R R R  (8) Connect the suction and delivery lines of the hydraulic ground power-supply to the aircraft connectors: - 2006GM suction - 2008GM delivery. 
R  (9) Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).
 4. Procedure_________
 Subtask 29-10-00-863-052
 A. Pressurization of the Blue Hydraulic System with a Hydraulic Ground Power Supply
 (1) Start the hydraulic ground power supply and pressurize the Blue hydraulic system to 3000 psi (206 bar).
 (2) Refer to the ECAM indication of the BLUE system pressure and make sure it shows 3000 psi.
 5. Close-up________
 Subtask 29-10-00-860-082
 A. Put the aircraft back to the serviceable condition. 
R  (1) Stop the hydraulic ground power-supply.
 (2) Refer to the ECAM indication of the BLUE system pressure and make sure that it shows 0 psi.
 (3) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
 (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 (5) Disconnect the suction and delivery lines from the aircraft connectors. 
R R R  (6) Make sure that the fluid level in the reservoir of the Blue hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002). 
R R  (7) If necessary, pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).

 Subtask 29-10-00-410-052
 B. Close the access door 197EB.
 1EFF : ALL 1 29-10-00Page 231 1 1 May 01/05R 1 1 1CES 1

 TASK 29-10-00-863-003- 01
 Pressurize the Blue Hydraulic System with the Blue Electric Pump
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
 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 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 1EFF : ALL 1 29-10-00Page 232 1 1 May 01/05R 1 1 1CES 1

 3. Job Set-up
__________ Subtask 29-10-00-865-082
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12 123VU B HYD/ELEC PUMP 2701GJ AB09
 Subtask 29-10-00-860-099
 B. 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, push the HYD pushbutton switch (P/BSW). Make sure that the lower (system) display shows the HYD page.

 (4)
 Make sure that the ECAM does not show any of these warnings:

 -
low air pressure in the Blue reservoir,

 -
low fluid level in the Blue reservoir.

 (5)
 If necessary, pressurize the reservoir (Ref. TASK 29-14-00-614-002).

 (6)
 If necessary, add fluid to the reservoir (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).

 4. Procedure
_________ Subtask 29-10-00-863-053
 A. Pressurization of the Blue Hydraulic System with the Electric Pump
 (1)
 On section 40VU of the overhead panel, make sure that the BLUE ELEC PUMP pushbutton switch is set to ON (OFF and FAULT legends are out).
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM HYDRAULIC POWER 液壓1(98)