Cirrus Design
Section 5
SR22T
Performance Data
P/N 13772-005
5-25
P/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
Original Issue
