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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A
757
MAINTENANCE MANUAL
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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A
757 MAINTENANCE MANUAL
(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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本文鏈接地址：757 AMM 飛機維護手冊 液壓 CHAPTER 29 - HYDRAULIC POWER 2(27)
