Cessna 206H - Temperature - Standard -20°C

SOLOY TURBINE PAC SECTION 5
POHS CESSNA T206H/206H PERFORMANCE
5-19
F.A.A. Approved May 23, 2003
TIME, FUEL AND DISTANCE TO CLIMB
MAXIMUM RATE OF CLIMB
CONDITIONS:
1. Flaps Up
2. 1810 RPM
3. Maximum Continuous Power, 78
PSI or 738°C
4. Inlet - Normal
5. Temperature - Standard -20°C
NOTES:
1. Add 20 lbs (3 gal.) of fuel for
engine start, taxi & takeoff.
2. Distances shown are based on
zero wind.
WT
LBS
PRESS
ALT FT
CLIMB
SPEED
KIAS
RATE OF
CLIMB
FPM
TIME
MIN
FUEL USED
DIST
NM
LB.
GAL.
3600
0
87
1477
0.0
0.0
0.0
0.0
2,000
86
1454
1.4
5.8
0.9
2.0
4,000
84
1430
2.8
11.3
1.7
4.0
6,000
82
1403
4.2
16.6
2.5
5.9
8,000
81
1373
5.6
21.8
3.2
7.9
10,000
79
1231
7.1
26.9
4.0
10.0
12,000
78
1107
8.8
32.3
4.8
12.3
14,000
76
965
10.4
38.0
5.7
14.9
16,000
74
831
13.0
44.2
6.6
17.8
18,000
72
704
15.6
51.0
7.6
21.1
20,000
71
569
18.8
58.6
8.7
25.0
3300
0
86
1675
0.0
0.0
0.0
0.0
2,000
85
1652
1.2
5.1
0.8
1.7
4,000
83
1628
2.4
10.0
1.5
3.4
6,000
81
1600
3.7
14.6
2.2
5.1
8,000
79
1570
4.9
19.1
2.8
6.9
10,000
78
1419
6.3
23.6
3.5
8.6
12,000
76
1286
7.7
28.2
4.2
10.6
14,000
74
1139
9.4
33.1
4.9
12.7
16,000
72
994
11.3
38.3
5.7
15.1
18,000
71
859
13.4
44.0
6.6
17.8
20,000
69
717
16.0
50.2
7.5
20.9
3000
0
86
1907
0.0
0.0
0.0
0.0
2,000
84
1885
1.1
4.5
0.7
1.5
4,000
82
1860
2.1
8.7
1.3
3.0
6,000
80
1832
3.2
12.8
1.9
4.4
8,000
79
1801
4.3
16.7
2.5
5.9
10,000
77
1638
5.5
20.6
3.1
7.4
12,000
75
1497
6.7
24.6
3.7
9.1
14,000
73
1336
8.2
28.8
4.3
10.9
16,000
71
1185
9.7
33.2
4.9
12.8
18,000
70
1042
11.5
37.9
5.6
15.0
20,000
68
892
13.6
42.9
6.4
17.5
Figure 5-10. Time, Fuel and Distance to Climb (Sheet 3 of 3)
UNCONTROLLED
COPY