DOC AIRBUS | AMM A320FReplacement of the Engine Oil Filter and Inspection of the Magnetic Chip Detector [PW11]
TASK 79-35-00-040-812-A
Replacement of the Engine Oil Filter and Inspection of the Magnetic Chip Detector
MMEL 79-09-05B
ENG 1(2) OIL SENSOR FAULT ALERT
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 79-35-00-861-052-A ** ON A/C NOT FOR ALL
Subtask 79-35-00-040-058-A ** ON A/C NOT FOR ALL
Subtask 79-35-00-860-068-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 03:42:26 UTC
Replacement of the Engine Oil Filter and Inspection of the Magnetic Chip Detector
WARNING:
BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
1. Reason for the JobMMEL 79-09-05B
ENG 1(2) OIL SENSOR FAULT ALERT
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 400 | POWER PLANT, NACELLES AND PYLONS |
| 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) |
| TASK 31-32-00-860-012-A | Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page |
| TASK 79-00-00-281-802-A | Inspection of the Magnetic Chip Collectors for Oil Contamination |
| TASK 79-21-06-960-801-A | Replace the Oil Filter Element |
Subtask 79-35-00-861-052-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized
(Ref. AMM TASK 24-41-00-861-002).
4. Procedure(1) Make sure that the aircraft electrical circuits are energized
(Ref. AMM TASK 24-41-00-861-002).
Subtask 79-35-00-040-058-A ** ON A/C NOT FOR ALL
A. On the Centralized Fault Display System (CFDS), do a check for the maintenance messages "ENGxD-0677-PHMU INTERNAL FAIL" and/or "ENGxD-0678-PHMU CAN BUS FAIL" and/or "ENGxD-0730-PHMU INTERNAL SNSR INTERFACE" and/or "ENGxA-0571-LOSS OF ODM" and/or "ENGxB-0572-LOSS OF ODM".
(1) On the Multipurpose Control and Display Unit (MCDU), in the interactive-mode fault reports of the Electronic Engine Control (EEC), make sure that these maintenance messages are not shown for channel A and/or channel B.
(a) Get access to the three reports that follow:
1 Ground report:
a On the left or right MCDU, get the SYSTEM REPORT/TEST/ENG menu page (Ref. AMM TASK 31-32-00-860-012).
b Initialize Menu Mode of the applicable engine and EEC channel by selecting FADEC XY (X = Engine position, Y = EEC channel).
c From the Menu Mode MAIN MENU, select the key adjacent to GROUND REPORT (5R).
d The GROUND REPORT screen is displayed, providing fault information.
2 Last leg report:
a On the left or right MCDU, get the SYSTEM REPORT/TEST/ENG menu page (Ref. AMM TASK 31-32-00-860-012).
b Initialize Menu Mode of the applicable engine and EEC channel by selecting FADEC XY (X = Engine position, Y = EEC channel).
c From the Menu Mode MAIN MENU, select the key adjacent to LAST LEG REPORT (1L).
d The LAST LEG REPORT screen is displayed, providing fault information.
3 Post Flight Report (PFR):
a On the printed report, read the list of failure messages.
(b) Make sure that the fault messages "ENGxD-0677-PHMU INTERNAL FAIL" and/or "ENGxD-0678-PHMU CAN BUS FAIL" and/or "ENGxD-0730-PHMU INTERNAL SNSR INTERFACE" and/or "ENGxA-0571-LOSS OF ODM" and/or "ENGxB-0572-LOSS OF ODM" are not shown on these reports.
Subtask 79-35-00-960-054-A ** ON A/C NOT FOR ALL Subtask 79-35-00-281-053-A ** ON A/C NOT FOR ALL 5. Close-up(1) On the Multipurpose Control and Display Unit (MCDU), in the interactive-mode fault reports of the Electronic Engine Control (EEC), make sure that these maintenance messages are not shown for channel A and/or channel B.
(a) Get access to the three reports that follow:
1 Ground report:
a On the left or right MCDU, get the SYSTEM REPORT/TEST/ENG menu page (Ref. AMM TASK 31-32-00-860-012).
b Initialize Menu Mode of the applicable engine and EEC channel by selecting FADEC XY (X = Engine position, Y = EEC channel).
c From the Menu Mode MAIN MENU, select the key adjacent to GROUND REPORT (5R).
d The GROUND REPORT screen is displayed, providing fault information.
2 Last leg report:
a On the left or right MCDU, get the SYSTEM REPORT/TEST/ENG menu page (Ref. AMM TASK 31-32-00-860-012).
b Initialize Menu Mode of the applicable engine and EEC channel by selecting FADEC XY (X = Engine position, Y = EEC channel).
c From the Menu Mode MAIN MENU, select the key adjacent to LAST LEG REPORT (1L).
d The LAST LEG REPORT screen is displayed, providing fault information.
3 Post Flight Report (PFR):
a On the printed report, read the list of failure messages.
(b) Make sure that the fault messages "ENGxD-0677-PHMU INTERNAL FAIL" and/or "ENGxD-0678-PHMU CAN BUS FAIL" and/or "ENGxD-0730-PHMU INTERNAL SNSR INTERFACE" and/or "ENGxA-0571-LOSS OF ODM" and/or "ENGxB-0572-LOSS OF ODM" are not shown on these reports.
Subtask 79-35-00-860-068-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Make an entry in the logbook to record that:
(Ref. AMM TASK 24-41-00-862-002).
(1) Make an entry in the logbook to record that:
- You replaced the oil filter element.
- You did the inspection of the magnetic chip detector.
(Ref. AMM TASK 24-41-00-862-002).