5-22 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
Time, Fuel & Distance to Climb: Cruise Climb
• Note •
Tax i F uel - Add 1. 5 ga ll on for s t ar t , ta xi , an d ta ke o ff.
Tem pe ra tur e - Ad d 1 0% to c om pu ted va lu es fo r ea ch 1 0º C a bo ve s ta nd ar d.
Fuel flow must be leaned to target fuel flow or less, per AFM Cruise Climb:
Lean of Peak Technique procedure.
If temperatures do not promote lean of peak climb, use AFM Full Power
Climb: Rich of Peak Technique procedures and tables.
Conditions:
•Power......................................................................................................30.5” MAP
• Mixture................................................................................ Target Fuel flow or less
•Weight........................................................................................................3600 LB
•Winds................................................................................................................Zero
•Climb Airspeed.........................................................................................120 KIAS
Press
Alt
FT
OAT
(ISA)
°C
Climb
Speed
KIAS
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
Fuel
U.S. Gal
Distance
NM
S.L. 15 120 0.0 0.0 0.0
1000 13 120 1.1 0.3 2.2
2000 11 120 2.2 .07 4.4
3000 9 120 3.3 1.0 6.7
4000 7 120 4.4 1.3 9.1
5000 5 120 5.5 1.7 11.5
6000 3 120 6.7 2.0 14.0
7000 1 120 7.8 2.4 16.6
8000 -1 120 9.0 2.7 19.2
9000 -3 120 10.2 3.1 21.9
10000 -5 120 11.4 3.5 24.7
11000 -7 120 12.6 3.8 27.6
12000 -9 120 13.8 4.2 30.6
13000 -11 120 15.1 4.6 33.6
14000 -13 120 16.3 5.0 36.8
15000 -15 120 17.6 5.4 40.0
16000 -17 120 18.9 5.8 43.3
17000 -19 120 20.2 6.2 46.8
18000 -21 120 21.6 6.6 50.3
19000 -23 120 22.9 7.0 53.8
20000 -25 120 24.1 7.4 57.3
21000 -27 120 25.4 7.7 60.7
22000 -29 120 26.7 8.1 64.5
23000 -31 120 28.2 8.6 68.7
24000 -33 120 29.7 9.1 73.3
25000 -35 120 31.5 9.6 78.6
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