TM 1-1510-223-10
ONE-ENGINE-INOPERATIVE MAXIMUM CRUISE POWER
1700 RPM
ISA +30°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
47
45
79
624
624
139
149
80
625
625
146
156
2000
43
41
77
593
593
134
148
78
595
595
141
157
4000
39
37
75
563
563
127
146
75
565
565
137
156
6000
35
33
---
---
---
---
---
73
535
535
131
155
8000
31
29
---
---
---
---
---
69
505
505
124
152
10,000
27
25
---
---
---
---
---
66
473
473
116
147
12,000
23
21
---
---
---
---
---
62
441
441
103
136
14,000
---
---
---
---
---
---
---
---
---
---
---
---
16,000
---
---
---
---
---
---
---
---
---
---
---
---
18,000
---
---
---
---
---
---
---
---
---
---
---
---
20,000
---
---
---
---
---
---
---
---
---
---
---
---
22,000
---
---
---
---
---
---
---
---
---
---
---
---
24,000
---
---
---
---
---
---
---
---
---
---
---
---
26,000
---
---
---
---
---
---
---
---
---
---
---
---
28,000
---
---
---
---
---
---
---
---
---
---
---
---
29,000'
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT03649
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 7-138. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 °C (Sheet 1 of 2) IR
Change 2 7-225
