TM 1-1510-225-10
7-89
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
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
-1
-5
1561
70
776
208
202
1494
67
760
206
200
2,000
-5
-9
1427
64
716
199
199
1360
61
698
197
196
4,000
-9
-13
1316
59
660
191
196
1249
56
642
189
194
6,000
-13
-17
1249
56
612
185
195
1160
52
592
182
192
8,000
-17
-21
1160
52
568
178
194
1093
49
546
175
191
10,000
-21
-25
1093
49
522
171
192
1004
45
500
168
188
12,000
-25
-29
1048
47
490
167
193
959
43
466
163
188
14,000
-29
-33
1026
46
460
162
193
914
41
434
157
187
16,000
-33
-37
981
44
432
156
192
847
38
402
151
186
18,000
-37
-41
937
42
408
152
193
825
37
374
145
185
20,000
-41
-45
914
41
384
147
192
781
35
348
139
183
22,000
-45
-49
914
41
370
143
195
758
34
332
136
185
24,000
-49
-53
937
42
366
142
200
803
36
328
136
191
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-83. Maximum Range Power, 1700 RPM, ISA 20 °C (Sheet 2 of 2)