CIRRUS DESIGN SR20, Pilot Operating Handbook

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P/N 11934-003 5-31
Cirrus Design Section 5
SR20 Performance Data
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.
• 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 .................. 2000 FT
• Airspeed ............... Best Rate of Climb
Climb Airspeed .....................74 Knots
Rate of Climb....................679 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~ °C
-20 0 20 40 ISA
2900
SL 75 779 699 626 558 644
2000 74 664 585 515 449 547
4000 73 548 475 408 346 451
6000 72 440 369 305 - 359
8000 71 335 268 206 - 271
10000 70 235 170 - - 186
2500
SL 75 987 894 807 728 829
2000 74 851 762 679 603 716
4000 73 721 635 557 484 608
6000 72 596 514 439 - 502
8000 71 477 398 327 - 401
10000 70 362 287 - - 305
Figure 5-18
Revision A5