CIRRUS DESIGN SR22 - Range; Endurance Profile

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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