Read CFDS for APU CLASS 3 Fault(s) of APU OIL DIFF PRESSURE SWITCH (P9) and GENERATOR SCAV DIFFERENTIAL PRESSURE SWITCH (P5) (131-9(A))
TASK 49-91-00-740-001-A
Read CFDS for APU CLASS 3 Fault(s) of APU OIL DIFF PRESSURE SWITCH (P9) and GENERATOR SCAV DIFFERENTIAL PRESSURE SWITCH (P5) (131-9(A))
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 49-91-00-860-052-A ** ON A/C NOT FOR ALL
Subtask 49-91-00-740-050-A ** ON A/C NOT FOR ALL
Subtask 49-91-00-860-053-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:33:02 UTC
Read CFDS for APU CLASS 3 Fault(s) of APU OIL DIFF PRESSURE SWITCH (P9) and GENERATOR SCAV DIFFERENTIAL PRESSURE SWITCH (P5) (131-9(A))
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TSM 49-90-00-810-812 | Lube Pump Filter SW P9/GEN SCAV Filter SW P5 Fault (131-9(A)) |
Subtask 49-91-00-860-052-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
(2) On the overhead panel, push the APU MASTER/SW to the ON position.
Subtask 49-91-00-865-054-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
(2) On the overhead panel, push the APU MASTER/SW to the ON position.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/MCDU/1 | 11CA1 | B01 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/MCDU/1 | 11CA1 | H07 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | PTR/SPLY | 6TW | J21 |
| 121VU | CFDS/CFDIU/SPLY | 2TW | J18 |
| 121VU | CFDS/CFDIU/BACK/UP | 8TW | J17 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | APU/APU/CTL | 2KD | L42 |
| 121VU | APU/ECB/SPLY | 1KD | L41 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | PTR/SPLY | 6TW | J44 |
| 121VU | CFDS/CFDIU/SPLY | 2TW | J41 |
| 121VU | CFDS/CFDIU/BACK/UP | 8TW | J40 |
Subtask 49-91-00-740-050-A ** ON A/C NOT FOR ALL
A. Do this procedure:
5. Close-up| ACTION | RESULT |
|---|---|
1.On the MCDU 1(2):
| |
| 2.Push the MCDU MENU mode key. | On the MCDU 1(2):
|
| 3.Push the line key adjacent to the CFDS indication. |
|
| 4.Push the line key adjacent to the SYSTEM REPORT/TEST indication. |
|
| 5.Push the NEXT PAGE function key. |
|
| 6.Push the line key adjacent to the APU indication. | The APU system page comes into view. |
| 7.Push the line key adjacent to the CLASS 3 FAULTS indication. | The APU CLASS 3 FAULTS page comes into view. |
| | If the maintenance message LUBE PUMP FILTER SW P9/GEN SCAV FILTER SW P5 with FCN 101 is shown:
|
| 8.Push the line key adjacent to the RETURN indication until: |
|
Subtask 49-91-00-860-053-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) On the overhead panel, push the APU MASTER/SW to OFF.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
(1) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) On the overhead panel, push the APU MASTER/SW to OFF.
(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)