-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
8. On the ground service panel of the Yellow hydraulic system:
-set the reservoir depressurizing valve to CLOSED.
9. Pressurize the reservoir to 50 psig.
5. Close-up
________ Subtask 29-34-00-860-052
-On the lower ECAM display:
-the message LO AIR PRESS comes on near the Yellow hydraulic system indication.
-The pressure in the resrvoir of theYellow hydraulic system increases to 50 psig.
-When the pressure increases to 25 psig, all of the warning given in step 7 are no longer shown
A. Put the aircraft back to the serviceable condition.
(1)
Disconnect the air supply from the reservoir air manifold.
(2)
Install the blanking cap on the air charging valve.
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
(4)
Close the main door of the main landing gear (Ref. TASK 32-12-00-410-001).
(5)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(6)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(7)
Remove the warning notice(s).
Subtask 29-34-00-410-052
B. Close Access
(1)
Close the access doors 197CB, 197EB, 197FB, 195BB, 196BB, 198CB. Subtask 29-34-00-865-055
C.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2701GJ, 3801GX, 3802GX.
R **ON A/C 001-049, 051-061, 101-105, 201-203,
TASK 29-34-00-710-002
R Operational Check of Reservoir Low Air Pressure Warning R
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G
Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-34-00Page 508 1 1 May 01/05 1 1 1CES 1
3. Job Set-up__________
Subtask 29-34-00-865-057
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU HYD/HYD PWR/B WARN/& CTL 49VU ANTI ICE/PROBES/AOA/1 49VU ANTI ICE/PROBES/PHC/1 49VU ANTI ICE/PROBES/PITOT/1 121VU RCDR/DFDR 121VU COM NAV/ATC/2 121VU EIS/FWC2/SPLY 122VU ANTI ICE/WHC/2 122VU ANTI ICE/WHC/1 122VU ANTI ICE/PROBES/PHC/3 122VU ANTI ICE/PROBES/2/TAT 122VU ANTI ICE/PROBES/2/PITOT 122VU ANTI ICE/PROBES/2/AOA 122VU ANTI ICE/PROBES/2/PHC 122VU ANTI ICE/PROBES/2/STATIC 122VU ANTI ICE/PROBES/3/PITOT 122VU ANTI ICE/PROBES/3/AOA 122VU ANTI ICE/PROBES/3/STATIC 122VU ANTI ICE/PROBES/1/STATIC 122VU ANTI ICE/PROBES/1/TAT 2702GJ 4DA1 2DA1 3DA1 7TU 5SH2 2WW 5DG2 5DG1 2DA3 1DA2 3DA2 4DA2 2DA2 5DA2 3DA3 4DA3 5DA3 5DA1 1DA1 C12D04D03D02K16K07Q07W13X13Y16Y15Y14Y13Y12Y11Z16Z15Z14Z13Z12
R **ON A/C 001-049, 052-061, 101-105, 201-203,
R 2000VU WASTE WIP-DRAINMAST-FWD 1DU B06
R **ON A/C 051-051,
R 2000VU WASTE WIP-DRAINMAST-FWD 1DU D02
R **ON A/C 001-049, 052-061, 101-105, 201-203,
R 2001VU WASTE WIP-DRAINMAST-AFT 11DU E01
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-34-00Page 509 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM HYDRAULIC POWER 液壓6(167)
