S 864-036
(24)
Make sure the flap control lever is in the ten unit position.
S 864-037
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. THE AILERONS, RUDDERS, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(25)
Supply hydraulic power with the applicable EMDP (AMM 29-15-00/201).
S 794-038
(26)
Make sure the hydraulic connections for the heat exchanger at the rear spar do not have leaks of hydraulic fluid.
(27)
Put the flap handle in the FLAP UP position.
S 864-039
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-04
ALL ú ú 02 Page 407 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 864-040
(28)
Remove hydraulic power (AMM 29-15-00/201).
S 614-041
(29)
Fill the applicable hydraulic reservoir (AMM 12-12-00/301).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-04
ALL ú ú 01 Page 408 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
PANEL, P6-1 CIRCUIT BREAKER
SEE B
P6 PANEL PANEL P6-2
SEE A
FLIGHT COMPARTMENT
(VIEW IN THE AFT DIRECTION)
A
SCREW
(4 LOCATIONS)
ELECTRICAL
CONNECTOR
GROUND
FAULT
DETECTOR
GROUND FAULT DETECTORS, M1106/M1105
B
Ground Fault Detector Installation Figure 401
K05905
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-06
ALL ú ú 01 Page 401 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
GROUND FAULT DETECTOR- REMOVAL/INSTALLATION
___________________________________________
1. General
________
A. This procedure has these tasks:
(1)
Ground Fault Detector Removal
(2)
Ground Fault Detector Installation
B. There are two ground fault detectors. The ground fault detectors for hydraulic systems A and B Electric Motor Driven Pump (EDMP) relay circuits are installed behind the P6-1 cicuit breaker panel located in the flight compartment.
C. The removal and installation instructions are the same for each of the ground fault detectors.
TASK 29-15-06-004-001
2. Ground Fault Detector Removal
______________________________
A. Access
(1) Location Zones
102 Control Cabin, Right
B. Prepare for the Removal.
S 014-002
(1) For the hydraulic system A ground fault detector, do these steps:
(a) Open these circuit breakers and attach the DO-NOT-CLOSE tag: 1) On the load control center panel, P6-1 a) ELEC HYD PUMP CONT SYS A
2) P6-12 Panel a) ELEC HYD PUMP SYS A
S 014-004
(2) For the hydraulic system B ground fault detectors, do these steps:
(a) Open these circuit breakers and attach the DO-NOT-CLOSE tag: 1) P6-2 Panel a) ELEC HYD PUMP CONT SYS B
2) P6-11 Panel a) ELEC HYD PUMP SYS B
C. Ground Fault Detector Removal.(Fig. 401)
S 014-006
(1)
Open the P6-1 and the P6-2 panel to gain access to the ground fault detector.
(2)
Disconnect the electrical connector from the ground fault detector.
S 024-007
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 液壓 HYDRAULIC POWER(86)
