34 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Range / Endurance: Full Power Climb with Ice
Accumulation
• Note •
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%.
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 1.4 78.1 152 18.3 4.3 654 8.3
4000 2.9 76.6 154 18.3 4.2 653 8.4
6000 4.5 75.0 155 18.3 4.1 650 8.5
8000 6.1 73.4 157 18.3 4.0 647 8.6
10000 7.8 71.7 158 18.3 3.9 643 8.6
12000 9.6 69.9 159 18.3 3.8 638 8.7
14000 11.5 68.1 160 18.3 3.7 632 8.7
16000 13.4 66.1 161 18.3 3.6 624 8.8
18000 15.5 64.1 161 18.3 3.5 615 8.8
20000 17.6 61.9 162 18.3 3.4 606 8.8
22000 20.0 59.5 162 18.3 3.2 595 8.8
24000 23.3 56.3 161 18.3 3.1 579 8.8
25000 25.4 54.1 161 18.3 3.0 569 8.8
Original Issue: 02-01-13
To Next Page
Loading...
Need help?
General
