Time, Fuel And Distance To Climb - Cirrus SR22 Pilot Operating Handbook

Aircraft serials 22-3915 & subsequent 3600 pound takeoff weight
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Section 5
Performance Data

Time, Fuel and Distance to Climb

Conditions:
• Power ................................................................................................... Full Throttle
• Mixture...............................................................................Per Schedule, Section 4
• Fuel Density...........................................................................................6.0 LB/GAL
• Weight ........................................................................................................ 3600 LB
• Winds................................................................................................................ Zero
• Climb Airspeed ...............................................................................................Noted
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.
Press
OAT
Alt
(ISA)
FT
°C
SL
15
1000
13
2000
11
3000
9
4000
7
5000
5
6000
3
7000
1
8000
-1
9000
-3
10000
-5
11000
-7
12000
-9
13000
-11
14000
-13
15000
-15
16000
-17
17000
-19
17500
-20
5-22
• Note •
Climb
Rate Of
Speed
Climb
KIAS
FPM
108
1251
107
1194
107
1136
106
1079
105
1021
104
964
104
906
103
849
102
791
102
734
101
676
100
619
99
561
98
504
98
446
97
389
96
331
95
274
95
245
TIME, FUEL, DISTANCE ~ From Sea Level
Time
Minutes
U.S. Gal
0.0
0.8
1.7
2.6
3.6
4.7
5.8
6.9
8.2
9.6
11.1
12.7
14.4
16.4
18.7
21.2
24.3
27.9
30.0
Cirrus Design
Fuel
Distance
NM
0.0
0.0
0.3
1.5
0.7
3.1
1.0
4.8
1.4
6.7
1.7
8.6
2.1
10.7
2.5
12.9
2.9
15.4
3.3
18.0
3.7
20.9
4.2
24.1
4.6
27.6
5.1
31.6
5.7
36.1
6.3
41.4
7.0
47.6
7.8
55.1
8.2
59.4
P/N 13772-004
Original Issue
SR22

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