TM 1-1510-225-10
7-112
ONE ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1900 RPM
ISA + 20 °C
NOTES: DURING OPERATION WITH ICE VANE EXTENDED, TORQUE WILL DECREASE. IF
ORIGINAL POWER IS NOT OR CANNOT BE RESET, TRUE AIRSPEED WILL DECREASE
APPROXIMATELY 20 KNOTS AND FUEL FLOW WILL DECREASE APPROXIMATELY 7%. IF
ORIGINAL POWER IS RESET, TRUE AIRSPEED WILL BE UNCHANGED AND FUEL FLOW
WILL INCREASE APPROXIMATELY 30 LB/HR/ENG.
IOAT, TORQUE, AND FUEL FLOW BASED ON 12,000 POUNDS.
TO OBTAIN FUEL FLOW PER ENGINE, DIVIDE THE TOTAL FUEL FLOW VALUE FOR THE
CORRESPONDING ALTITUDE BY TWO.
AIRSPEED ~ KNOTS
PRESSURE
ALT
IOAT OAT
TORQUE PER
ENGINE
TOTAL
FUEL
FLOW
13,000 LB
12,000 LB
11,000 LB
10,000 LB
FEET
° C
° C
FT-LB
%
LB/HR
IAS
TAS
IAS
TAS
IAS
TAS
IAS
TAS
SL
38
35
2230
100
530
181
188
183
191
185
193
187
195
2000
35
31
2230
100
515
178
191
181
194
183
196
185
198
4000
31
27
2230
100
500
176
194
178
197
181
200
183
202
6000
27
23
2163
97
475
170
193
173
197
176
200
178
203
8000
23
19
2052
92
447
163
191
167
196
170
200
173
203
10,000
19
15
1962
88
418
155
188
160
194
164
198
167
202
12,000
15
11
1873
84
394
148
185
153
192
158
197
161
202
14,000
11
7
1829
82
376
140
180
147
190
153
197
157
202
16,000
7
3
1762
79
359
129
172
140
187
147
196
152
202
18,000
2
-1
1695
76
343
132
182
141
194
146
201
20,000
-1
-5
1628
73
327
133
189
140
199
22,000
-6
-9
1539
69
307
120
178
132
195
24,000
-9
-13
1427
64
285
120
184
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-100. One Engine Inoperative Maximum Cruise Power, 1900 RPM, ISA + 20 °C