Beechcraft Baron G58 Pilot Operating Handbook page 262

Section 5
Performance
20°C RICH
OF PEAK EGT
PRESS.
ALT.
FEET
SL
2000
4000
6000
8000
10,000
12,000
14,000
16,000
SL
2000
4000
6000
8000
10,000
12,000
14,000
16,000
SL
2000
4000
6000
8000
10,000
12,000
14,000
16,000
NOTES: 1. Full throttle manifold pressure settings are approximate.
2. Shaded area represents operation with full throttle.
3. Fuel flows are to be used for flight planning only and will vary
from airplane to airplane. Lean using the EGT.
5-38
CRUISE POWER SETTINGS
RECOMMENDED CRUISE POWER
23 IN. HG (OR FULL THROTTLE)
MAN.
OAT
PRESS.
°C °F IN. HG
-5 23
-9 16
-13 9
-17 2
-21 -6
-25 -13
-29 -20
-33 -27
-37 -34
15 59
11 52
7 45
3 38
-1 30
-5 23
-9 16
-13 9
-17 2
35 95
31 88
27 81
23 74
19 66
15 59
11 52
7 45
3 38
@ 2300 RPM (5200 LBS.)
FUEL FLOW
/ENGINE
PPH GPH KIAS KTAS
23 81 13.5
23 84 14.0
23 87 14.5
23 91 15.2
22 89 14.8
21 84 14.0
19 78 13.0
18 73 12.2
17 68 11.3
23 78 13.0
23 79 13.5
23 85 14.2
23 88 14.7
22 87 14.5
21 81 13.5
19 76 12.7
18 71 11.8
17 66 11.0
23 76 12.7
23 79 13.2
23 82 13.7
23 85 14.2
22 84 14.0
21 78 13.0
19 73 12.2
18 68 11.3
17 64 10.7
Model G58
AIR-
SPEED
176 170
178 176
179 182
180 188
177 190
169 188
162 185
154 182
146 178
171 171
173 177
174 183
175 190
171 192
164 189
156 186
149 183
140 178
166 171
168 178
169 184
169 191
166 193
159 190
151 187
143 182
135 178
TH05C
120030AA.AI
July, 2014