SOLOY TURBINE PAC
SECTION 5
POHS CESSNA U/TU 206G
PERFORMANCE
5-14
F.A.A. Approved
October 4, 2005
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
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
1447
0.0
0.0
0.0
0.0
2,000
86
1424
1.4
5.4
0.8
2.0
4,000
84
1399
2.8
10.6
1.6
4.0
6,000
82
1326
4.3
15.7
2.3
6.1
8,000
81
1228
5.8
20.8
3.1
8.3
10,000
79
1089
7.6
26.2
3.9
10.6
12,000
78
959
9.5
31.8
4.7
13.2
14,000
76
826
11.6
38.0
5.7
16.2
16,000
74
708
14.4
44.7
6.7
19.6
18,000
72
603
17.4
52.0
7.8
23.5
20,000
71
476
21.1
60.4
9.0
28.2
3300
0
86
1644
0.0
0.0
0.0
0.0
2,000
85
1622
1.2
4.7
0.7
1.8
4,000
83
1596
2.5
9.3
1.4
3.5
6,000
81
1519
3.7
13.8
2.0
5.3
8,000
79
1416
5.1
18.2
2.7
7.1
10,000
78
1286
6.6
22.8
3.4
9.1
12,000
76
1130
8.3
27.7
4.1
11.3
14,000
74
989
10.2
32.8
4.9
13.8
16,000
72
867
12.3
38.4
5.7
16.5
18,000
71
759
14.8
44.3
6.6
19.6
20,000
69
626
17.7
50.8
7.6
23.1
3000
0
86
1876
0.0
0.0
0.0
0.0
2,000
84
1853
1.1
4.2
0.6
1.5
4,000
82
1827
2.2
8.1
1.2
3.0
6,000
80
1746
3.3
12.0
1.8
4.5
8,000
79
1635
4.5
15.9
2.4
6.1
10,000
77
1476
5.7
19.9
3.0
7.8
12,000
75
1329
7.2
24.0
3.6
9.7
14,000
73
1179
8.8
28.4
4.2
11.7
16,000
71
1050
10.6
33.0
4.9
13.9
18,000
70
936
12.6
37.8
5.6
16.4
20,000
68
798
14.9
43.0
6.4
19.2
Figure 5-10. Time, Fuel and Distance to Climb (Sheet 1 of 3)
UNCONTROLLED
COPY
