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
43
41
74
623
623
139
149
74
624
624
146
157
2000
43
41
72
593
593
134
149
73
595
595
143
158
4000
39
37
70
563
563
128
147
71
565
565
138
157
6000
35
33
---
---
---
---
---
68
536
536
133
157
8000
31
29
---
---
---
---
---
66
506
506
126
154
10,000
27
25
---
---
---
---
---
62
473
473
118
149
12,000
23
21
---
---
---
---
---
59
442
442
106
140
14,000
---
---
---
---
---
---
---
---
---
---
---
---
16,000
---
---
---
---
---
---
---
---
---
---
---
---
18,000
---
---
---
---
---
---
---
---
---
---
---
---
20,000
---
---
---
---
---
---
---
---
---
---
---
---
22,000
---
---
---
---
---
---
---
---
---
---
---
---
24,000
---
---
---
---
---
---
---
---
---
---
---
---
26,000
---
---
---
---
---
---
---
---
---
---
---
---
28,000
---
---
---
---
---
---
---
---
---
---
---
---
29,000
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT0559013
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 7-139. One Engine Inoperative Max Cruise Power at 1700 RPM - ISA +30 °C (Sheet 1 of 2) CA
Change 2 7-227
