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12000 4.4 59.8 178 15.4 4.3 785 11.8
55% POWER Mixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 70.8 149 13.1 5.4 806 11.4
2000 0.7 69.0 152 13.1 5.4 815 11.6
4000 1.3 67.2 154 13.1 5.3 825 11.9
6000 2.0 65.3 157 13.1 5.3 835 12.2
8000 2.7 63.5 160 13.1 5.2 845 12.4
10000 3.5 61.6 163 13.1 5.1 856 12.7
12000 4.4 59.8 166 13.1 5.1 865 13.0
14000 5.3 57.8 169 13.1 5.0 875 13.4
Figure 5-17
Sheet 2 of 3
Revision A5
5-32 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Figure 5-17
Range / Endurance Profile
55% POWER Mixture = Best Economy
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 70.8 149 11.3 6.2 930 13.1
2000 0.7 69.0 152 11.3 6.2 941 13.4
4000 1.3 67.2 154 11.3 6.1 951 13.7
6000 2.0 65.3 157 11.3 6.1 962 14.0
8000 2.7 63.5 160 11.3 6.0 974 14.3
10000 3.5 61.6 163 11.3 5.9 985 14.6
12000 4.4 59.8 166 11.3 5.9 995 15.0
14000 5.3 57.8 169 11.3 5.8 1006 15.4
Sheet 3 of 3
Revision A5
P/N 13772-001 5-33
Cirrus Design Section 5
SR22 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.
• 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 ...................... Set per Placard Weight .................................. 3400 LB
• Flaps ................................ 100% (DN) Pressure Altitude .................. 4000 FT
• Climb Airspeed...........................VREF
Climb Airspeed .....................77 Knots
Rate of Climb....................633 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile Best
Rate
of
Climb
KIAS
Temperature ~ °C
-20 0 20 40 ISA
3400
SL 77 834 835 823 803 827 80
2000 77 750 744 728 704 736 80
4000 77 666 654 633 604 648 78
6000 77 581 564 537 504 560 78
8000 77 496 472 440 402 473 77
10000 77 409 379 341 296 387 77
2900
SL 77 1069 1070 1056 1032 1060
2000 77 969 962 942 914 953
4000 77 869 855 829 796 847
6000 77 789 747 716 677 743
8000 77 668 639 602 556 641
10000 77 565 529 484 432 639
Figure 5-18
Revision A5
5-34 P/N 13772-001
Section 5 Cirrus Design
Performance Data SR22
Figure 5-19
Balked Landing Rate of Climb
• 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.
• 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 the 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.......................Set per Placard Weight...................................3400 LB
• Flaps.................................100% (DN) Pressure Altitude...................4000 FT
• Climb Airspeed .......................... VREF
Climb Airspeed..................... 77 Knots
Rate of Climb ................... 878 FT/NM
Weight
LB
Press
Alt
FT
Climb
Speed
KIAS
RATE OF CLIMB - Feet per Minute Best
Rate
of
Climb
KIAS
Temperature ~ °C
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(50)
