TM 1-1510-225-10
7-108
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
-2
-5
2230
100
520
187
181
189
184
191
185
193
187
2000
-6
-9
2230
100
505
185
184
187
187
189
189
191
190
4000
-10
-13
2230
100
492
182
187
185
190
187
192
189
194
6000
-13
-17
2230
100
480
180
190
182
193
184
195
186
197
8000
-17
-21
2230
100
468
177
193
180
196
182
198
184
201
10,000
-21
-25
2230
100
456
174
196
177
199
180
202
182
204
12,000
-25
-29
2230
100
446
171
198
175
202
177
205
179
207
14,000
-29
-33
2230
100
440
168
201
172
205
175
208
177
211
16,000
-33
-37
2163
97
423
162
199
166
204
170
209
173
212
18,000
-37
-41
2052
92
400
154
195
159
202
163
207
166
211
20,000
-41
-45
1940
87
378
144
190
151
199
156
205
160
210
22,000
-45
-49
1829
82
356
131
178
142
193
149
202
154
208
24,000
-50
-53
1673
75
326
127
179
138
194
145
203
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-96. Maximum Cruise Power, 1900 RPM, ISA 20 °C