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• Climb Airspeed ...............................................................................................VREF
Weight
LB
Press
Alt
FT
Climb
Speed,
VREF
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile
Temperature ~°C
-20 -10 0 5 ISA
3400
SL 88 536 584 574 569
2000 88 449 441 433 428
4000 88 366 359 351 346
6000 88 288 281 273 268
8000 88 214 207 199 195 200
10000 88 145 138 130 126 134
2900
SL 88 682 658 634 622
2000 88 551 529 506 495
4000 88 428 407 386 375
6000 88 313 293 273 263
8000 88 205 186 167 158 169
10000 88 103 86 68 60 77
Revision 02: 11-17-09
P/N 13772-134 33 of 44
Cirrus Design Section 9
SR22 Supplements
Balked Landing Rate of Climb with Ice Accumulation
• Note •
Balked Landing Rate of Climb values shown are the full flaps change in altitude for unit
time expended expressed in Feet per Minute.
For operation in air colder than this table provides, use coldest data shown.
This chart is required data for certification. However it is recommended that the best rate
of climb speed with flaps down be used, or that the balked landing procedures of
Section 4 of this POH be used for significantly better climb performance on a go-around.
Conditions:
• Power ....................................................................................................Full Throttle
• Mixture ............................................................................................Set per Placard
• Flaps .................................................................................................................50%
• Climb Airspeed............................................................................................... VREF
Weight
LB
Press
Alt
FT
Climb
Speed,
VREF
KIAS
RATE OF CLIMB - Feet per Minute
Temperature ~°C
-20 -10 0 5 ISA
3400
SL 88 740 745 747 747
2000 88 644 646 645 645
4000 88 546 545 543 541
6000 88 446 443 438 435
8000 88 345 340 333 329 333
10000 88 242 235 226 220 230
2900
SL 88 941 926 909 900
2000 88 790 773 754 744
4000 88 638 618 597 586
6000 88 484 462 439 427
8000 88 329 305 279 266 282
10000 88 173 146 119 104 132
Revision 02: 11-17-09
34 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Landing Distance with Ice Accumulation
• Note •
The following factors are to be applied to the computed landing distance for the noted
condition:
• Normal landings will be completed with the flaps set to 50%.
• VREF with flaps at 50% is 88 KIAS. The VREF indication can be utilized to fly
approaches at precisely 1.3 VSO in any flap configuration.
• Sloped Runway - Increase table distances by 27% of the ground roll distance for each
1% of downslope. Decrease table distances by 9% of the ground roll distance for
each 1% of upslope.
• Note •
The above corrections for runway slope are required to be included herein for
certification. They should be used with caution since published runway slope data is
usually the net slope from one end of the runway to the other. Many runways will have
portions of their length at greater or lesser slopes than the published slope, lengthening
(or shortening) landing ground run values estimated from the published slope as
described above.
• For operation in outside air temperatures colder than this table provides, use coldest
data shown.
• For operation in outside air temperatures warmer than this table provides, use
extreme caution.
Conditions:
• Winds................................................................................................................Zero
• Runway.........................................................................................Dry, Level, Paved
Revision 02: 11-17-09
P/N 13772-134 35 of 44
Cirrus Design Section 9
SR22 Supplements
Landing Distance - Flaps 50%
WEIGHT: 3400 LB
Speed over 50 Ft Obstacle: 88 KIAS
Flaps: 50%
Power: Smooth power reduction from
obstacle to idle at touchdown.
Runway: Dry, Paved, Level
Headwind: Subtract 10% for each 13
knots headwind.
Tailwind: Add 10% for each 2 knots
tailwind up to 10 knots.
Runway Slope: Reference Notes
Dry Grass: Add 20% to Ground Roll
Wet Grass: Add 60% to Ground Roll
PRESS
ALT
FT
DISTANCE
FT
TEMPERATURE ~°C
-20 -10 0 5 ISA
SL Grnd Roll 1346 1399 1452 1479
　
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本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 2979(109)