Enroute Climb Gradient - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

Enroute Climb Gradient

Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• 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.
Fuel flow must be set to the placarded limit for all takeoffs and climbs.
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.
Weight Press
Altitude
LB FT
SL
2000
4000
6000
3400 8000
10000
12000
14000
16000
SL
2000
4000
6000
2900 8000
10000
12000
14000
16000
P/N 13772-001
Revision A10
• Note •
Climb CLIMB GRADIENT - Feet per Nautical Mile
Speed
-20
KIAS
101 911
100 813
99 720
98 630
97 544
96 461
95 381
94 304
93 231
101 1130
100 1015
99 905
98 800
97 699
96 603
95 610
94 422
93 337
Figure 5-12
Temperature ~°C
0 20
867 823
771 729
679 639
590 552
505 468
424 388
346 312
271 238
199 168
1078 1026
965 915
857 809
753 708
654 611
560 518
469 429
382 344
299 263
Section 5
Performance Data
40 ISA
781 834
689 748
600 665
515 584
433 507
354 433
279 361
207 292
139 226
975 1039
867 937
763 840
664 746
569 656
478 570
391 487
308 407
229 331
5-17