5-28
P/N 13772-005
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 ..................................................3600 LB for Climb, Avg 3400 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
0.7
78.9
170
18.3
4.3
739
9.3
4000
1.3
78.2
174
18.3
4.3
751
9.5
6000
2.0
77.5
177
18.3
4.2
763
9.7
8000
2.7
76.8
180
18.3
4.2
775
9.8
10000
3.5
76.1
184
18.3
4.2
788
10.0
12000
4.2
75.3
187
18.3
4.1
801
10.2
14000
5.0
74.6
191
18.3
4.1
813
10.4
16000
5.8
73.8
194
18.3
4.0
827
10.6
18000
6.6
73.0
198
18.3
4.0
840
10.8
20000
7.4
72.2
202
18.3
3.9
854
11.0
22000
8.1
71.4
206
18.3
3.9
869
11.3
24000
9.1
70.5
210
18.3
3.8
883
11.5
25000
9.6
69.9
213
18.3
3.8
890
11.6
Original Issue
