Cirrus SR22 Pilot Operating Handbook page 421

Plane
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Cirrus Design
SR22
Conditions:
• Power .............................. Full Throttle
• Mixture ...................... Set Per Placard
• Flaps .....................................0% (UP)
• Airspeed ............... Best Rate of Climb
• Climb Gradients shown are the gain in altitude for the horizontal distance traversed
expressed as Feet per Nautical Mile.
• 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.
Weight
Press
Alt
LB
FT
SL
2000
4000
6000
3400
8000
10000
12000
14000
16000
SL
2000
4000
6000
2900
8000
10000
12000
14000
16000
P/N 13772-129
Revision 02: 08-26-09
Enroute Climb Gradient
Climb
CLIMB GRADIENT - Feet per Nautical Mile
Speed
KIAS
-20
112
769
110
682
109
598
108
518
107
440
105
366
104
295
103
228
102
163
112
951
110
849
109
751
108
657
107
567
105
481
104
398
103
320
102
244
Example:
Outside Air Temp ........................20°C
Weight .................................. 3400 LB
Pressure Altitude .................. 4000 FT
Climb Airspeed ...................109 Knots
Gradient............................529 FT/NM
• Note •
Temperature ~°C
0
731
645
563
484
408
335
266
199
135
907
806
709
617
529
444
363
286
212
Supplements
20
40
694
657
610
574
529
495
451
419
376
346
305
276
237
209
171
145
109
84
862
819
763
722
669
629
578
540
491
455
408
374
329
296
253
222
181
152
Section 9
ISA
703
689
607
528
452
379
308
240
175
873
867
771
679
591
506
425
346
271
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