TM 1-1510-223-10
NORMAL CRUISE POWER
1500 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
84
606
1212
204
216
84
606
1212
206
219
2000
45
41
82
576
1152
199
218
82
576
1152
202
220
4000
42
37
79
546
1092
195
219
79
546
1092
197
222
6000
38
33
76
517
1034
189
220
77
517
1034
192
223
8000
34
29
74
489
978
184
221
74
489
978
187
224
10,000
30
25
71
461
922
179
221
71
462
924
182
225
12,000
26
21
68
436
872
174
222
69
437
874
177
226
14,000
22
17
66
413
826
168
222
66
413
826
172
227
16,000
18
13
62
387
774
160
220
62
387
774
165
226
18,000
14
9
56
356
712
150
213
56
358
716
156
221
20,000
9
5
51
329
658
139
205
52
331
662
147
216
22,000
5
1
48
309
618
129
198
49
311
622
139
212
24,000
1
-3
44
288
576
115
184
45
291
582
131
207
26,000
-3
-7
---
---
---
---
---
43
273
546
121
201
28,000
-7
-10
---
---
---
---
---
40
257
514
110
190
29,000
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT0559113
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 7-78. Normal Cruise Power at 1500 RPM - ISA +30 °C (Sheet 1 of 2) CA
7-118 Change 2
