Temperature - Standard; Time, Fuel And Distance To Climb, Maximum - Cessna U206G STATIONAIR Pilot Operating Handbook

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
TIME, FUEL AND DISTANCE TO CLIMB
CONDITIONS:
1. Flaps Up
2. 1810 RPM
3. Maximum Continuous Power, 78
PSI or 738°C
4. Inlet - Normal
5.

Temperature - Standard

WT PRESS
LBS ALT FT
3600 0
2,000
4,000
6,000
8,000
10,000
12,000
14,000
16,000
18,000
20,000
3300 0
2,000
4,000
6,000
8,000
10,000
12,000
14,000
16,000
18,000
20,000
3000 0
2,000
4,000
6,000
8,000
10,000
12,000
14,000
16,000
18,000
20,000
Figure 5-10. Time, Fuel and Distance to Climb (Sheet 1 of 3)
F.A.A. Approved
MAXIMUM RATE OF CLIMB
CLIMB RATE OF
SPEED CLIMB
KIAS FPM
87 1447
86 1424
84 1399
82 1326
81 1228
79 1089
78 959
76 826
74 708
72 603
71 476
86 1644
85 1622
83 1596
81 1519
79 1416
78 1286
76 1130
74 989
72 867
71 759
69 626
86 1876
84 1853
82 1827
80 1746
79 1635
77 1476
75 1329
73 1179
71 1050
70 936
68 798
5-14
PERFORMANCE
NOTES:
1. Add 20 lbs (3 gal.) of fuel for
engine start, taxi & takeoff.
2. Distances shown are based on
zero wind.
TIME FUEL USED
MIN
LB.
0.0 0.0
1.4 5.4
2.8 10.6
4.3 15.7
5.8 20.8
7.6 26.2
9.5 31.8
11.6 38.0
14.4 44.7
17.4 52.0
21.1 60.4
0.0 0.0
1.2 4.7
2.5 9.3
3.7 13.8
5.1 18.2
6.6 22.8
8.3 27.7
10.2 32.8
12.3 38.4
14.8 44.3
17.7 50.8
0.0 0.0
1.1 4.2
2.2 8.1
3.3 12.0
4.5 15.9
5.7 19.9
7.2 24.0
8.8 28.4
10.6 33.0
12.6 37.8
14.9 43.0
October 4, 2005
SECTION 5
DIST
NM
GAL.
0.0 0.0
0.8 2.0
1.6 4.0
2.3 6.1
3.1 8.3
3.9 10.6
4.7 13.2
5.7 16.2
6.7 19.6
7.8 23.5
9.0 28.2
0.0 0.0
0.7 1.8
1.4 3.5
2.0 5.3
2.7 7.1
3.4 9.1
4.1 11.3
4.9 13.8
5.7 16.5
6.6 19.6
7.6 23.1
0.0 0.0
0.6 1.5
1.2 3.0
1.8 4.5
2.4 6.1
3.0 7.8
3.6 9.7
4.2 11.7
4.9 13.9
5.6 16.4
6.4 19.2