Cirrus DESIGN SR22T Pilot Operating Handbook page 397

Cirrus Design
SR22 / SR22T
Range / Endurance Profile with Ice Accumulation
Conditions:
• Weight ........................................................................................................ 3400 LB
• Temperature ....................................................................................... Standard Day
• Winds ............................................................................................................... Zero
• Mixture ..............................................................................................Best Economy
• Total Fuel.................................................................................................92 Gallons
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.
75% POWER
Press Climb
Alt Fuel
FT Gal
SL 0.0
2000 0.7
4000 1.3
6000 2.0
8000 2.7
P/N 13772-134
Revision 04: 12-17-10
Fuel Airspeed
Remaining
For Cruise
Gal KTAS
81.8 139
81.1 141
80.4 143
79.7 144
79.0 146
• Note •
Fuel Endurance
Flow
GPH Hours
17.8 4.6
17.8 4.6
17.8 4.5
17.8 4.5
17.8 4.4
Section 9
Supplements
Mixture: Best Power
Range Specific
Range
NM Nm/Gal
639 7.8
645 7.9
650 8.1
655 8.2
660 8.3
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