TM 1-1510-225-10
7-88
MAXIMUM RANGE POWER
1700 RPM
ISA 20 °C
NOTES: DURING OPERATION WITH ICE VANES E XTENDED, 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
-1
-5
1717
77
814
214
207
1650
74
796
211
205
2,000
-5
-9
1606
72
758
206
205
1494
67
734
202
201
4,000
-9
-13
1494
67
702
197
202
1405
63
678
194
199
6,000
-13
-17
1405
63
654
191
201
1316
59
632
187
198
8,000
-17
-21
1338
60
612
185
201
1249
56
588
181
197
10,000
-21
-25
1271
57
568
178
200
1182
53
544
175
196
12,000
-25
-29
1249
56
540
174
201
1160
52
514
170
197
14,000
-29
-33
1227
55
514
170
202
1115
50
486
166
198
16,000
-33
-37
1204
54
490
165
203
1093
49
460
161
198
18,000
-37
-41
1182
53
472
162
205
1070
48
440
157
199
20,000
-41
-45
1182
53
465
158
207
1048
47
420
152
200
22,000
-45
-49
1182
53
446
156
211
1048
47
408
150
203
24,000
-49
-53
1204
54
444
155
217
1070
48
404
149
208
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-83. Maximum Range Power, 1700 RPM, ISA 20 °C (Sheet 1 of 2)