A. Put the aircraft back to the serviceable condition.
(1)
On the overhead panel 50VU, push the B/LEAK MEASUREMENT VALVES P/BSW. Make sure that the OFF light goes out.
(2)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
002).
TASK 29-32-00-710-003
Operational Test of the System Pressure Switch (3151GN), Pressure Transmitter (3065GN) and the associated Indicating System of the Yellow Hydraulic System WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump
12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic
Service Cart
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
29-00-00-910-002 Safety Procedures of the Hydraulic System
29-10-00-863-002 Pressurize the Yellow Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector
29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-23-00-860-002 Connection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-23-00-863-002 Pressurize the Yellow Hydraulic System from the Green
Hydraulic System through the PTU with the Ground
Service Cart
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU
29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________
Subtask 29-32-00-865-052
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD/PRESS/XMTR 1841GN C11 121VU HYDRAULIC/SOL VALVES/G/Y/B/LEAK/TST 1881GP N35
Subtask 29-32-00-860-055
B. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1) Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
NOTE : This procedure pressurizes the Green hydraulic system together
____ with the Yellow hydraulic system. If you do not want to pressurize the Green system, you must disconnect the PTU isolation coupling.
(2)
If required, disconnect the PTU isolation coupling (Ref. TASK 29-23-00-860-001).
(3)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(4)
On the overhead panel 50VU, make sure that the HYD /LEAK MEASUREMENT VALVES/B pushbutton switch (P/BSW) is set to on (OFF light is not on).
(5)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(6)
On the ECAM control panel on the center pedestal, press the HYD pushbutton. Make sure that the ECAM lower display unit (DU) shows the HYD page.
(7)
Make sure that the ECAM shows none of these conditions:
-
Yellow reservoir low air pressure,
-
Yellow reservoir low fluid contents.
(8)
In addition, if you have not isolated the PTU, make sure that the ECAM does not show:
-
low air pressure in the reservoir of the Green hydraulic system,
-
low fluid contents in the reservoir of the Green hydraulic system.
(9)
If necessary, pressurize the reservoir(s) (Ref. TASK 29-14-00-614-002).
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本文鏈接地址：A320飛機維護手冊 AMM HYDRAULIC POWER 液壓6(134)
