INDICATING - DESCRIPTION AND OPERATION
______________________________________
 1. General_______
 The three hydraulic systems have sensors which monitor the condition of the systems. The sensors monitor
 -
the contents of the reservoirs (Ref. 29-31-00)

 -
the system pressure (Ref. 29-32-00)

 -
the output pressure of the pumps (not the electric pump of the Yellow system) (Ref. 29-32-00)

 -
the temperature of the hydraulic fluid (Ref. 29-33-00)

 -
the internal pressure of the reservoir (Ref. 29-34-00)

 The information from the sensors is sent to the flight compartment and used for
 -FAULT warnings on the overhead panel
 -audio warnings
 -MASTER CAUTION and MASTER WARNING lights
 -electronic centralized aircraft monitor (ECAM) displays (system and
 engine/warning displays).

 INDICATING - DEACTIVATION/REACTIVATION
______________________________________

R **ON A/C 001-049, 051-061, 101-105, 201-203,
 TASK 29-30-00-040-001
 Deactivation of RAT Fault Warning on the ECAM Upper Display Unit
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 29-30-04-H)
 Indicating - Warning and Caution on ECAM
 RAT FAULT

 NOTE : Use this procedure together with the Master Minimum Equipment List
____ (MMEL). If the fault indication is because of a defect in the indication system it is permitted to dispatch the aircraft. It is also permitted to dispatch the aircraft if the defect is in the RAT ground test system (if the system is known to be in the "flight" condition). It is not permitted to dispatch the aircraft if the fault indication is because of a defect which could prevent operation of the RAT.
 NOTE : If any part of the system is deactivated, the aircraft can be
____ dispatched for one flight only. After that flight, the deactivated component must be reactivated and this procedure done again. This is to find any faults which were not shown because of the deactivation.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific tie-wrap 98D29207542000 1 SAFETY DEVICE - RAT 98D29207550001 1 PROTECTION EQUIPMENT - RAT

 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-22-00-860-001 Installation of the Safety Device of the Ram Air
 Turbine 29-22-00-860-002 Removal of the Safety Device of the Ram Air Turbine 29-22-00-869-002 Retraction of the Ram Air Turbine (RAT) on the Ground 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 29-30-00-991-002 Fig. 401 29-30-00-991-003 Fig. 402
 3. Job Set-up
__________
 Subtask 29-30-00-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 On the ECAM control panel on the center pedestal, press the HYD pushbutton switch (P/BSW). Make sure that the ECAM lower Display Unit (DU) shows the HYD page.

 (4)
 Make sure that the ECAM upper DU shows the RAT FAULT indication.

R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-30-00Page 402 1 1 May 01/05 1 1 1CES 1

 4. Procedure_________
 (Ref. Fig. 401/TASK 29-30-00-991-002, 402/TASK 29-30-00-991-003)
 Subtask 29-30-00-040-050
 A. Deactivation of the RAT Fault Warning
 (1) Do a visual check of the left belly fairing to find if the RAT is extended. If the RAT is extended, there is a fault (unwanted extension of the RAT) which you must repair before you can dispatch the aircraft.
 NOTE : If the RAT is not extended, continue with the subsequent____ procedure.
 (2) Open the access panels 195BB and 197EB.
 (3) If it is available, install the SAFETY DEVICE - RAT (98D29207542000) on the RAT (Ref. TASK 29-22-00-860-001).
　
中國航空網(wǎng) 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(110)