W DOC AIRBUS | TSM A320F

Overheat Indication of the Yellow Hydraulic System


TASK 29-13-00-810-802-A
Overheat Indication of the Yellow Hydraulic System


1. Possible Causes
  • CHECK VALVE Y [3083GM]
  • PACKAGE E-PUMP [3075GX]
  • internal leakage
  • RELIEF VALVE Y SYS [3063GM]
  • LP FILTER [3002GM]
  • HP FILTER Y [3048GM]
  • CHECK VALVE G [3022GM]
  • BRAKE RELIEF VALVE [3067GM]
  • SEL VALVE-CARGO DOORS ELEC/MAN CTL [2500MJ]
  • PUMP VARIABLE DTS [3084GM]
  • TEMP TRANSM SWITCH-connector plug (3381GR-A)
  • TEMP TRANSM SWITCH [3381GR]
  • SDAC-1 [1WV1]
  • SDAC-2 [1WV2]
  • 3705GD
  • PUMP VARIABLE DTS [3030GD]
  • FIRE-S.-O.V. [3046GD]
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
OHMMETER MODEL 260
 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 29-00-00-280-003
Check of the Internal Leakage of the Yellow Hydraulic System
AMM 29-00-00-910-003
General Removal and Installation Procedure of the Check Valves in the Hydraulic Systems
AMM 29-10-00-220-001
Functional Check to Monitor Internal Leak Rate of Yellow and Green Hydraulic Systems
AMM 29-13-00-710-002
Operational Test of the Yellow Hydraulic System
ASM 291301
AMM 29-13-14-000-001
Removal of the HP Manifold of the Yellow Hydraulic System
AMM 29-13-14-400-001
Installation of the HP Manifold of the Yellow Hydraulic System
AMM 29-13-32-000-001
Removal of the Pressure Relief Valve of the Yellow Hydraulic System
AMM 29-13-32-400-001
Installation of the Pressure Relief Valve of the Yellow Hydraulic System
AMM 29-13-43-610-040
Servicing of the Engine Pump Case-Drain Filter
AMM 29-13-43-610-802
Servicing of the Engine-Pump Case-Drain Filter
AMM 29-13-44-610-001
Servicing of the LP-Filter
AMM 29-13-45-610-001
Servicing of the HP-Filter
AMM 29-13-51-000-003
Removal of the Yellow Engine Pump
AMM 29-13-51-000-004
Removal of the Yellow Engine Pump
AMM 29-13-51-000-806
Removal of the Yellow Engine Driven Pump
AMM 29-13-51-100-801
Cleaning of the Engine Pump Solenoid-Valve
AMM 29-13-51-100-802
Cleaning of the Engine Pump Solenoid-Valve
AMM 29-13-51-100-804
Cleaning of the Engine Pump Solenoid-Valve
AMM 29-13-51-400-003
Installation of the Yellow Engine Pump
AMM 29-13-51-400-004
Installation of the Yellow Engine Pump
AMM 29-13-51-400-806
Installation of the Yellow Engine Driven Pump
AMM 29-24-00-863-001
Pressurize the Yellow Hydraulic System with the Electric Pump
AMM 29-24-00-864-001
Depressurize the Yellow Hydraulic System
AMM 29-24-21-000-001
Removal of the Yellow E-Pump Check Valve
AMM 29-24-21-400-001
Installation of the Yellow E-Pump Check Valve
ASM 293301
AMM 29-33-11-000-003
Removal of the Temperature Transmitter
AMM 29-33-11-400-003
Installation of the Temperature Transmitter
AMM 31-50-00-710-001
Ground Scanning of the Central Warning System
AMM 31-55-34-000-001
Removal of the SDAC
AMM 31-55-34-400-001
Installation of the SDAC
AMM 31-60-00-860-001
EIS Start Procedure
AMM 32-44-15-000-001
Removal of the Pressure Relief Valve
AMM 32-44-15-400-001
Installation of the Pressure Relief Valve
AMM 52-36-12-000-001
Removal of the Electro-Manual Selector Valve
AMM 52-36-12-400-001
Installation of the Electro-Manual Selector Valve
3. Fault Confirmation
Subtask 29-13-00-865-052-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUHYDRAULIC/Y HYD/PUMP ENG2/MONG3700GDQ37
Subtask 29-13-00-710-073-A
B. Fault Conformation
   (1) Do the Operational test of the Yellow hydraulic system AMM 29-13-00-710-002.
