TM 1-1510-223-10
NORMAL CRUISE POWER
1500 RPM
ISA +10°C
WEIGHT®
16,000 POUNDS
14,000 POUNDS
TORQUE
FUEL
TOTAL
TORQUE
FUEL
TOTAL
PRESSURE
PER
FLOW
FUEL
PER
FLOW
FUEL
ALTITUDE
IFAT
FAT
ENGINE
PER
FLOW
IAS
TAS
ENGINE
PER
FLOW
IAS
TAS
ENGINE
ENGINE
FEET
°C
°C
PERCENT
LBS/HR
LBS/HR
KTS
KTS
PERCENT LBS/HR LBS/HR
KTS
KTS
0
29
25
94
624
1248
209
215
94
624
1248
211
216
2000
25
21
94
604
1208
207
219
94
603
1206
208
220
4000
22
17
94
586
1172
204
223
94
585
1170
206
224
6000
18
13
94
571
1142
202
227
94
570
1140
204
229
8000
14
9
94
559
1118
200
231
94
559
1118
202
233
10,000
10
5
91
538
1076
195
233
92
539
1078
197
235
12,000
6
1
87
510
1020
189
233
88
511
1022
191
236
14,000
2
-3
83
483
966
183
233
83
484
968
186
236
16,000
-2
-7
79
456
912
176
232
79
457
914
179
236
18,000
-6
-11
74
430
860
169
230
74
430
860
173
235
20,000
-10
-15
69
404
808
161
228
70
405
810
166
233
22,000
-14
-19
65
380
760
153
224
65
381
762
159
231
24,000
-18
-23
60
356
712
144
219
61
357
714
151
228
26,000
-22
-27
56
332
664
134
212
56
334
668
142
224
28,000
-26
-30
---
---
---
---
---
52
311
622
133
218
29,000
-28
-32
---
---
---
---
---
50
300
600
128
214
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
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BT03629
NOTE
During operations with ice vanes extended, torque will decrease approximately 10
percentage points (E. G., 64% - 10 percentage points = 54%), fuel flow will
decrease approximately 35 LBS/HR/ENG, and true airspeed will be reduced
approximately 20 knots.
Figure 7-73. Normal Cruise Power at 1500 RPM - ISA +10 °C (Sheet 1 of 2) IR
7-108 Change 2