ON ON
w w 
PRESS 
PRESS 
a 
a FLIGHT COMPARTMENT 
OVHT OVHT 
a a 
5. CONNECTOR 
HYDRAULIC CONTROL PANEL A 
4. CONNECTOR 
2. MODULE 
3. CONNECTOR 
FWD 
MODULE CONNECTORS B 
Hydraulic Control Panel, M10050 Figure 401 
H05880
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 S 034-006
 (5)  
Disconnect the electrical connectors (3), (4), and (5).
S 024-007
 (6)  
Remove the M10050 Hydraulic Control Module (2).
S 024-008
 (7)  
Install protective caps on the electrical connectors (3), (4), and
 (5) and on the module (2) to pevent damage or contamination.
 TASK 29-11-40-404-009
 3. Install the Hydraulic Control Module (Fig. 401)
____________________________________
 A. References
 (1)  AMM 24-22-00/201, Electrical Power - Control
 B. Access
 (1)  Location Zones
 211/212 Cabin Control
 C. Procedure
 S 434-010
 (1)  
Remove the protective caps from the electrical connectors (3), (4), (5), and the module (2).
S 434-011
 (2)  
Reconnect the electrical connectors (3, (4) and (5).
S 424-012
 (3)  
Put the Hydraulic Control Module (2) into the Pilot's overhead panel, P5.
S 414-013
 (4)  
Tighten the four quarter-turn fasteners (1) which hold the module
 (2) to the Pilot's overhead panel, P5.
 S 214-014
 (5)  
Make sure all the switches on the Hydraulic Control Module (2) are in the OFF position.
 (6)  
Supply Electrical Power (AMM 24-22-00/201).
S 864-016
 (7)  
Close these circuit breakers on the overhead panel, P11:
 S 864-015
 (a)  11K14, HYDRAULIC L ENGINE PUMP DEPRESS
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 (b) 
11K15, HYDRAULIC ELEC PUMP C1
 (c) 
11K16, HYDRAULIC R ELEC PUMP
 (d) 
11K17, HYD SYS PRESS L
 (e) 
11K18, HYD SYS PRESS C
 (f) 
11K23, HYDRAULIC R ENGINE PUMP DEPRESS
 (g) 
11K24, HYDRALIC ELEC PUMP C2
 (h) 
11K25, HYDRAULIC ELEC PUMP L
 (i) 
11K26, HYD SYS PRESS R
 S 714-017
 (8) Do an operational test on the following (AMM 29-11-00/501):
 (a) 
L EDP HYD PUMP
 (b) 
C1 ACMP ELEC PUMP
 (c) 
R ACMP ELEC PUMP
 (d) 
C HYD SYS PRESS
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