Cirrus SR22 Pilot Operating Handbook page 454

Section 9
Supplements
Balked Landing Climb Gradient
Conditions:
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set per Placard
• Flaps...................................................................................................... 100% (DN)
• Climb Airspeed ...............................................................................................V REF
Balked Landing 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.
This chart is required data for certification. However, significantly better
performance can be achieved by climbing at Best Rate of Climb speeds
shown with flaps down or following the Go-Around / Balked Landing
procedure in Section 4.
Weight Press
Alt
LB FT
SL
2000
4000
3400
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
30 of 48
• Note •
CLIMB GRADIENT ~ Feet/Nautical Mile
Climb
Speed
KIAS -20
77 834
77 750
77 666
77 581
77 496
77 409
77 1069
77 969
77 869
77 789
77 668
77 565
Temperature ~°C
0 20
835 823
744 728
654 633
564 537
472 440
379 341
1070 1056
962 942
855 829
747 716
639 602
529 484
Cirrus Design
40 ISA
803 827
704 736
604 648
504 560
402 473
296 387
1032 1060
914 953
796 847
677 743
556 641
432 639
13772-130
Revision 03: 05-09-11
SR22
Best
Rate
of
Climb
KIAS
80
80
79
78
77
77