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EAPS Penalty Table (Continued) - TM-1-1520-240-10_360
CRUISE EXAMPLE
TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-10
7-7-5
Table 7-7-1 EAPS Penalty Table (Continued)
Increase Total
Decrease
Torque
Available (%)
Pressure
Altitude (ft)
OAT
(
_
C)
Fuel Flow By
(lb/hr)
KTAS = 0
85
135
160
18000
-50
25
2
2
5
6
-40
25
2
2
4
6
-30
25
2
2
4
6
-20
25
2
3
7
10
-10
25
2
3
7
9
0
25
2
3
7
9
10
25
2
3
6
9
20
25
2
3
6
9
20000
-50
25
2
2
5
6
-40
25
2
2
4
6
-30
25
2
2
4
6
-20
25
2
3
7
10
-10
25
2
3
7
9
0
25
2
3
7
9
10
25
2
3
6
9
20
25
2
3
6
9
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