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Range is reduced by a maximum of 2% as a result of the Anti-Ice System
installation.
Residual ice on unprotected airplane surfaces can cause a loss in rate of
climb of approximately 50%.
Normally aspirated service ceiling is 10,000 feet density altitude with ice
accretion.
Fuel Remaining For Cruise is equal to 92.0 gallons usable, less climb fuel,
less 9.8 gallons for 45 minutes IFR reserve fuel at 47% power (ISA @ 10,000
ft PA), less descent fuel, less fuel used prior to takeoff.
Range and endurance shown includes descent to final destination at
approximately 178 KIAS and 500 fpm.
Aircraft with optional air-conditioning system - Range is decreased by 1%. For
maximum range the air-conditioner should be off.
Conditions:
• Weight ........................................................................................................3400 LB
• Temperature ...................................................................................... Standard Day
• Winds................................................................................................................Zero
• Mixture.............................................................................................. Best Economy
• Total Fuel ................................................................................................ 92 Gallons
75% 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 81.8 139 17.8 4.6 639 7.8
2000 0.7 81.1 141 17.8 4.6 645 7.9
4000 1.3 80.4 143 17.8 4.5 650 8.1
6000 2.0 79.7 144 17.8 4.5 655 8.2
8000 2.7 79.0 146 17.8 4.4 660 8.3
Revision 02: 11-17-09
P/N 13772-134 31 of 44
Cirrus Design Section 9
SR22 Supplements
Range / Endurance Profile (Continued)
65% 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 81.8 127 15.4 5.3 674 8.2
2000 0.7 81.1 128 15.4 5.3 677 8.3
4000 1.3 80.4 129 15.4 5.2 679 8.4
6000 2.0 79.7 130 15.4 5.2 681 8.5
8000 2.7 79.0 131 15.4 5.1 681 8.6
10000 3.5 78.2 131 15.4 5.1 681 8.7
12000 4.4 77.4 132 15.4 5.0 681 8.8
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 81.8 111 13.1 6.3 696 8.5
2000 0.7 81.1 111 13.1 6.2 693 8.6
4000 1.3 80.4 111 13.1 6.2 691 8.6
6000 2.0 79.7 111 13.1 6.1 687 8.6
8000 2.7 79.0 111 13.1 6.0 682 8.6
10000 3.5 78.3 110 13.1 6.0 677 8.7
12000 4.4 77.4 110 13.1 5.9 670 8.7
14000 5.3 76.5 109 13.1 5.8 663 8.7
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 81.8 111 11.3 7.2 803 9.8
2000 0.7 81.1 111 11.3 7.2 800 9.9
4000 1.3 80.4 111 11.3 7.1 796 9.9
6000 2.0 79.7 111 11.3 7.0 791 9.9
8000 2.7 79.0 111 11.3 7.0 786 9.9
10000 3.5 78.2 110 11.3 6.9 779 10.0
12000 4.4 77.4 110 11.3 6.8 770 10.0
14000 5.3 76.5 109 11.3 6.7 761 10.0
Revision 02: 11-17-09
32 of 44 P/N 13772-134
Section 9 Cirrus Design
Supplements SR22
Balked Landing Climb Gradient with Ice Accumulation
• 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.
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:
• Power.................................................................................................... Full Throttle
• Mixture............................................................................................ Set per Placard
• Flaps........................................................................................................ 50% (DN)
　
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