Oil Debris Reset (Menu Mode) [CFML]
TASK 79-36-00-740-801-A
Oil Debris Reset (Menu Mode)
PRE CFM SB 73-0021
This option will be used to clear the count of the number of metallic chips that have been detected by the oil debris monitoring system during the last flight and the cumulative count during all flights. This function will only be available on channel B.
END OF PRE CFM SB 73-0021
POST CFM SB 73-0021
This option will be used to set the number of metallic chips that have been detected by the oil debris monitoring system for the cumulative count during all flights. This value should be set to zero when you clean and do an inspection of the ODMS chips or set to previous chip count if you reprogram or replace EEC channel B and not clean and do an inspection of the ODMS chips. This function will only be available on channel B.
END OF POST CFM SB 73-0021
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 79-36-00-861-050-A Subtask 79-36-00-865-050-A
Subtask 79-36-00-740-050-A
Subtask 79-36-00-862-050-A Subtask 79-36-00-860-050-A
[Rev.10 from 2021]
2026.04.01 13:07:12 UTC
Oil Debris Reset (Menu Mode)
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
ZONE: 400
1. Reason for the JobPRE CFM SB 73-0021
This option will be used to clear the count of the number of metallic chips that have been detected by the oil debris monitoring system during the last flight and the cumulative count during all flights. This function will only be available on channel B.
END OF PRE CFM SB 73-0021
POST CFM SB 73-0021
This option will be used to set the number of metallic chips that have been detected by the oil debris monitoring system for the cumulative count during all flights. This value should be set to zero when you clean and do an inspection of the ODMS chips or set to previous chip count if you reprogram or replace EEC channel B and not clean and do an inspection of the ODMS chips. This function will only be available on channel B.
END OF POST CFM SB 73-0021
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 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 |
Subtask 79-36-00-861-050-A Subtask 79-36-00-865-050-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 79-36-00-866-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENGINE 1) | |||
| 49VU | ENGINE/1/FADEC A/AND EIU 1 | 2KS1 | A04 |
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R40 |
| FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENGINE 2) | |||
| 49VU | ENGINE/2/FADEC A/AND EIU 2 | 2KS2 | A05 |
| 121VU | ENGINE/ENG2/FADEC B/AND EIU2 | 4KS2 | R41 |
C. Aircraft Maintenance Configuration
(1) On ENG panel 115VU:
(a) Make sure that the ENG MASTER switch 1(2) is set to OFF.
(b) Make sure that the ENG/MODE rotary selector switch is set to NORM.
(2) On the ENG section of maintenance panel 50VU:
(a) Release the FADEC GND PWR1(2) pushbutton switch. The ON legend of this pushbutton switch comes on.
4. Procedure(1) On ENG panel 115VU:
(a) Make sure that the ENG MASTER switch 1(2) is set to OFF.
(b) Make sure that the ENG/MODE rotary selector switch is set to NORM.
(2) On the ENG section of maintenance panel 50VU:
(a) Release the FADEC GND PWR1(2) pushbutton switch. The ON legend of this pushbutton switch comes on.
NOTE: After the FADEC is energized, wait ten seconds before you start the test. If you do not wait ten seconds, the interactive mode stops the EEC self-test and this can cause spurious faults.
(3) On the left or right MCDU, get the SYSTEM REPORT/TEST/ENG page (Ref. AMM TASK 31-32-00-860-012). Subtask 79-36-00-740-050-A
A. Oil Debris Reset
END OF PRE CFM SB 73-0021
POST CFM SB 73-0021
END OF POST CFM SB 73-0021
5. Close-upNOTE: The EEC will not enter the menu mode (interactive mode) after an enquire command from the Centralized Fault Display System (CFDS) when any of the following conditions are set:
- N2 more than ten percent or invalid
- Engine not off or engine initializing
- Engine not in default start state
- Throttle Lever Angle (TLA) not at idle or invalid
- Aircraft in the air
- MASTER lever on or invalid
- BITE command code input label invalid.
