Beechcraft Baron G58 Pilot Operating Handbook page 261

Model G58
20°C LEAN
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.
July, 2014
CRUISE POWER SETTINGS
RECOMMENDED CRUISE POWER
25 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
@ 2500 RPM (5200 LBS.)
FUEL FLOW
/ENGINE
PPH GPH KIAS KTAS
25 87 14.5
25 91 15.2
25 94 15.7
24 91 15.2
22 84 14.0
21 78 13.0
19 72 12.0
18 67 11.2
16 62 10.3
25 84 14.0
25 87 14.5
25 91 15.2
24 88 14.7
22 81 13.5
21 75 12.5
19 70 11.7
18 65 10.8
16 60 10.0
25 81 13.5
25 84 14.0
25 87 14.5
24 84 14.0
22 78 13.0
21 72 12.0
19 67 11.2
18 62 10.3
16 58 9.7
Section 5
Performance
AIR-
SPEED
189 182
191 188
191 194
186 195
179 193
172 191
164 188
157 185
149 181
184 184
185 190
186 196
181 197
174 195
167 193
159 190
152 186
143 182
179 185
180 191
181 197
176 198
169 196
161 192
154 190
146 187
138 182
TH05C
120029AA.AI
5-37