D. Procedure
 S 862-014
 (1)  
Release the pressure from the pneumatic system (AMM 36-05-00/201).

 (2)  
Put a container below the vent to catch hydraulic fluid.

 S 492-015
 NOTE: Make sure the hydraulic fluid does not touch persons or
____
 the airplane.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-09-00
 ALL  ú ú 03A Page 204 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 862-027
 WARNING: PUT A RAG AROUND THE MANUAL DEPRESSURIZATION VALVES ON THE
_______ RESERVOIR PRESSURIZATION MODULE TO CATCH SPRAY OF HYDRAULIC FLUID. THE SPRAY OF HYDRAULIC FLUID CAN CAUSE INJURIES TO PERSONS. IF THE HYDRAULIC FLUID TOUCHES THE SKIN, FLUSH YOUR SKIN WITH WATER. IF THE HYDRAULIC FLUID TOUCHES YOUR EYES, FLUSH THE EYES WITH WATER AND GET MEDICAL AID.
 (3)  
Slowly open the depressurization (vent) valves to prevent a spray of hydraulic fluid.

 S 492-017

 (4)  
Install the lock on each depressurization (vent) valve when the valve is fully open.

 NOTE: To release the pressure from only one reservoir, put the
____ lock on the applicable depressurization (vent) valve. The pressure is removed from the reservoir when the air flow from the depressurization (vent) valve stops.
 E. Put the Airplane Back to Its Usual Condition
 S 092-018
 (1)  
Remove the lock(s) from the depressurization (vent) valve(s).

 (2)
Do the procedure above to pressurize the hydraulic reservoirs.

 S 862-019
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-09-00
 ALL  ú ú 02A Page 205 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM - ADJUSTMENT/TEST
___________________________________________________________
 1.  General
_______
 A.  This procedure gives you a leakage test of the pressurization system for the hydraulic reservoirs .
 TASK 29-09-00-795-074
 2.  Hydraulic Reservoir Pressurization System Test
______________________________________________
 A.  Special Tools and Equipment
 (1)  Applicable hydraulic caps and plugs
 B.  Standard Tools and Equipment
 (1)  Controlled source of clean, dry nitrogen, 0 to 70 psi
 C.  References
 (1)  
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System

 (2)  
AMM 29-15-00/201, Hydraulic Systems A, B and Standby

 D.  Access
 (1)  Location Zone
 216, 217 Main Wheel Well

 E.  Procedure
 S 845-075
 (1)  
Make sure the two engines and the APU are off.

 S 865-111

 (2)  
Release the pressure from the hydraulic reservoirs
 (AMM 29-09-00/201).

 S 615-077

 (3)  
Make sure the reservoirs for the hydraulic systems A and B are filled with hydraulic fluid (AMM 29-15-00/201).

 S 035-078

 (4)  
Remove the vents from the lines leading to the reservoir pressurization module from the right and left ECS ducts.

 NOTE: One vent is located at approximately RBL 25 on the forward
____ bulkhead. The other vent is located at approximately LBL 30 on the forward bulkhead.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-09-00
 ALL  ú ú 02 Page 501 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
　
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(47)