P/N 11934-003
5-21
Cirrus Design
Section 5
SR20
Performance Data
Takeoff Climb Gradient
• Note •
• Climb Gradients shown are the gain in altitude for the horizontal distance traversed
expressed as Feet per Nautical Mile.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
• 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.
Conditions:
Example:
• Power .............................. Full Throttle
Outside Air Temp .......................20° C
• Mixture ................................. Full Rich
Weight .................................. 3000 LB
• Flaps ........................................... 50%
Pressure Altitude .................. 1750 FT
• Airspeed ............... Best Rate of Climb
Climb Airspeed .....................85 Knots
Gradient............................491 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20
0
20
40
ISA
3000
SL
85
678
621
568
518
581
2000
85
587
532
481
433
504
4000
84
500
447
398
351
430
6000
83
416
365
318
358
8000
82
336
287
241
289
10000
82
259
212
224
2500
SL
84
957
880
808
741
826
2000
84
841
767
698
634
729
4000
83
730
659
593
531
636
6000
82
624
555
492
545
8000
81
522
456
396
459
10000
80
425
362
377
Figure 5-10
Revision A4
Summary of Contents for SR20
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Page 22: ...2 2 P N 11934 003 Section 2 Cirrus Design Limitations SR20 Placards 2 21 Revision A6 ...
Page 308: ...9 2 P N 11934 003 Section 9 Cirrus Design Supplements SR20 Intentionally Left Blank Reissue A ...