CIRRUS DESIGN SR20, Pilot Operating Handbook

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5-32 P/N 11934-003
Section 5 Cirrus Design
Performance Data SR20
Figure 5-19
Balked Landing Rate of Climb
• Note •
• Balked Landing Rate of Climb values shown are the full flaps change in altitude for
unit time expended expressed in Feet per Minute.
• Dashed cells in the table represent performance below the minimum balked landing
climb requirements.
• 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: Example:
• Power...............................Full Throttle Outside Air Temp ...................... 20° C
• Mixture..................................Full Rich Weight................................... 2500 LB
• Flaps................................. 100% (DN) Pressure Altitude................... 4000 FT
• Climb Airspeed ......................... Noted
Climb Airspeed..................... 73 Knots
Rate of Climb ................... 733 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB - Feet per Minute
Temperature ~ °C
-20 0 20 40 ISA
2900
SL 75 905 845 785 724 800
2000 74 789 726 662 598 691
4000 73 671 604 538 471 581
6000 72 552 482 412 - 471
8000 71 432 359 286 - 362
10000 70 310 234 - - 252
2500
SL 75 1142 1076 1009 942 1026
2000 74 1011 942 872 801 904
4000 73 880 807 733 660 781
6000 72 747 670 593 - 658
8000 71 613 533 453 - 537
10000 70 478 394 - - 414
Revision A5