880 807 733 660 781
6000 72 747 670 593 - 658
8000 71 613 533 453 - 537
10000 70 478 394 - - 414
March 2010
Information Manual 5-33
Cirrus Design Section 5
SR20 Performance Data
Landing Distance
Factors:
The following factors are to be applied to the computed landing
distance for the noted condition:
• Headwind - Subtract 10% from table distances for each 13
knots headwind
• Tailwind - Add 10% to table distances for each 2 knots tailwind
up to 10 knots.
• Grass Runway, Dry - Add 20% to ground roll distance.
• Grass Runway, Wet - Add 60% to ground roll distance.
• Sloped Runway - Increase table distances by 27% of the
ground roll distance for each 1% of downslope. Decrease table
distances by 9% of the ground roll distance for each 1% of
upslope.
• Caution •
The above corrections for runway slope are required to be
included herein. These corrections should be used with
caution since published runway slope data is usually the net
slope from one end of the runway to the other. Many runways
will have portions of their length at greater or lesser slopes
than the published slope, lengthening (or shortening) landing
ground roll estimated from the table.
• For operation in outside air temperatures colder than this table
provides, use coldest data shown.
• For operation in outside air temperatures warmer than this table
provides, use extreme caution.
Conditions: Example:
• Technique .............................. Normal Outside Air Temp........................10°C
• Winds ..........................................Zero Weight .................................. 2900 LB
• Runway .................................... Paved Pressure Altitude .................. 2000 FT
• Flaps. ........................................100% Headwind ................................... Zero
• Power .................. 3° Power Approach
to 50 FT obstacle, then reduce power Landing Ground Roll ............ 1072 FT
passing the estimated 50 foot point Dist. over 50' Obstacle.......... 2116 FT
and smoothly continue power
reduction to reach idle just prior to
touchdown.
March 2010
5-34 Information Manual
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 20% to Ground Roll
Wet Grass: Add 60% 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
Total 1972 2017 2063 2109 2156 2040
1000 Grnd Roll 997 1034 1070 1067 1143 1045
Total 2018 2065 2113 2161 2210 2079
2000 Grnd Roll 1034 1072 1110 1148 1186 1076
Total 2066 2116 2166 2217 2268 2121
3000 Grnd Roll 1073 1112 1151 1191 1230 1108
Total 2117 2169 2222 2275 2329 2164
4000 Grnd Roll 1113 1154 1195 1236 1142
Total 2170 2225 2281 2337 2209
5000 Grnd Roll 1156 1198 1240 1283 1177
Total 2227 2285 2343 2402 2256
6000 Grnd Roll 1200 1244 1288 1332 1214
Total 2287 2348 2409 2471 2306
7000 Grnd Roll 1246 1292 1337 1251
Total 2351 2415 2479 2358
8000 Grnd Roll 1295 1342 1389 1291
Total 2418 2485 2553 2412
9000 Grnd Roll 1345 1394 1444 1331
Total 2490 2560 2631 2470
10000 Grnd Roll 1398 1449 1373
Total 2565 2639 2529
March 2010
Information Manual 6-1
Cirrus Design Section 6
SR20 Weight and Balance
Section 6
Weight and Balance
Table of Contents
Introduction .....................................................................................6-3
Airplane Weighing Form .................................................................6-6
Airplane Weighing Procedures .......................................................6-7
Weight & Balance Record .............................................................6-10
　
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