TM 1-1510-224-10
ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER
1700 RPM
ISA +37°C
WEIGHT®
16,000 POUNDS
14,000 POUNDS
PRESSURE
ALTITUDE
IOAT
OAT
TORQUE
PER
ENGINE
FUEL
FLOW
PER
ENGINE
TOTAL
FUEL
FLOW
IAS
TAS
TORQUE
PER
ENGINE
FUEL
FLOW
PER
ENGINE
TOTAL
FUEL
FLOW
IAS
TAS
FEET
°C
°C
PERCENT
LBS/HR
LBS/HR
KTS
KTS
PERCENT
LBS/HR
LBS/HR
KTS
KTS
0
54
52
66
597
597
135
147
67
598
598
146
159
2000
50
48
---
---
---
---
---
66
569
569
143
159
4000
46
44
---
---
---
---
---
64
540
540
138
160
6000
42
40
---
---
---
---
---
62
512
512
133
159
8000
38
36
---
---
---
---
---
60
482
482
125
154
10,000
---
---
---
---
---
---
---
---
---
---
---
---
12,000
---
---
---
---
---
---
---
---
---
---
---
---
14,000
---
---
---
---
---
---
---
---
---
---
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16,000
----
---
---
---
---
---
---
---
---
---
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18,000
----
---
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---
---
---
---
---
---
---
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20,000
---
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---
---
---
---
---
---
---
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22,000
---
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---
---
---
---
---
---
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24,000
---
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---
---
---
---
---
---
---
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26,000
---
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---
---
---
---
---
---
---
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28,000
---
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---
---
---
---
---
---
---
---
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29,000
---
---
---
---
---
---
---
---
---
---
---
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31,000
---
---
---
---
---
---
---
---
---
---
---
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33,000
----
---
---
---
---
---
---
---
---
---
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35,000
---
---
---
---
---
---
---
---
---
---
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BT05290
NOTE
During operations with ice vanes extended, torque will decrease approximately
10%, fuel flow will decrease approximately 6%, and true airspeed will be reduced
by approximately 10 knots.
Figure 7-93, One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37°C (Sheet 1 of 2)
7-150
