TM 1-1510-224-10
ONE-ENGINE INOPERATIVE
MAXIMUM CRUISE POWER
1700 RPM
ISA +30°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
47
45
75
625
625
148
159
75
626
626
157
168
2000
43
41
73
595
595
143
158
74
597
597
153
168
4000
39
37
70
565
565
136
156
71
567
'567
148
168
6000
36
33
---
---
---
---
---
69
538
538
142
167
8000
32
29
---
---
---
---
---
66
508
508
135
164
10,000
28
25
---
---
---
---
---
63
476
476
126
159
12,000
---
---
---
---
---
---
---
---
---
---
---
---
14,000
---
---
---
---
---
---
---
---
---
---
---
---
16,000
---
---
---
---
---
---
---
---
---
---
---
---
18,000
---
---
---
---
---
---
---
---
---
---
---
---
20,000
---
---
---
---
---
---
---
---
---
---
---
---
22,000
---
---
---
---
---
---
---
---
---
---
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---
24,000
---
---
---
---
---
---
---
---
---
---
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---
26,000
---
---
---
---
---
---
---
---
---
---
---
---
28,000
---
---
---
---
---
---
---
---
---
---
---
---
29,000
---
---
---
---
---
---
---
---
---
---
---
---
31,000
---
---
---
---
---
---
---
---
---
---
---
---
33,000
---
---
---
---
---
---
---
---
---
---
---
---
35,000
---
---
---
---
---
---
---
---
---
---
---
---
BT058703
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-92. One Engine Inoperative Max Cruise Power at 1700 RPM (Ice Vanes Retracted) - ISA +30°C (Sheet 1 of 2)
7A-148
