Failure of the Hydraulic Pressurizing Valve on Engine 2
TASK 78-31-00-810-802-A
Failure of the Hydraulic Pressurizing Valve on Engine 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 78-31-00-710-052-A ** ON A/C NOT FOR ALL
Subtask 78-31-00-810-118-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:37:58 UTC
Failure of the Hydraulic Pressurizing Valve on Engine 2
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 73-21-60-000-001 | Removal of the Electronic Control Unit (ECU) |
| AMM 73-21-60-400-001 | Installation of the Electronic Control Unit (ECU) |
| AMM 78-31-00-710-040 | Operational Test of the Thrust Reverser System |
| AMM 78-31-00-710-042 | Operational Test of the Thrust Reverser System |
| AMM 78-31-16-000-040 | Removal of the Hydraulic Control Unit Pressure Switch |
| AMM 78-31-16-000-041 | Removal of the Hydraulic Control Unit Pressure Switch |
| AMM 78-31-16-400-040 | Installation of the Hydraulic Control Unit Pressure Switch |
| AMM 78-31-16-400-041 | Installation of the Hydraulic Control Unit Pressure Switch |
| AMM 78-31-51-000-040 | Removal of the Hydraulic Control Unit |
| AMM 78-31-51-000-042 | Removal of the Hydraulic Control Unit |
| AMM 78-31-51-400-040 | Installation of the Hydraulic Control Unit |
| AMM 78-31-51-400-042 | Installation of the Hydraulic Control Unit |
Subtask 78-31-00-710-052-A ** ON A/C NOT FOR ALL
A. Test
(1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser system (2A) (MENU mode test) AMM 78-31-00-710-040. Make sure that the hydraulic pressure is correct during the test. The pressure must not drop below the advisory threshold.
Subtask 78-31-00-710-052-C ** ON A/C NOT FOR ALL (1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser system (2A) (MENU mode test) AMM 78-31-00-710-040. Make sure that the hydraulic pressure is correct during the test. The pressure must not drop below the advisory threshold.
NOTE: If the test gives the maintenance message HCU (TRPV), HYD, do the test again with a hydraulic ground cart or do the operational test of the thrust reverser without CFDS with engine running AMM 78-31-00-710-040.
If you do the test with an engine ground run, enter a new flight number in the FMGC menu via the MCDU keypad to get a Post Flight Report (PFR) after the test.
If warning ENG 2 REVERSER FAULT and maintenance message HCU (TRPV), HYD are shown during the test, do the following trouble shooting. If they are not shown during the test or are not recorded in the Post Flight Report (PFR) after the ground run, no further action is required.
If you do the test with an engine ground run, enter a new flight number in the FMGC menu via the MCDU keypad to get a Post Flight Report (PFR) after the test.
If warning ENG 2 REVERSER FAULT and maintenance message HCU (TRPV), HYD are shown during the test, do the following trouble shooting. If they are not shown during the test or are not recorded in the Post Flight Report (PFR) after the ground run, no further action is required.
A. Test
(1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser system (2A) (MENU mode test) AMM 78-31-00-710-042. Make sure that the hydraulic pressure is correct during the test. The pressure must not drop below the advisory threshold.
Subtask 78-31-00-710-052-D ** ON A/C NOT FOR ALL (1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser system (2A) (MENU mode test) AMM 78-31-00-710-042. Make sure that the hydraulic pressure is correct during the test. The pressure must not drop below the advisory threshold.
A. Test
(1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser without CFDS with engine running AMM 78-31-00-710-040.
4. Fault Isolation(1) Make sure that the thrust reverser system is not mechanically deactivated (Inhibition pin on HCU).
(2) Do the operational test of the thrust reverser without CFDS with engine running AMM 78-31-00-710-040.
NOTE: Enter a new flight number in the FMGC menu via the MCDU keypad to get a Post Flight Report (PFR) after the test. If warning ENG 1 REVERSER FAULT and maintenance message HCU (TRPV), HYD are shown during the test, do the following trouble shooting. If they are not shown during the test or are not recorded in the Post Flight Report (PFR) after the ground run, no further action is required.
Subtask 78-31-00-810-118-A ** ON A/C NOT FOR ALL
A. The fault message is generated if a position fault is detected on the HCU pressurizing valve (valve detected not open when reverse is commanded). The HCU pressurizing valve position monitoring is based upon the output signal of the HCU pressure switch (4102KS):
Subtask 78-31-00-810-118-B ** ON A/C NOT FOR ALL - if the switch is closed, there is no pressure,
- if the switch is open, the valve is pressurized.
- no further action is required.
- do the trouble shooting as if the maintenance message was confirmed on test.
- replace the
HCU-THRUST REV (4101KS) AMM 78-31-51-000-040 and AMM 78-31-51-400-040.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
- replace the PRESS SW-HCU [4102KS] AMM 78-31-16-000-040 and AMM 78-31-16-400-040.
- replace the HCU-THRUST REV (4101KS) AMM 78-31-51-000-040 and AMM 78-31-51-400-040.
- replace the ECU (4000KS) AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
A. The fault message is generated if a position fault is detected on the HCU pressurizing valve (valve detected not open when reverse is commanded). The HCU pressurizing valve position monitoring is based upon the output signal of the HCU pressure switch (4102KS):
Subtask 78-31-00-710-053-A ** ON A/C NOT FOR ALL - if the switch is closed, there is no pressure,
- if the switch is open, the valve is pressurized.
- no further action is required.
- do the trouble shooting as if the maintenance message was confirmed on test.
- replace the
HCU-THRUST REV (4101KS) AMM 78-31-51-000-042 and AMM 78-31-51-400-042.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
- replace the PRESS SW-HCU [4102KS] AMM 78-31-16-000-041 and AMM 78-31-16-400-041.
- replace the HCU-THRUST REV (4101KS) AMM 78-31-51-000-042 and AMM 78-31-51-400-042.
- replace the ECU (4000KS) AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
B. Do the test given in Para. 3.A.