TM 1-1510-218-10
7A-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
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
%
LB/HR
KTS
KTS
%
LB/HR
KTS
KTS
SL
-11
-15
66
734
205
195
63
736
203
193
2,000
-15
-19
61
694
197
192
57
672
194
190
4,000
-20
-23
55
632
188
189
51
612
184
186
6,000
-24
-27
51
580
180
187
47
556
176
183
8,000
-28
-31
48
534
173
185
43
510
169
180
10,000
-32
-35
45
492
167
184
40
466
162
179
12,000
-35
-39
43
458
162
184
38
430
157
178
14,000
-39
-43
41
428
156
183
35
398
150
176
16,000
-43
-47
39
402
152
183
34
368
145
175
18,000
-47
-51
38
376
146
182
31
338
138
172
20,000
22,000
24,000
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7A-82. Maximum Range Power, 1700 RPM, ISA 30 C (Sheet 2 of 2)
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