     (a) Do a check for unusual noise during the test at CHECK VALVE Y [3083GM] and PACKAGE E-PUMP [3075GX] .
     (b) If there is more noise than usual, go to Para 4.A.
Subtask 29-13-00-710-051-A
C. 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.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
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
AMM 24-41-00-861-002.
   (2) Pressurize the Yellow hydraulic system with the electric pump AMM 29-24-00-863-001.
   (3) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
   (4) Operate the sidestick for ailerons, spoilers and elevators at full travel for 5 min.
   (5) Operate the rudder pedals at full travel for 5 min.
   (6) Operate the flap and slat control lever at full travel for 5 min.
4. Fault Isolation
Subtask 29-13-00-810-078-A
A. If there is more noise than usual from CHECK VALVE Y [3083GM] or PACKAGE E-PUMP [3075GX] during the test:
   (1) Replace the CHECK VALVE Y [3083GM] AMM 29-24-21-000-001 and AMM 29-24-21-400-001.
NOTE: Failure of CHECK VALVE Y [3083GM] allows a reverse flow of fluid through the Yellow E-pump case drain back to the Yellow Reservoir resulting in possible mechanical damage to the Yellow E-pump.
   (2) Do the test in Para 3.C.
Subtask 29-13-00-810-054-A ** ON A/C NOT FOR ALL
B. If the test gives:
  • The message HYD Y RSVR OVHT on the upper ECAM DU
  • The PTU P/BSW FAULT light on panel 40VU
  • The YELLOW ENG 2 PUMP P/BSW FAULT light on panel 40VU
  • The OVHT flag on the HYD page of the lower ECAM DU.
NOTE: The fault warning system shows that the temperature is more than 95 +2.2 deg.C or -2.2 deg.C (203.00 +3.96 deg.F or -3.96 deg.F). The temperature (TEMP) transducers (XDCRs) and the thermal switch of the reservoir (RSVR) TEMP sensor FIN 3381GR sense this temperature.
   (1) Do a check of the internal leakage of the Yellow hydraulic system AMM 29-00-00-280-003 and the PTU AMM 29-10-00-220-001:
     (a) If the internal leakage is more than permitted:
       1 Examine the system to find the defective component.
       2 Replace or repair the detective component.
       3 Make sure that the manual selector valve of the forward and aft cargo door is not jammed in the OPEN or CLOSE position.
       4 Do a check for local increase of the temperature and unusual noise at the components that follow. Replace the components as necessary:
       5 Do a check of the CHECK VALVE Y [3083GM] as per para E (1) if:
  • A fault duplication occurs
  • The system is pressurized by a ground power cart
  • The system is pressurized by a Engine Driven Pump (EDP).
     (b) If the internal leakage is in the correct limits:
       1 Do a check of the filter elements of the PUMP VARIABLE DTS [3084GM] HP FILTER Y [3048GM] and LP FILTER [3002GM] .
       2 Replace the filter element as necessary AMM 29-13-43-610-040 or AMM 29-13-45-610-001 or AMM 29-13-44-610-001.
Subtask 29-13-00-810-054-D ** ON A/C NOT FOR ALL
B. If the test gives:
  • The message HYD Y RSVR OVHT on the upper ECAM DU
  • The PTU P/BSW FAULT light on panel 40VU
  • The YELLOW ENG 2 PUMP P/BSW FAULT light on panel 40VU
  • The OVHT flag on the HYD page of the lower ECAM DU.
NOTE: The fault warning system shows that the temperature is more than 100 +2.2 deg.C or -2.2 deg.C (212.00 +3.96 deg.F or -3.96 deg.F). The temperature (TEMP) transducers (XDCRs) and the thermal switch of the reservoir (RSVR) TEMP sensor FIN 3381GR sense this temperature.
   (1) Do a check of the internal leakage of the Yellow hydraulic system AMM 29-00-00-280-003 and the PTU AMM 29-10-00-220-001:
     (a) If the internal leakage is more than permitted:
       1 Examine the system to find the defective component.
       2 Replace or repair the detective component.
       3 Make sure that the manual selector valve of the forward and aft cargo door is not jammed in the OPEN or CLOSE position.
