TM 1-1510-225-10
7-111
ONE ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1900 RPM
ISA + 10 °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
28
25
2230
100
527
182
187
185
189
187
191
189
193
2000
24
21
2230
100
513
180
189
182
192
185
194
186
196
4000
21
17
2230
100
499
177
192
180
195
182
198
184
200
6000
17
13
2230
100
484
174
195
177
198
180
200
182
203
8000
13
9
2230
100
470
171
197
174
201
177
204
179
207
10,000
9
5
2119
95
441
164
195
168
199
171
203
174
207
12,000
5
1
2029
91
415
157
192
161
198
165
202
168
206
14,000
1
-3
1940
87
395
149
189
155
196
160
202
163
206
16,000
-3
-7
1873
84
376
141
184
148
194
153
201
158
206
18,000
-7
-11
1784
80
355
128
173
140
189
147
198
151
205
20,000
-12
-15
1695
76
338
130
182
139
195
145
203
22,000
-15
-19
1606
72
319
128
186
137
198
24,000
-19
-23
1494
67
296
126
190
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-99. One Engine Inoperative Maximum Cruise Power, 1900 RPM, ISA + 10 °C