5-28 P/N 13772-003
Section 5 Cirrus Design
Performance Data SR22T
Range / Endurance: Cruise Climb
• Note •
Fuel Remaining for Cruise in this table is based on AFM Cruise Climb: Lean of
Peak Technique; if Full Power Climb: Rich of Peak Technique is performed,
use Range/Endurance: Full Power Climb tables.
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 ..................................................3400 LB for Climb, Avg 3200 LB for Cruise
• Winds................................................................................................................Zero
• Total Fuel ................................................................................................ 92 Gallons
Range / Endurance: 85% Power Cruise - Cruise 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 0.6 78.9 170 18.3 4.3 738 9.3
4000 1.3 78.3 174 18.3 4.3 752 9.5
6000 1.9 77.7 178 18.3 4.2 766 9.7
8000 2.5 77.0 181 18.3 4.2 779 9.9
10000 3.1 76.4 185 18.3 4.2 793 10.1
12000 3.8 75.8 188 18.3 4.1 806 10.3
14000 4.4 75.1 192 18.3 4.1 820 10.5
16000 5.1 74.5 196 18.3 4.1 834 10.7
18000 5.8 73.7 200 18.3 4.0 848 10.9
20000 6.6 73.0 204 18.3 4.0 863 11.1
22000 7.3 72.2 208 18.3 3.9 878 11.3
24000 8.2 71.4 212 18.3 3.9 893 11.6
25000 8.6 70.9 214 18.3 3.9 900 11.7
Revision 1
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