P/N 13772-134 31 of 48
Cirrus Design Section 9
SR22 / SR22T Supplements
Range / Endurance Profile with Ice Accumulation
• Note •
Range is decreased by a approximately 10% with ice accretion on the aircraft.
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 04: 12-17-10
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