TM 1-1510-225-10
7-113
ONE ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1900 RPM
ISA + 30 °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
48
45
2163
97
521
176
186
179
189
182
192
184
194
2000
44
41
2096
94
499
172
187
175
190
178
193
180
196
4000
40
37
2052
92
478
167
188
171
192
174
195
177
198
6000
37
33
2007
90
453
162
187
166
192
169
195
172
199
8000
33
29
1918
86
425
154
184
159
190
163
194
166
198
10,000
28
25
1829
82
397
146
180
152
187
157
193
160
198
12,000
24
21
1739
78
375
137
175
145
185
151
192
155
197
14,000
20
17
1695
76
358
126
166
138
182
145
191
150
197
16,000
16
13
1628
73
342
130
177
139
189
145
197
18,000
13
9
1606
72
329
133
187
140
196
20,000
8
5
1561
70
316
125
181
134
195
22,000
5
1
1472
66
297
125
189
24,000
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-101. One Engine Inoperative Maximum Cruise Power, 1900 RPM, ISA + 30 °C