Cessna TU206G STATIONAIR, Руководство по эксплуатации для пилотов

Страница: 107 / 188

SOLOY TURBINE PAC SECTION 5
POHS CESSNA U/TU 206G PERFORMANCE
5-15
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 - St20°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 1354 0.0 0.0 0.0 0.0
2,000 86 1263 1.5 5.4 0.8 2.2
4,000 84 1162 3.2 10.9 1.6 4.6
6,000 82 1061 5.0 16.7 2.5 7.1
8,000 81 961 7.0 22.6 3.4 9.9
10,000 79 848 9.2 28.9 4.3 12.9
12,000 78 744 11.7 35.6 5.3 16.3
14,000 76 635 14.6 42.9 6.4 20.1
16,000 74 547 18.0 50.9 7.6 24.6
18,000 72 491 21.9 59.4 8.9 29.5
20,000 71 404 26.3 68.5 10.2 35.1
3300 0 86 1544 0.0 0.0 0.0 0.0
2,000 85 1448 1.3 4.7 0.7 1.9
4,000 83 1342 2.8 9.5 1.4 3.9
6,000 81 1235 4.3 14.5 2.2 6.1
8,000 79 1130 6.0 19.6 2.9 8.4
10,000 78 1012 7.9 24.9 3.7 10.9
12,000 76 905 10.0 30.4 4.5 13.7
14,000 74 791 12.3 36.4 5.4 16.8
16,000 72 699 15.0 42.7 6.4 20.2
18,000 71 641 18.0 49.3 7.3 23.9
20,000 69 551 21.4 56.2 8.4 28.0
3000 0 86 1768 0.0 0.0 0.0 0.0
2,000 84 1666 1.2 4.1 0.6 1.7
4,000 82 1552 2.4 8.3 1.2 3.4
6,000 80 1438 3.7 12.5 1.9 5.2
8,000 79 1326 5.2 16.9 2.5 7.2
10,000 77 1200 6.8 21.4 3.2 9.3
12,000 75 1087 8.5 26.1 3.9 11.5
14,000 73 969 10.5 30.9 4.6 14.0
16,000 71 873 12.7 36.1 5.4 16.8
18,000 70 814 15.0 41.3 6.2 19.7
20,000 68 719 17.6 46.7 7.0 22.8
Figure 5-10. Time, Fuel and Distance to Climb (Sheet 2 of 3)
UNCONTROLLED
COPY