Enroute Rate Of Climb - Cirrus DESIGN SR20 Information Manual

Section 5
Performance Data
Conditions:
• Power...............................Full Throttle
• Mixture..................................Full Rich
• Flaps..................................... 0% (UP)
• Airspeed ...............Best Rate of Climb
• Rate-of-Climb values shown are change in altitude in feet per unit time expressed in
Feet per Minute.
• 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.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
• The Maximum Operating Altitude of 17,500 feet MSL may be obtained if the
airplane's gross weight does not exceed 2900 lb and the ambient temperature is
-20° C or less.
Weight Press
Alt
LB FT
SL
2000
4000
6000
3000
8000
10000
12000
14000
SL
2000
4000
6000
2500
8000
10000
12000
14000
5-24

Enroute Rate of Climb

• Note •
Climb
Speed
KIAS -20
96 979
95 868
94 756
93 642
92 527
91 411
91 294
90 175
93 1231
92 1109
92 987
91 863
90 738
89 612
88 484
88 355
Figure 5-13
Example:
Outside Air Temp ...................... 10° C
Weight................................... 3000 LB
Pressure Altitude................... 6500 FT
Climb Airspeed..................... 93 Knots
Rate of Climb .......................513 FPM
RATE OF CLIMB ~ Feet per Minute
Temperature ~ °C
0 20
923 866
808 748
693 630
576 510
458 389
339
218
97
1175 1117
1050 988
923 858
796 727
667 595
537
405
273
P/N 13999-002 Info Manual
Cirrus Design
SR20
40 ISA
808 880
688 775
567 671
445 566
321 462
357
252
148
1058 1132
926 1016
793 900
785
670
555
440
325
September 2011