TM 1-1510-225-10
7-86
MAXIMUM RANGE POWER
1700 RPM
ISA 30 °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
-11
-15
1628
73
788
210
200
1539
69
768
207
197
2,000
-15
-19
1494
67
730
201
197
1427
64
710
199
195
4,000
-20
-23
1405
63
674
194
195
1316
59
654
191
192
6,000
-24
-27
1316
59
628
187
194
1227
55
604
184
191
8,000
-28
-31
1249
56
584
181
193
1160
52
560
177
189
10,000
-32
-35
1204
54
546
175
193
1093
49
520
171
189
12,000
-35
-39
1182
53
516
171
194
1070
48
488
167
189
14,000
-39
-43
1137
51
490
167
194
1026
46
460
162
189
16,000
-43
-47
1115
50
468
163
196
1004
45
436
158
190
18,000
-47
-51
1115
50
446
158
197
981
44
412
153
190
20,000
22,000
24,000
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-82. Maximum Range Power, 1700 RPM, ISA 30 °C (Sheet 1 of 2)