TM 1-1510-218-10
7-60
RECOMMENDED CRUISE POWER
1800 RPM
ISA + 37 °C
NOTE:
TO OBTAIN FUEL FLOW PER ENGINE, DIVIDE THE TOTAL FUEL FLOW VALUE FOR
THE CORRESPONDING ALTITUDE BY TWO.
AIRSPEED ~ KNOTS
PRESSURE
ALT
IOAT
OAT
TORQUE
PER
ENGINE
FUEL FLOW
TOTAL
@12,000 LB
@11,000 LB
@10,000 LB
FEET
° C
° C
%
LB/HR
IAS
TAS
IAS
TAS
IAS
TAS
SL
58
52
97
982
232
243
234
249
235
250
2,000
54
48
95
942
228
251
230
252
231
253
4,000
50
44
93
902
224
254
226
255
227
256
6,000
46
40
91
866
220
257
222
259
223
260
8,000
42
36
89
826
216
259
217
261
218
263
10,000
39
32
85
780
210
260
212
262
213
264
12,000
35
28
81
736
203
260
205
263
207
265
14,000
31
24
76
690
196
259
198
262
200
264
16,000
27
20
72
648
189
258
191
261
193
264
18,000
23
16
68
608
181
256
184
260
182
263
20,000
19
12
64
568
173
254
177
258
179
262
22,000
15
9
60
532
165
250
169
256
172
260
24,000
10
5
56
496
156
245
161
252
165
258
26,000
6
1
52
462
146
237
152
247
157
254
28,000
2
-3
48
430
134
226
142
240
148
250
29,000
0
-5
46
414
125
216
134
235
144
247
31,000
-5
-9
42
382
---
---
123
220
133
238
33,000
---
---
---
---
---
---
---
---
---
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35,000
---
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Figure 7-56. Recommended Cruise Power, 1800 RPM - ISA + 37 °C
