Cirrus SR22 Pilot Operating Handbook page 148

TPOH
POH Temporary Change
Range / Endurance Profile
Conditions:
• Weight ........................................................................................................ 3400 LB
• Temperature ...................................................................................... Standard Day
• Winds................................................................................................................ Zero
• Mixture.............................................................................................. Best Economy
• Total Fuel ................................................................................................ 81 Gallons
Fuel Remaining For Cruise is equal to 81.0 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
Range is decreased by 5% if nose wheel pant and fairings removed.
Range is decreased by 15% if nose and main wheel pants and fairings
removed.
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 Remaining
For Cruise
FT Gal
SL 0.0
2000 0.7
4000 1.3
6000 2.0
8000 2.7
2 of 3
• Note •
Fuel Airspeed
Gal KTAS
70.8 166
69.0 170
67.2 173
65.3 177
63.5 180
Fuel Endurance
Flow
GPH Hours
17.8 4.0
17.8 3.9
17.8 3.9
17.8 3.9
17.8 3.8
Cirrus Design
SR22
Mixture: Best Power
Range Specific
Range
NM Nm/Gal
661 9.3
670 9.6
680 9.8
689 10.0
700 10.3
TPOH 11-03
June 30, 2011