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EAPS Penalty Table (Continued) - TM-1-1520-240-10_475
EAPS Penalty Table (Continued) - TM-1-1520-240-10_477
TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-10
7A-7-4
Table 7A-7-1. EAPS Penalty Table (Continued)
Increase Total
Fuel Flow By
Decrease
Torque
Available (%)
Pressure
Altitude (ft)
OAT
(
_
C)
(lb/hr)
KTAS = 0
85
135
160
12000
-50
30
2
2
5
6
-40
30
2
2
4
6
-30
30
2
2
4
6
-20
30
2
3
7
10
-10
30
2
3
7
9
0
30
2
3
7
9
10
30
2
3
6
9
20
30
2
3
6
9
30
30
2
3
6
8
40
30
2
3
6
8
50
30
2
3
6
8
14000
-50
30
2
2
5
6
-40
30
2
2
4
6
-30
30
2
2
4
6
-20
30
2
3
7
10
-10
30
2
3
7
9
0
30
2
3
7
9
10
30
2
3
6
9
20
30
2
3
6
9
30
30
2
3
6
8
40
30
2
3
6
8
50
30
2
3
6
8
16000
-50
30
2
2
5
6
-40
30
2
2
4
6
-30
30
2
2
4
6
-20
30
2
3
7
10
-10
30
2
3
7
9
0
30
2
3
7
9
10
30
2
3
6
9
20
30
2
3
6
9
30
30
2
3
6
8
40
30
2
3
6
8
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