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13772-130 31 of 58
Cirrus Design Section 9
SR22 Supplements
Time, Fuel and Distance to Climb
Factors:
• Taxi Fuel - Add 1.5 gallon for start, taxi, and takeoff.
• Temperature - Add 10% to computed values for each 10º C above standard.
• Fuel flow must be set to the placarded limit for all takeoffs and climbs.
• Cruise climbs or short duration climbs are permissible at best power as long as
altitudes and temperatures remain within those specified in the table.
Conditions: Example:
• Power .............................. Full Throttle Outside Air Temp..........................ISA
• Mixture .........Per Schedule, Section 4 Weight .................................. 3400 LB
• Fuel Density .....................6.0 LB/GAL Airport Pressure Altitude ...... 1000 FT
• Weight ...................................3400 LB Pressure Altitude ................ 12000 FT
• Winds ..........................................Zero
• Climb Airspeed..........................Noted Time to Climb ................ 11.3 Minutes
Fuel to Climb ..................... 5.6 Gallon
Distance to Climb ................. 20.5 NM
Press
Alt
FT
OAT
(ISA)
°C
Climb
Speed
KIAS
Rate Of
Climb
FPM
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
Fuel
U.S. Gal
Distance
NM
SL 15 101 1398 0.0 0.0 0.0
1000 13 100 1339 0.7 0.3 1.0
2000 11 100 1279 1.5 0.7 2.5
3000 9 99 1220 2.5 1.0 4.0
4000 7 99 1160 3.0 1.3 5.5
5000 5 97 1101 4.0 1.7 7.0
6000 3 98 1041 5.0 2.0 8.5
7000 1 96 982 6.0 2.4 10.5
8000 -1 97 922 7.0 2.7 12.0
9000 -3 95 863 8.0 3.1 14.5
10000 -5 95 803 9.5 3.5 16.5
11000 -7 94 744 10.5 3.9 19.0
12000 -9 95 684 12.0 4.4 21.5
13000 -11 93 625 13.5 4.8 24.5
14000 -13 93 565 15.0 5.3 28.0
15000 -15 92 506 17.0 5.8 31.5
16000 -17 92 446 19.0 6.4 35.5
17000 -19 91 387 21.5 7.1 40.0
17500 -20 91 357 24.0 7.8 45.5
Revision 02: 08-26-09
32 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Range / Endurance Profile
• Note •
• Fuel Remaining For Cruise is equal to 92.0 gallons usable, less climb fuel, less 9.8
gallons for 45 minutes IFR reserve fuel at 47% power (ISA @ 10,000 ft PA), less
descent fuel, less fuel used prior to takeoff.
• Range and endurance shown includes descent to final destination at approximately
178 KIAS and 500 fpm
• Range is decreased by 5% if nose wheel pant and fairings removed.
• Range is decreased by 15% if nose and main wheel pants and fairings removed.
Conditions: Example:
• Weight .................................. 3400 LB Power Setting ............................. 55%
• Temperature .................Standard Day Takeoff Press Alt ..................2000 FT
• Winds.......................................... Zero Cruise Press Alt ....................6000 FT
• Mixture.........................Best Economy
• Total Fuel .......................... 92 Gallons Fuel to Climb..........................1.3 Gal.
Cruise Fuel Flow................ 13.1 GPH
Endurance................................ 6.1 Hr
Range ....................................968 NM
True Airspeed..................... 157 Knots
75% POWERMixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.3 166 17.8 4.6 763 9.3
2000 0.7 81.1 170 17.8 4.6 775 9.6
4000 1.3 80.4 173 17.8 4.5 786 9.8
6000 2.0 79.7 177 17.8 4.5 797 10.0
8000 2.7 79.0 180 17.8 4.4 811 10.3
Revision 02: 08-26-09
13772-130 33 of 58
Cirrus Design Section 9
SR22 Supplements
Range / Endurance Profile
65% POWERMixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
For Cruise
Gal
Airspeed
KTAS
Fuel
Flow
GPH
Endurance
Hours
Range
NM
Specific
Range
Nm/Gal
SL 0.0 81.3 158 15.4 5.3 838 10.3
2000 0.7 81.1 161 15.4 5.3 850 10.5
4000 1.3 80.4 165 15.4 5.2 862 10.7
6000 2.0 79.7 168 15.4 5.2 874 11.0
8000 2.7 79.0 171 15.4 5.1 887 11.2
10000 3.5 78.2 174 15.4 5.1 899 11.5
12000 4.4 77.1 178 15.4 5.0 912 11.8
55% POWERMixture = Best Power
Press
Alt
FT
Climb
Fuel
Gal
Fuel
Remaining
　
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