NOTE: The EEC will abort the oil debris function and display the FUNCTION TERMINATED page when any of the following conditions becomes set:
- N2 more than ten percent or invalid
- Engine not in default start state
- Throttle Lever Angle (TLA) not at idle or invalid
- MASTER lever on or invalid
- You enter in the interactive mode of the other channel
- RETURN key is selected on the MCDU during a running test or a special function.
Refer to the figure.
NOTE: If one of the following conditions occurs while the menu mode is active, Menu Mode session will be exited directly, without displaying a specific screen:
- RETURN key selected on main menu screen
- Channel in Menu Mode is not the active channel
- Invalid BITE command or invalid equipment code received by the EEC
- A LOGOFF condition received by the EEC
- Engine start detected whereas function requiring idle speed (as idle test, vibration ground run) is not active
- Selected Mach is more than 0.12 or invalid
- Aircraft indicates in air.
NOTE: During the test, obey the instructions shown on the MCDU.
| ACTION | RESULT |
|---|---|
| 1.Initialize Menu Mode on the applicable engine and EEC, by selecting FADEC XY (X = engine position, Y = channel number). For this test, Y shall be set to B because this function is only available on channel B. | |
2.On the MCDU ENGINE MAIN MENU page:
| SPECIAL FUNCTIONS pages will be shown. |
3.On the SPECIAL FUNCTIONS main page:
| The page display the chip count from the last flight and cumulative count. |
4.On the MCDU OIL DEBRIS RESET page:
| Confirm reset will be shown. Wait a minimum of four seconds. The EEC must perform the following:
NOTE: The last flight count is unchanged and can be reset only through EEC depowering.
|
5.On the MCDU OIL DEBRIS RESET page:
| The SPECIAL FUNCTIONS main page will be shown. |
6.On the SPECIAL FUNCTIONS main page:
| The MCDU Home page comes into view. |
END OF PRE CFM SB 73-0021
POST CFM SB 73-0021
NOTE: During the test, obey the instructions shown on the MCDU.
| ACTION | RESULT |
|---|---|
| 1.Initialize Menu Mode on the applicable engine and EEC, by selecting FADEC XY (X = engine position, Y = channel number). For this test, Y shall be set to B because this function is only available on channel B. | |
2.On the MCDU ENGINE MAIN MENU page:
| SPECIAL FUNCTIONS page will be shown. |
3.On the SPECIAL FUNCTIONS main page:
| The page display the chip count from the last flight and cumulative count. |
4.On the MCDU OIL DEBRIS RESET page:
| Oil Debris Chip Count Entry Input screen will be shown. |
5.On the MCDU Oil Debris Count Entry Input screen:
| The SPECIAL FUNCTIONS main page will be shown. NOTE: The input value must consist of two characters (0-9 for each character). The cumulative chip count entered must be between 00-19. NOTE: An input of zero should be entered if the oil debris monitoring sensor has been cleaned and inspected. If you reprogram or replace EEC channel B, enter the previous cumulative chip count. |
6.On the MCDU Oil Debris Count Entry Input screen:
| If the input value is correct (two characters with a value between 00-19), the DMS Chip Count Entry Confirmation screen is shown. If the input is not correct, the DMS Chip Count Invalid Entry screen is shown. Select RETURN (5R) and the SPECIAL FUNCTIONS main screen is shown. |
7.On the MCDU DMS Chip Count Entry Confirmation screen, verify that the entered chip count is correct.
| If CONFIRM (5R) was selected and the NVM store was successful, the OIL DEBRIS RESET page (with CONFIRM RESET indication) is shown. Wait a minimum of four seconds. If the NVM store failed, the OIL DEBRIS RESET page (NVM Store Failed) is shown. If UPDATE (5L) was selected, the OIL Debris Count Entry Input screen is shown. Apply the previous steps from step 5 again. |
8.On the MCDU OIL DEBRIS RESET page:
| The SPECIAL FUNCTIONS main page will be shown. |
9.On the SPECIAL FUNCTIONS main page:
| The MCDU Home page comes into view. |
Subtask 79-36-00-862-050-A Subtask 79-36-00-860-050-A
B. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(1) Make sure that the work area is clean and clear of tools and other items.
FUNCTION TERMINATED page