       4 Do a check for local increase of the temperature and unusual noise at the components that follow. Replace the components as necessary:
       5 Do a check of the CHECK VALVE Y [3083GM] as per para E (1) if:
  • A fault duplication occurs
  • The system is pressurized by a ground power cart
  • The system is pressurized by a Engine Driven Pump (EDP).
     (b) If the internal leakage is in the correct limits:
       1 Do a check of the filter elements of the PUMP VARIABLE DTS [3084GM] HP FILTER Y [3048GM] and LP FILTER [3002GM] .
       2 Replace the filter element as necessary AMM 29-13-43-610-802 or AMM 29-13-45-610-001 or AMM 29-13-44-610-001.
Subtask 29-13-00-810-073-A
C. If the test gives:
  • The message HYD Y RSVR OVHT on the upper ECAM DU
  • The OVHT flag on the HYD page of the lower ECAM DU.
NOTE: If the P/BSW FAULT lights are not on, this confirms that the OVHT warning condition is only detected by the TEMP XDCRs of the RSVR TEMP sensor FIN 3381GR. It is referred to as a spurious warning from the TEMP XDCRs or wiring or System Data Acquisition Concentrators (SDACs).
   (1) Do a wiring check:
     (a) Disconnect the TEMP TRANSM SWITCH-connector plug (3381GR-A) from the TEMP TRANSM SWITCH [3381GR] and do a visual check of the connector's integrity.
       1 If the connector is not in the correct condition:
     (b) Do a check of the continuity between pin A/G and pin A/K of the TEMP TRANSM SWITCH [3381GR] ASM 293301.
       1 If there is no continuity, replace the TEMP TRANSM SWITCH [3381GR] AMM 29-33-11-000-003 AMM 29-33-11-400-003.
     (c) Do a check of the continuity between pin A/F and pin A/E of the TEMP TRANSM SWITCH [3381GR] ASM 293301.
       1 If there is no continuity, replace the TEMP TRANSM SWITCH [3381GR] AMM 29-33-11-000-003 AMM 29-33-11-400-003.
     (d) Measure the DC resistance between the pins A/G and A/K and between the pins A/E and A/F of the TEMP TRANSM SWITCH [3381GR] with an OHMMETER MODEL 260.
       1 If the difference is more than 1.5 Ohm between the two measurements, replace the TEMP TRANSM SWITCH [3381GR] AMM 29-33-11-000-003 AMM 29-33-11-400-003.
     (e) If the fault continues, make sure that the wiring is not connected to GND between the TEMP TRANSM SWITCH-connector plug (3381GR-A), pin E and the SDAC-1 [1WV1] connector AE, pin 12J ASM 293301.
       1 If the wiring is connected to GND, repair the wiring as necessary.
     (f) If the fault continues, make sure that the wiring is not connected to GND between the TEMP TRANSM SWITCH-connector plug (3381GR-A), pin K and the SDAC-2 [1WV2] connector AE, pin 12J ASM 293301.
       1 If the wiring is connected to GND, repair the wiring as necessary.
     (g) If the fault continues, do the operational test of the central warning system AMM 31-50-00-710-001.
       1 If the test gives the maintenance message SDAC1 : Y HYD TEMP XMTR 3381GR:
       2 If the test gives the maintenance message SDAC2 : Y HYD TEMP XMTR 3381GR:
Subtask 29-13-00-810-074-A
D. If the test gives:
  • The message HYD Y RSVR OVHT on the upper ECAM DU
  • The PTU P/BSW FAULT light on panel 40VU
  • The YELLOW ENG 2 PUMP P/BSW FAULT light on panel 40VU.
NOTE: If the OVHT flag is not shown on the HYD page of the lower ECAM DU, this confirms that the OVHT warning condition is only detected by the thermal switch of the RSVR TEMP sensor FIN 3381GR. It is referred to as a spurious warning from the thermal switch or wiring or SDACs.
   (1) Do a wiring check:
     (a) Do a check of the continuity between pin A/A and pin A/B of the TEMP TRANSM SWITCH [3381GR] ASM 293301.
       1 If there is continuity, replace the TEMP TRANSM SWITCH [3381GR] AMM 29-33-11-000-003 AMM 29-33-11-400-003.
       2 If there is no continuity, make sure that the wiring is not connected to GND between the TEMP TRANSM SWITCH-connector plug (3381GR-A), pin B and the 3705GD pin Z ASM 293301 and ASM 291301.
         a If the wiring is connected to GND, repair the wiring as necessary.
