TM 1-1510-223-10
NORMAL CRUISE POWER
1500 RPM
ISA + 37°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
56
52
75
581
1162
194
208
76
581
1162
196
211
2000
52
48
73
550
1100
190
210
73
551
1102
192
213
4000
48
44
71
520
1040
185
211
71
520
1040
188
214
6000
44
40
69
491
982
180
212
69
491
982
183
216
8000
40
36
66
464
928
175
213
67
464
928
179
217
10,000
36
32
64
438
876
170
214
64
438
876
174
218
12,000
32
28
62
414
828
165
214
62
415
830
169
219
14,000
29
24
60
391
782
159
214
60
392
784
164
220
16,000
24
20
56
365
730
152
211
57
366
732
157
218
18,000
20
16
51
336
672
141
203
52
337
674
148
213
20,000
16
12
46
307
614
127
191
47
310
620
138
207
22,000
11
8
42
285
570
110
172
44
289
578
129
200
24,000
8
4
---
---
---
---
---
40
268
536
117
190
26,000
3
0
---
---
---
---
---
37
251
502
104
176
28,000
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29,000
---
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31,000
---
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33,000
---
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35,000
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BT0559115
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 7-80. Normal Cruise Power at 1500 RPM - ISA +37 °C (Sheet 1 of 2) CA
7-122 Change 2
