Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-25P/N 13772-005 5-25
Range / Endurance: Full Power Climb
• Note •
Fuel Remaining for Cruise is equal to 92.0 gallons usable, less 1.5 gallons
(pre-takeoff fuel consumed), 11 gallons (45 minute IFR reserve at 65%
power), and listed volume for fuel consumed in Full Power Climb.
Range is decreased by 5% if nose wheel pant and fairings removed.
Range is decreased by 15% of nose wheel and main wheel pants and fairings
removed.
For aircraft with optional Air Conditioning System: range is decreased by 1% if
system in operation.
Aircraft with optional Enhanced Vision System: range is decreased by ½%.
Conditions:
•Mixture....................................................Best Economy - Target Fuel Flow or less
•Weight..................................................3600 LB for Climb, Avg 3400 LB for Cruise
•Winds...............................................................................................................Zero
•Total Fuel.................................................................................................92 Gallons
Range / Endurance: 85% Power Cruise - Full Power Climb
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
2000 1.0 78.5 170 18.3 4.3 734 9.3
4000 2.1 77.5 174 18.3 4.2 742 9.5
6000 3.2 76.4 177 18.3 4.2 749 9.7
8000 4.3 75.3 180 18.3 4.1 756 9.8
10000 5.4 74.2 184 18.3 4.0 763 10.0
12000 6.5 73.0 187 18.3 4.0 770 10.2
14000 7.7 71.9 191 18.3 3.9 777 10.4
16000 8.9 70.7 194 18.3 3.9 784 10.6
18000 10.1 69.4 198 18.3 3.8 791 10.8
20000 11.3 68.2 202 18.3 3.7 798 11.0
22000 12.6 66.9 206 18.3 3.7 805 11.3
24000 14.2 65.4 210 18.3 3.6 810 11.5
25000 15.1 64.4 213 18.3 3.5 812 11.6
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