Cessna TU206G STATIONAIR, Pilot Operating Handbook

Page: 110 / 188

SOLOY TURBINE PAC SECTION 5
POHS CESSNA U/TU 206G PERFORMANCE
5-18
F.A.A. Approved October 4, 2005
CRUISE PERFORMANCE
CONDITIONS:
1. 3600 Pounds
2. 1810 RPM
3. Inlet – Normal
PRESSURE ALTITUDE
– 4,000
STD -20

C
(-13

C)
STD
(7

C)
STD +20

C
(27

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
69 151 184 72 157 191 72 160 200
60 143 167 60 146 172 60 149 177
50 132 148 50 135 153 50 137 157
40 118 130 40 120 133 40 123 137
30 96 111 30 86 114 30 88 117
PRESSURE ALTITUDE
– 6,000
STD -20

C
(-17

C)
STD
(3

C)
STD +20

C
(23

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
71 156 186 74 161 196 68 160 191
60 145 163 60 149 168 60 152 172
50 134 144 50 137 148 50 140 152
40 120 125 40 122 129 40 125 132
30 85 107 30 87 110 30 89 113
Figure 5-11. Cruise Performance (Sheet 2 of 6)
UNCONTROLLED
COPY