TM 1-1510-218-10
7-84
ONE ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1900 RPM
ISA -20 °C
NOTE:
FOR OPERATION WITH ICE VANE EXTENDED, DECREASE FUEL FLOW AND TAS BY 7%.
AIRSPEED ~ KNOTS
PRESSURE
ALT
IOAT
OAT
TORQUE
PER
ENGINE
FUEL FLOW
TOTAL
@12,000 LB
@11,000 LB
@10,000 LB
FEET
° C
° C
%
LB/HR
IAS
TAS
IAS
TAS
IAS
TAS
SL
-2
-5
100
515
189
184
191
185
193
187
2,000
-6
-9
100
501
187
187
189
189
191
190
4,000
-10
-13
100
489
185
190
187
192
189
194
6,000
-13
-17
100
478
182
193
184
195
186
197
8,000
-17
-21
100
467
180
196
182
198
184
200
10,000
-21
-25
100
460
177
199
180
202
182
204
12,000
-25
-29
100
454
175
202
177
205
180
207
14,000
-29
-33
99
445
171
203
174
207
177
210
16,000
-33
-37
92
416
162
199
166
204
169
208
18,000
-37
-41
86
387
153
195
158
201
162
205
20,000
-41
-45
80
360
143
188
149
196
154
202
22,000
-45
-48
74
335
130
177
139
189
145
197
24,000
-50
-52
68
310
127
179
136
191
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-80. One-Engine-Inoperative Maximum Cruise Power - 1900 RPM, - ISA 20 °C