29-15-06
ALL ú ú 01 Page 402 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 024-008
(3)
Remove the screws that attach the ground fault detector to the structure.
S 024-009
(4)
Remove the ground fault detector.
TASK 29-15-06-404-010
3. Ground Fault Detector Installation___________________________________
A. Access
(1) Location Zones
102 Control Cabin, Right
B. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 29-15-22/501 Ground Fault Protection Test
C. Install Ground Fault Detector.(Fig. 401)
S 864-023
(1) Make sure that these circuit breakers are open:
(a)
For the hydraulic system A ground fault detector: 1) P6-2 Panel a) ELEC HYD PUMP CONT SYS A
2) P6-12 Panel a) ELEC HYD PUMP SYS A
(b)
For the hydraulic system B ground fault detector: 1) P6-2 Panel a) ELEC HYD PUMP CONT SYS B
2) P6-11 Panel a) ELEC HYD PUMP SYS B
S 414-011
(2)
Open P6-1 panel and P6-2 panel to access ground fault detector.
(3)
Put the ground fault detector in its position behind the P6-1 panel.
S 424-013
(4)
Install the screws that attach the ground fault detector to the structure.
(5)
Connect the electrical connector to the ground fault detector.
S 424-012
S 424-015
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A
737-300/400/500MAINTENANCE MANUAL
S 914-014
(6)
Make sure all tools, unwanted parts, and unwanted objects are removed from P6-1 panel.
S 414-016
(7)
Close P6-1 and P6-2 panels and secure.
D. Installation test.
S 864-024
(1) Do the ground fault detector test (AMM 29-15-22/501).
E. Put the Airplane Back to Its Usual Condition.
S 844-017
(1) If these circuit breakers are open, remove DO-NOT-CLOSE tags and close:
(a)
P6-1 Panel
1) ELEC HYD PUMP CONT SYS A
(b)
P6-2 Panel
1) ELEC HYD PUMP CONT SYS B
(c)
P6-11 Panel
1) ELEC HYD PUMP SYS B
(d)
P6-12 Panel
1) ELEC HYD PUMP SYS A
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-06
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1.
2.
3.
A
737-300/400/500MAINTENANCE MANUAL
GROUND SERVICE DISCONNECT FILTER - REMOVAL/INSTALLATION
_______________________________________________________General
_______
A. The ground service disconnect module (referred to as the module) is used to supply hydraulic power to the airplane from a hydraulic test stand. This procedure tells you how to replace the filter that is in the module.
B. If you get hydraulic fluid on the airplane, clean it off immediately (AMM 12-40-00/201).
TASK 29-15-08-004-001
Ground Service Disconnect Filter Removal (Fig. 401)
________________________________________
A. Consumable Materials
(1)
D00054 Skydrol Assembly Lube - MCS 352
(2)
D00153 Hydraulic Fluid - BMS 3-11
B. References
(1) AMM 12-40-00/201, Cleaning and Washing
C. Access
(1)
Location Zones
211 Left Ram Air Duct
213 Right Ram Air Duct
(2)
Access Panels
3302L Underwing Fairing Access Panel
3401R Underwing Fairing Access Panel
