Balked Landing Climb Gradient - Cirrus SR22 Pilot's Operating Handbook And Flight Manual

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Cirrus Design
SR22

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.
Weight
Press
Alt
LB
FT
SL
2000
4000
3600
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
P/N 13772-004
P/N 13772-004
Original Issue
• Note •
CLIMB GRADIENT ~ Feet/Nautical Mile
Climb
Speed
(V
REF)
KIAS
-20
79
860
79
732
79
611
79
497
79
391
79
291
79
1196
79
1033
79
880
79
737
79
603
79
478
Temperature ~°C
0
20
808
756
682
633
564
518
453
410
349
308
251
213
1129
1063
1000
970
908
821
763
681
627
551
500
429
381
Section 5
Performance Data
40
50
ISA
706
681
769
586
563
655
474
452
548
368
348
446
269
250
351
177
159
261
969
1080
849
820
936
707
680
800
575
550
673
451
428
553
336
314
441
5-27
5-27

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