     (b) If the fault continues, make sure that the wiring is not connected to GND between the TEMP TRANSM SWITCH-connector plug (3381GR-A), pin B and the SDAC-1 [1WV1] connector AD, pin 4G ASM 293301.
       1 If the wiring is connected to GND, repair the wiring as necessary.
     (c) If the fault continues, make sure that the wiring is not connected to GND between the TEMP TRANSM SWITCH-connector plug (3381GR-A), pin B and the SDAC-2 [1WV2] connector AD, pin 4G ASM 293301.
       1 If the wiring is connected to GND, repair the wiring as necessary.
     (d) If the fault continues, do the operational test of the central warning system AMM 31-50-00-710-001.
       1 If the test gives the maintenance message SDAC1 : Y HYD TEMP XMTR 3381GR:
       2 If the test gives the maintenance message SDAC2 : Y HYD TEMP XMTR 3381GR:
Subtask 29-13-00-810-065-A ** ON A/C NOT FOR ALL
E. If the test gives:
  • No message on the upper and lower ECAM DUs
  • No FAULT lights illumination.
NOTE: No OVHT warning is found, when the Yellow hydraulic system is pressurized with the Yellow Electric Motor Pump (Y EMP).
   (1) Remove the CHECK VALVE Y [3083GM] AMM 29-24-21-000-001.
     (a) Do a visual inspection of the CHECK VALVE Y [3083GM] for damage and missing parts.
       1 If parts are missing, do the steps that follow before you install the new CHECK VALVE Y:
   (2) Install the CHECK VALVE Y [3083GM] AMM 29-24-21-400-001.
   (3) If the fault continues:
     (a) Clean the Solenoid Valve of the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-100-801.
     (b) Do the test given in Para. 3.
   (4) If the fault continues:
     (a) Replace the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-000-003 and AMM 29-13-51-400-003.
Subtask 29-13-00-810-065-B ** ON A/C NOT FOR ALL
E. If the test gives:
  • No message on the upper and lower ECAM DUs
  • No FAULT lights illumination.

NOTE: No OVHT warning is found, when the Yellow hydraulic system is pressurized with the Yellow Electric Motor Pump (Y EMP).
   (1) Remove the CHECK VALVE Y [3083GM] AMM 29-24-21-000-001.
     (a) Do a visual inspection of the CHECK VALVE Y [3083GM] for damage and missing parts.
       1 If parts are missing, do the steps that follow before you install the new CHECK VALVE Y:
   (2) Install the CHECK VALVE Y [3083GM] AMM 29-24-21-400-001.
   (3) If the fault continues:
     (a) Clean the Solenoid Valve of the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-100-802.
     (b) Do the test given in Para. 3.
   (4) If the fault continues:
     (a) Replace the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-000-004 and AMM 29-13-51-400-004.
Subtask 29-13-00-810-065-D ** ON A/C NOT FOR ALL
E. If the test gives:
  • No message on the upper and lower ECAM DUs
  • No FAULT lights illumination.
NOTE: No OVHT warning is found, when the Yellow hydraulic system is pressurized with the Yellow Electric Motor Pump (Y EMP).
   (1) Remove the CHECK VALVE Y [3083GM] AMM 29-24-21-000-001.
     (a) Do a visual inspection of the CHECK VALVE Y [3083GM] for damage and missing parts.
       1 If parts are missing, do the steps that follow before you install the new CHECK VALVE Y:
   (2) Install the CHECK VALVE Y [3083GM] AMM 29-24-21-400-001.
   (3) If the fault continues:
     (a) Clean the Solenoid Valve of the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-100-804.
     (b) Do the test given in Para. 3.
   (4) If the fault continues:
     (a) Replace the PUMP VARIABLE DTS [3030GD] AMM 29-13-51-000-806 and AMM 29-13-51-400-806.
Subtask 29-13-00-710-055-A
F. When the FIRE-S.-O.V. [3046GD] was not the cause of the malfunction:
  • Do the test as given in Para. 3. C. to make sure that operation is correct (no message shown).
5. Close-up
Subtask 29-13-00-860-052-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the Yellow hydraulic system is de-pressurrized AMM 29-24-00-864-001.
   (2) Make sure that the aircraft electrical circuits are de-energized AMM 24-41-00-862-002.
[Rev.8 from Aug 2018] 2026.04.04 04:29:25 UTC