TM 1-1510-225-10
7-87
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
11,000 POUNDS
10,000 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
1472
66
734
205
195
1405
63
736
203
193
2,000
-15
-19
1360
61
694
197
192
1271
57
672
194
190
4,000
-20
-23
1227
55
632
188
189
1137
51
612
184
186
6,000
-24
-27
1137
51
580
180
187
1048
47
556
176
183
8,000
-28
-31
1070
48
534
173
185
959
43
510
169
180
10,000
-32
-35
1004
45
492
167
184
892
40
466
162
179
12,000
-35
-39
959
43
458
162
184
847
38
430
157
178
14,000
-39
-43
914
41
428
156
183
781
35
398
150
176
16,000
-43
-47
870
39
402
152
183
758
34
368
145
175
18,000
-47
-51
847
38
376
146
182
691
31
338
138
172
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 2 of 2)