Cirrus DESIGN SR22 - Balked Landing Climb Gradient

Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-27P/N 13772-002 5-27
Balked Landing Climb Gradient
• Note •
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.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................ Set per Placard
• Flaps ...................................................................................................... 100% (DN)
• Climb Airspeed............................................................................................... V
REF
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile Best
Rate
of
Climb
KIAS
Temperature ~°C
-20 0 20 40 50 ISA
3400
SL 77 834 799 788 769 757 827 80
2000 77 750 744 728 704 690 736 80
4000 77 666 654 633 604 588 648 79
6000 77 581 564 537 504 486 560 78
8000 77 496 472 440 402 381 473 77
10000 77 409 379 341 296 272 387 77
2900
SL 77 1069 1070 1056 1032 1017 1060
2000 77 969 962 942 914 897 953
4000 77 869 855 829 796 776 847
6000 77 789 747 716 677 655 743
8000 77 668 639 602 556 532 641
10000 77 565 529 484 432 403 639
Reissue A