TM 1-1510-223-10
MAXIMUM CRUISE POWER
1700 RPM
ISA +30°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
49
45
83
624
1248
206
219
83
623
1246
208
220
2000
46
41
83
604
1208
204
223
83
603
1206
205
225
4000
42
37
81
576
1152
199
225
81
576
1152
201
227
6000
38
33
78
547
1094
194
226
79
547
1094
197
228
8000
34
29
75
518
1036
189
227
75
519
1038
191
229
10,000
30
25
72
490
980
183
227
72
490
980
186
230
12,000
26
21
68
459
918
177
226
68
460
920
180
230
14,000
22
17
64
430
860
170
224
64
431
862
173
229
16,000
18
13
59
401
802
161
221
59
401
802
165
226
18,000
14
9
53
370
740
151
214
54
371
742
156
221
20,000
9
5
49
344
688
141
208
50
345
690
148
217
22,000
5
1
46
324
648
133
203
47
326
652
141
215
24,000
1
-3
43
304
608
122
195
44
306
612
133
211
26,000
-3
-7
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41
288
576
125
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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BT03289
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 7-54. Maximum Cruise Power at 1700 RPM - ISA +30 °C (Sheet 1 of 2) IR
Change 2 7-77
