Google+
Facebook
LinkedIn
Twitter
Digg
StumbleUpon
Home
Download PDF
Order CD-ROM
Order in Print
SECTION VII. CRUISE - TM-1-1520-240-10_473
EAPS Penalty Table (Continued) - TM-1-1520-240-10_475
TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
Page Navigation
455
456
457
458
459
460
461
462
463
464
465
TM 1-1520-240-10
7A-7-2
Table 7A-7-1. EAPS Penalty Table
Increase Total
Fuel Flow By
Decrease
Torque
Available (%)
Pressure
Altitude (ft)
OAT
(
_
C)
(lb/hr)
KTAS = 0
85
135
160
Seal Level
-50
40
0
0
0
0
-40
40
0
0
0
0
-30
40
0
0
0
0
-20
40
0
0
0
0
-10
40
0
0
0
0
0
40
0
0
0
0
10
40
0
0
0
0
20
40
0
0
3
5
30
40
2
3
6
8
40
40
2
3
6
8
50
40
2
3
6
8
2000
-50
40
0
0
0
0
-40
40
0
0
0
0
-30
40
0
0
0
0
-20
40
0
0
0
0
-10
40
0
0
0
0
0
40
0
0
0
0
10
40
0
0
3
5
20
40
2
3
6
9
30
40
2
3
6
8
40
40
2
3
6
8
50
40
2
3
6
8
4000
-50
40
0
0
0
0
-40
40
0
0
0
0
-30
40
0
0
0
0
-20
40
0
0
0
0
-10
40
0
0
0
0
0
40
0
0
0
0
10
40
2
3
6
9
20
40
2
3
6
9
30
40
2
3
6
8
40
40
2
3
6
8
50
40
2
3
6
8
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business