TM 1-1510-223-10
ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER
1700 RPM
ISA +37°C
WEIGHT®
16,000 POUNDS
14,000 POUNDS
TORQUE
FUEL
TOTAL
TORQUE
FUEL
TOTAL
PRESSURE
PER
FLOW
FUEL
PER
FLOW
FUEL
ALTITUDE
IFAT
FAT
ENGINE
PER
FLOW
IAS
TAS
ENGINE
PER
FLOW
IAS
TAS
ENGINE
ENGINE
FEET
°C
°C
PERCENT
LBS/HR
LBS/HR
KTS
KTS
PERCENT LBS/HR LBS/HR
KTS
KTS
0
54
52
71
598
598
127
139
72
599
599
136
148
2000
50
48
---
---
---
---
---
70
568
568
132
149
4000
46
44
---
---
---
---
---
68
538
538
128
148
6000
42
40
---
---
---
---
---
66
510
510
122
146
8000
38
36
---
---
---
---
---
63
481
481
114
142
10,000
34
32
---
---
---
---
---
59
448
448
101
131
12,000
---
---
---
---
---
---
---
---
---
---
---
---
14,000
---
---
---
---
---
---
---
---
---
---
---
---
16,000
---
---
---
---
---
---
---
---
---
---
---
---
18,000
---
---
---
---
---
---
---
---
---
---
---
---
20,000
---
---
---
---
---
---
---
---
---
---
---
---
22,000
---
---
---
---
---
---
---
---
---
---
---
---
24,000
---
---
---
---
---
---
---
---
---
---
---
---
26,000
---
---
---
---
---
---
---
---
---
---
---
---
28,000
---
---
---
---
---
---
---
---
---
---
---
---
29,000
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT03651
NOTE
During operations with ice vanes extended, torque will decrease approximately 7
percentage points (E. G., 67% - 7 percentage points = 60%), fuel flow will decrease
approximately 25 LBS/HR/ENG, and true airspeed will be reduced approximately 15
knots.
Figure 7-140. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +37 °C (Sheet 1 of 2) IR
Change 2 7-229
