Cessna TU206G STATIONAIR, Руководство по эксплуатации для пилотов

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SOLOY TURBINE PAC SECTION 5
POHS CESSNA U/TU 206G PERFORMANCE
5-16
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 -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 10.8 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 1136 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