TM 1-1510-218-10
7A-86
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
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
%
LB/HR
KTS
KTS
%
LB/HR
KTS
KTS
SL
-11
-15
73
788
210
200
69
768
207
197
2,000
-15
-19
67
730
201
197
64
710
199
195
4,000
-20
-23
63
674
194
195
59
654
191
192
6,000
-24
-27
59
628
187
194
55
604
184
191
8,000
-28
-31
56
584
181
193
52
560
177
189
10,000
-32
-35
54
546
175
193
49
520
171
189
12,000
-35
-39
53
516
171
194
48
488
167
189
14,000
-39
-43
51
490
167
194
46
460
162
189
16,000
-43
-47
50
468
163
196
45
436
158
190
18,000
-47
-51
50
446
158
197
44
412
153
190
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 1 of 2)