Balked Landing Climb Gradient - Cirrus SR20 Pilot Operating Handbook

Cirrus Design
SR20

Balked Landing Climb Gradient

Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps ...................................................................................................... 100% (DN)
• Airspeed .....................................................................................Best Rate of Climb
Balked Landing Climb Gradients shown are the gain in altitude for the
horizontal distance traversed expressed as Feet per Nautical Mile.
Blank shaded 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 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
3050
6000
8000
10000
SL
2000
4000
2500
6000
8000
10000
P/N 21399-004 P/N 21399-004
Revision A1
• Note •
CLIMB GRADIENT ~ Feet/Nautical Mile
Climb
Speed
KIAS -20
84 654
81 569
78 484
75 399
72 313
69 225
84 878
81 779
78 680
75 582
72 485
69 387
Temperature ~°C
0 20
588 527 470
504 444 388
420 361 306
335 277
250 193
164
796 720 650
698 624 556
601 528 461
504 433
408 338
311
Section 5
Performance Data
40 50 ISA
443 542
362 470
280 399
326
253
179
617 739
523 657
430 575
493
412
329
5-27 5-27