Cirrus DESIGN SR22 - Range; Endurance Profile

Cirrus Design Section 5
SR22 Performance Data
P/N 13772-002 5-25P/N 13772-002 5-25
Range / Endurance Profile
• Note •
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.
Aircraft with optional Enhanced Vision System: range is decreased by ½%.
Conditions:
• Weight........................................................................................................ 3400 LB
• Temperature .......................................................................................Standard Day
• Winds ............................................................................................................... Zero
• Mixture ..............................................................................................Best Economy
• Total Fuel.................................................................................................81 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 70.8 166 17.8 4.0 661 9.3
2000 0.7 69.0 170 17.8 3.9 670 9.6
4000 1.3 67.2 173 17.8 3.9 680 9.8
6000 2.0 65.3 177 17.8 3.9 689 10.0
8000 2.7 63.5 180 17.8 3.8 700 10.3
Reissue A