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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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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 (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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