Beechcraft Baron G58, Руководство по эксплуатации для пилотов

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Performance
Section 5
Model G58
5-39
TH05C
120031AA.AI
CRUISE POWER SETTINGS
RECOMMENDED CRUISE POWER
23 IN. HG (OR FULL THROTTLE)
@ 2300 RPM (5200 LBS.)
ISA
- 20° C (ISA
- 36° F)
ST
ANDARD DA
Y (ISA)
ISA
+ 20° C (ISA
+ 36° F)
20°C LEAN
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
164
170
176
182
184
182
179
176
171
165
171
177
184
185
183
180
176
171
166
172
178
184
186
182
180
175
169
171
172
173
174
171
164
156
149
140
166
167
168
169
166
158
151
143
135
161
162
163
164
160
153
145
137
128
67
70
73
76
75
69
64
60
56
64
67
70
73
72
67
62
58
54
62
65
68
70
69
64
60
56
52
23
23
23
23
22
21
19
18
17
23
23
23
23
22
21
19
18
17
23
23
23
23
22
21
19
18
17
23
16
9
2
-6
-13
-20
-27
-34
59
52
45
38
30
23
16
9
2
95
88
81
74
66
59
52
45
38
-5
-9
-13
-17
-21
-25
-29
-33
-37
15
11
7
3
-1
-5
-9
-13
-17
35
31
27
23
19
15
11
7
3
PRESS.
ALT.
MAN.
PRESS. OAT
FUEL FLOW
/ENGINE
AIR-
SPEED
OF PEAK EGT
FEET °C °F IN. HG PPH GPH KIAS KTAS
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.
11.2
11.7
12.2
12.7
12.5
11.5
10.7
10.0
9.3
10.7
11.2
11.7
12.2
12.0
11.2
10.3
9.7
9.0
10.3
10.8
11.3
11.7
11.5
10.7
10.0
9.3
8.7
July, 2014
58-590000-67A11_sec05.fm Page 39 Tuesday, July 29, 2014 8:32 AM