12.
PACKING
22.
BOLT
23.
WASHER
13. PRESSURE LINE
(16 LOCATIONS)
14. BOLT
21. MOUNTING PLATE 15. WASHER
19. NUT (2 LOCATIONS)
20. WASHER (2) 16. BONDING JUMPER
18. VIBRATION ISOLATOR 17. BONDING
(4 LOCATIONS) JUMPER
FWD 1 AIRPLANES WITH A TWO-PIECE
ALTERNATING CURRENT MOTOR PUMP (ACMP) BONDING JUMPER 2 AIRPLANES WITH A ONE-PIECE
B1
BONDING JUMPER
Alternating Current Motor Pump (ACMP) Installation for the Left and Right Systems Figure 401 (Sheet 1)
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MAINTENANCE MANUAL
1. ELECTRICAL CONNECTOR
2. ELECTRICAL
CONNECTOR
3. ELBOW
4.
UNION
5.
PACKING
28. PUMP
6.
SUPPLY HOSE
7.
SELF-SEAL
COUPLER
26.
NUT
27.
WASHER
8.
REDUCER
(3 LOCATIONS)
9.
PACKING
24. BOLT
10. CASE DRAIN LINE
25. WASHER (4 LOCATIONS)
13. PRESSURE LINE
22.
BOLT
23.
WASHER (16 LOCATIONS)
21. MOUNTING PLATE
11.
REDUCER 19. NUT
12.
PACKING 20. WASHER (2)
17. BONDING JUMPER
18. VIBRATION ISOLATOR (4 LOCATIONS)
ALTERNATING CURRENT MOTOR PUMP (ACMP) C2
Alternating Current Motor Pump (ACMP) Installation for the Left and Right Systems
Figure 401 (Sheet 2)
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MAINTENANCE MANUAL
(3) S 864-004Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags: (a) 11K16, HYDRAULICS ELEC PUMP RIGHT (b) 11K25, HYDRAULICS ELEC PUMP LEFT
(4) S 864-005Remove the pressure from the applicable hydraulic system and the reservoir (AMM 29-11-00/201).
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本文链接地址：757 AMM 飞机维护手册 液压 CHAPTER 29 - HYDRAULIC POWER 1(174)
