Cirrus SR22 Pilot Operating Handbook page 424

Aircraft serials 22-3915 & subsequent 3600 pound takeoff weight
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Section 9
Supplements
Range / Endurance: Full Power Climb with Ice
Accumulation
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
Fuel Remaining for Cruise in this table is based on climb per AFM Full Power
Climb (Rich of Peak Technique) procedure.
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%.
Range / Endurance: 75% Power Cruise - Full Power Climb
Press
Climb
Alt
Fuel
FT
Gal
0
0.0
2000
0.7
4000
1.5
6000
2.3
8000
3.1
32 of 50
Airspee
Fuel
Remaining
For Cruise
Gal
KTAS
81.8
139
79.9
141
78.0
143
76.1
144
74.1
146
Fuel
Endurance
d
Flow
GPH
17.8
17.8
17.8
17.8
17.8
Cirrus Design
Range
Hours
NM
4.6
639
4.5
644
4.5
650
4.5
655
4.4
659
P/N 13772-150
Original Issue: 02-01-13
SR22
Specific
Range
Nm/Gal
7.8
8.0
8.1
8.2
8.4

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