「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 205
Aug 01/01 CES
TASK 29-11-00-810-802
Overheat Indication of the Green Hydraulic System
1. Possible Causes
_______________
- XMTR-TEMP, G RSVR (1381GR)
- DRAIN-HYDRAULIC FILTER CASE ASSEMBLY (1084GM)
- FILTER-HP, G (1048GM)
- FILTER-LP, G (1002GM)
- SDAC-1 (1WV1)
- SDAC-2 (1WV2)
- VALVE-G PUMP FIRE, ENG 1 (1046GK)
- internal leakage
- wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific temperature sensor
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power AMM 29-00-00-280-001 Check of the Internal Leakage of the Green Hydraulic
System R AMM 29-00-00-280-004 Check of the Internal Leakage of the Power Transfer R Unit (PTU)
AMM 29-00-00-280-006 Check of the Green or Yellow Hydraulic System after Operation in a Possible Cavitation Condition of the Engine Pump
R AMM 29-10-00-710-001 Operational Check of Hydraulic Fire Shut Off Valves R and Associated Indicating System AMM 29-11-43-610-040 Servicing of the Engine-Pump Case-Drain Filter
(1084GM) AMM 29-11-44-610-001 Servicing of the LP-Filter (1002GM) AMM 29-11-45-610-001 Servicing of the HP-Filter 1048GM AMM 29-11-52-000-001 Removal of the Engine Pump Fire-Valve (1046GK) AMM 29-11-52-400-001 Installation of the Engine Pump Fire-Valve (1046GK)
R
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 206
Aug 01/04 CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 29-33-11-000-001 Removal of the Temperature Transmitter (1381GR)
AMM 29-33-11-400-001 Installation of the Temperature Transmitter (1381GR)
AMM 31-50-00-710-001 Ground Scanning of the Central Warning System
AMM 31-55-34-000-001 Removal of the SDAC (1WV1,1WV2)
AMM 31-55-34-400-001 Installation of the SDAC (1WV1,1WV2)
AMM 31-60-00-860-001 EIS Start Procedure
R AMM 71-00-00-710-003 Engine Automatic Start R AMM 71-00-00-710-028 Engine Shutdown ASM 29-33/01
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
B. Test
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002). R
R (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
R (3) Do an Engine Automatic Start to pressurize the Green hydraulic system R (Ref. AMM TASK 71-00-00-710-003).
(4) Operate the sidestick for ailerons, spoilers and elevators at full travel for 5 min.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 液壓(18)
