TM 1-1510-218-10
7-86
ONE ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1900 RPM
ISA
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
18
15
100
522
186
187
188
189
490
191
2,000
14
11
100
508
184
190
186
192
188
194
4,000
11
7
100
494
181
193
184
196
186
198
6,000
7
3
100
482
179
196
181
199
184
201
8,000
3
-1
100
472
176
200
179
202
181
205
10,000
-1
-5
100
462
174
202
176
205
179
208
12,000
-5
-9
97
445
168
203
172
206
174
210
14,000
-9
-13
91
416
160
199
164
204
167
208
16,000
-13
-17
85
388
151
194
456
200
160
205
18,000
-17
-20
79
361
141
187
147
195
152
201
20,000
-21
-25
73
334
126
173
137
188
143
196
22,000
-26
-28
67
311
125
177
134
190
24,000
-31
-32
60
283
123
181
26,000
28,000
29,000
31,000
33,000
35,000
Figure 7-82. One-Engine-Inoperative Maximum Cruise Power - 1900 RPM, - ISA