TM 1-1510-224-10
MAXIMUM CRUISE POWER
1700 RPM
ISA +37°C
WEIGHT®
16,000 POUNDS
14,000 POUNDS
PRESSURE
ALTITUDE
IFAT
FAT
TORQUE
PER
ENGINE
FUEL
FLOW
PER
ENGINE
TOTAL
FUEL
FLOW
IAS
TAS
TORQUE
PER
ENGINE
FUEL
FLOW
PER
ENGINE
TOTAL
FUEL
FLOW
IAS
TAS
FEET
°C
°C
PERCENT
LBS/HR
LBS/HR
KTS
KTS
PERCENT
LBS/HR
LBS/HR
KTS
KTS
0
57
52
73
607
1214
212
227
74
607
1214
214
230
2000
53
48
72
577
1154
208
230
72
577
1154
211
232
4000
49
44
70
548
1096
204
232
70
548
1096
206
235
6000
45
40
68
522
1044
199
234
68
522
1044
202
237
8000
41
36
66
495
990
194
235
66
495
990
197
239
10,000
37
32
63
467
934
189
236
64
468
936
192
240
12,000
33
28
60
436
872
181
234
60
437
874
185
239
14,000
29
24
56
407
814
174
232
57
437
874
185
239
16,000
25
20
53
378
756
165
228
53
379
758
170
236
18,000
21
16
48
349
698
155
222
49
350
700
162
231
20,000
17
12
44
323
646
144
214
45
324
648
152
226
22,000
12
8
41
302
604
132
204
42
304
608
143
221
24,000
9
4
---
---
---
---
---
38
283
566
133
213
26,000
4
0
---
---
---
---
---
36
266
532
123
206
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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BT05868
NOTE
During operations with ice vanes extended, torque will decrease approximately
12%, fuel flow will decrease approximately 8%, and true airspeed will be reduced
by approximately 15 knots.
Figure 7A-47. Maximum Cruise Power at 1700 RPM - ISA +37°C (Sheet 1 of 2)
7A-72
