Cessna 206H, Руководство по эксплуатации самолета

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SOLOY TURBINE PAC SECTION 5
POHS CESSNA T206H/206H PERFORMANCE
5-23
F.A.A. Approved May 23, 2003
CRUISE PERFORMANCE
CONDITIONS:
1. 3600 Pounds
2. 1810 RPM
3. Inlet – Normal
PRESSURE ALTITUDE
– 12,000
STD -20

C
(-29

C)
STD
(-9

C)
STD +20

C
(11

C)
TOR
QU
E
P
S
I
K
TA
S
FU
E
L
FLOW LB
/H
R
TOR
QU
E
P
S
I
K
TA
S
FU
E
L
FLOW LB
/H
R
TOR
QU
E
P
S
I
K
TA
S
FU
E
L
FLOW LB
/H
R
72 165 189 66 164 179
60 153 156 60 157 160 58 158 160
50
141 134 50 145 138 50 147 141
40
126 115 40 128 118 40 130 121
30
90 96 30 92 99 30 94 101
PRESSURE ALTITUDE
– 14,000
STD –20  C
(-33  C)
STD
(-13  C)
STD +20  C
(7  C)
TOR
QU
E
P
SI
K
TA
S
FU
E
L
FLO
W
LB
/H
R
TOR
QU
E
P
SI
K
TA
S
FU
E
L
FLO
W
LB
/H
R
TOR
QU
E
P
SI
K
TA
S
FU
E
L
FLO
W
LB
/H
R
67
163 175
60
156 156 62 162 166 55 157 151
50
144 131 50 147 135 50 150 138
40
128 112 40 130 115 40 132 118
30
92 93 30 94 96 30 96 99
Figure 5-11. Cruise Performance (Sheet 4 of 6)
UNCONTROLLED
COPY