TM 1-1510-224-10
ON E-ENGINE-INOPERATIVE
MAXIMUM CRUISE POWER
1700 RPM
ISA +37°C
WEIGHT®
16,000 POUNDS
14,000 POUNDS
PRESSURE
ALTITUDE
IFAT
FAT
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
596
596
133
144
67
598
598
144
156
2000
50
48
---
---
---
---
---
66
568
568
140
157
4000
46
44
---
---
---
---
---
64
539
539
136
157
6000
42
40
---
---
---
---
---
62
511
511
131
156
8000
38
36
---
---
---
---
---
60
482
482
123
151
10,000
---
---
---
---
---
---
---
---
---
---
---
---
12,000
---
---
---
---
---
---
---
---
---
---
---
---
14,000
---
---
---
---
---
---
---
---
---
---
---
---
16,000
---
---
---
----
---
---
---
---
---
---
---
---
18,000
---
---
---
---
---
---
---
---
---
---
---
---
20,000
---
---
---
---
---
---
---
---
---
---
---
---
22,000
---
---
---
---
---
---
---
---
---
---
---
---
24,000
---
---
---
---
---
---
---
---
---
---
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---
26,000
---
---
---
---
---
---
---
---
---
---
---
---
28,000
--
---
---
---
---
---
---
---
---
---
---
---
29,000
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT05870
NOTE
During operations with ice vanes extended, torque will decrease approximately
10%0/, fuel flow will decrease approximately 6%, and true airspeed will be reduced by
approximately 10 knots.
Figure 7A-93. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +37°C (Sheet 1 of 2)
7A-150
