Cirrus SR22 Pilot Operating Handbook page 427

Cirrus Design
SR22
Balked Landing Climb Gradient with Ice Accumulation
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................ Set per Placard
• Flaps ........................................................................................................ 50% (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.
Climb gradient less than 3.3% shown in heavier table borders
Weight Press
Alt
LB FT
SL
2000
4000
3600
6000
8000
10000
SL
2000
4000
2900
6000
8000
10000
P/N 13772-150
Original Issue: 02-01-13
• Note •
Climb
Speed,
V
REF
KIAS -20
88 479
88 397
88 320
88 247
88 178
88 113
88 682
88 551
88 428
88 313
88 205
88 103
CLIMB GRADIENT ~ Feet/Nautical Mile
Temperature ~°C
-10 0
472 464
391 383
313 306
240 233
171 164
107 99
658 634
529 506
407 386
293 273
186 167
86 68
Section 9
Supplements
5 ISA
460
378
301
229
160 165
96 103
622
495
375
263
158 169
60 77
35 of 50