TM 1-1510-223-10
MAXIMUM CRUISE POWER
1700 RPM
ISA -30°C
WEIGHT®
12,000 POUNDS
10,000 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
-11
-15
83
611
1222
215
206
83
611
1122
216
206
2000
-15
-19
83
592
1184
214
210
83
592
1184
215
211
4000
-19
-23
83
574
1148
214
216
83
574
1148
215
217
6000
-22
-27
83
559
1118
212
220
83
559
1118
213
221
8000
-26
-31
83
546
1092
211
225
83
546
1092
212
227
10,000
-30
-35
83
538
1076
209
230
83
538
1076
210
231
12,000
-34
-39
83
530
1060
207
235
83
530
1060
208
236
14,000
-37
-43
83
523
1046
205
239
83
523
1046
206
241
16,000
-41
-47
83
517
1034
203
245
83
517
1034
204
246
18,000
-45
-51
83
513
1026
201
250
83
512
1024
202
251
20,000
-49
-55
83
509
1018
199
255
83
508
1016
200
257
22,000
-52
-59
83
505
1010
197
261
83
504
1008
198
263
24,000
-56
-63
79
481
962
191
262
80
482
964
193
264
26,000
-60
-67
73
446
892
183
259
73
447
894
185
262
28,000
-65
-70
66
404
808
173
254
66
405
810
176
258
29,000
-67
-72
62
383
766
168
251
62
385
770
171
255
31,000
-71
-76
55
346
692
157
244
55
347
694
161
249
33,000
-75
-80
49
311
622
147
237
49
313
626
151
244
35,000
-80
-84
42
277
554
134
226
43
279
558
140
235
BT03278
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 7-42. Maximum Cruise Power at 1700 RPM - ISA -30 °C (Sheet 2 of 2) IR
7-54 Change 2