TM 1-1510-225-10
7-98
MAXIMUM RANGE POWER
1700 RPM
ISA + 30 °C
NOTES: DURING OPERATION WITH ICE VANES EXTENDED, TORQUE WILL DECREASE. IN
ORDER TO MAINTAIN MAXIMUM RANGE CONFIGURATION, DO NOT RESET POWER TO
ORIGINAL SETTING. FUEL FLOW WILL REMAIN ABOUT THE SAME, BUT TRUE AIRSPEED
WILL BE REDUCED APPROXIMATELY 10 KNOTS.
TO OBTAIN FUEL FLOW PER ENGINE, DIVIDE THE TOTAL FUEL FLOW VALUE FOR THE
CORRESPONDING ALTITUDE BY TWO.
WEIGHT Ü
13,000 POUNDS
12,000 POUNDS
PRESSURE
ALT
IOAT
OAT
TORQUE PER
ENGINE
FUEL
FLOW
TOTAL
IAS
TAS
TORQUE PER
ENGINE
FUEL
FLOW
TOTAL
IAS
TAS
FEET
°C
°C
FT-LB
%
LB/HR
KTS
KTS
FT-LB
%
LB/HR
KTS
KTS
SL
49
45
1673
75
820
205
217
1561
70
798
202
214
2,000
45
41
1561
70
768
198
215
1494
67
750
196
213
4,000
41
37
1516
68
726
193
216
1450
65
710
192
215
6,000
37
33
1472
66
690
189
218
1427
64
674
188
217
8,000
34
29
1427
64
650
184
219
1383
62
636
183
218
10,000
30
25
1383
62
612
179
19
1338
60
596
178
219
12,000
26
21
1360
61
582
174
221
1316
59
566
174
220
14,000
22
17
1338
60
556
170
223
1271
57
538
169
221
16,000
18
13
1338
60
536
167
226
1249
56
514
165
224
18,000
14
9
1338
60
518
163
229
1249
56
496
162
227
20,000
10
5
1316
59
504
160
232
1249
56
480
159
230
22,000
6
1
1338
60
498
159
238
1227
55
464
155
232
24,000
3
-3
1383
62
498
158
245
1227
55
452
151
235
26,000
-1
-7
1360
61
486
153
246
1271
57
456
152
244
28,000
-5
-11
1249
56
448
148
246
29,000
31,000
33,000
35,000
Figure 7-88. Maximum Range Power, 1700 RPM, ISA + 30 °C (Sheet 1 of 2)