Lube Filter Delta Pressure Sensor Electrical Failure channel B
TASK 79-33-00-810-836-A
Lube Filter Delta Pressure Sensor Electrical Failure channel B
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Fault Confirmation
Subtask 79-33-00-710-106-A ** ON A/C NOT FOR ALL
Subtask 79-33-00-860-063-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:38:31 UTC
Lube Filter Delta Pressure Sensor Electrical Failure channel B
1. Possible Causes
- OIL FILTER DIFFERENTIAL PRESSURE SENSOR [4077KS]
- W03 HARNESS [4087KS]
- WC10 HARNESS-CORE [4011KS]
[4000KS]
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | MULTIMETER - STANDARD |
| No specific | 1 | PLIERS - JAWED, SOFT |
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 71-00-00-810-834-A | General Troubleshooting Guidelines for Additional Troubleshooting Information |
| TSM TASK 71-00-00-810-835-A | Component and Harness Intermittent Troubleshooting Procedure for Guidance Troubleshooting Intermittent Faults |
| AMM 70-70-00-910-803 | SPOP 6 - Cleaning of the Contact Points and Wiring Harnesses |
| AMM 73-21-00-710-806 | Test No.7 - EEC Operation Test (Self Test) |
| AMM 73-21-01-000-801 | Removal of the Electronic Engine Control (EEC) |
| AMM 73-21-01-400-801 | Installation of the Electronic Engine Control (EEC) |
| AMM 73-21-63-000-802 | Removal of the Electronic Engine Control (EEC) Wiring Harness (W03) |
| AMM 73-21-63-400-802 | Installation of the Electronic Engine Control (EEC) Wiring Harness (W03) |
| AMM 73-21-69-000-802 | Removal of the EEC Wiring Harness (WC10) |
| AMM 73-21-69-400-802 | Installation of the EEC Wiring Harness (WC10) |
| AMM 78-36-00-010-802 | Opening of the Thrust Reverser Cowl-Doors |
| AMM 78-36-00-410-802 | Closing of the Thrust Reverser Cowl-Doors |
| AMM 79-33-23-000-801 | Removal of the Oil Filter Differential Pressure Sensor |
| AMM 79-33-23-400-801 | Installation of the Oil Filter Differential Pressure Sensor |
Subtask 79-33-00-710-106-A ** ON A/C NOT FOR ALL
A. Do the EEC system interactive test to confirm this fault. Refer to FADEC self test AMM 73-21-00-710-806.
(a) If no problems are found, return the engine to service. Monitor the engine for reoccurring maintenance message.
(2) If the maintenance message comes back (hard fault) in channel B, go to the Para. Fault Isolation.
4. Fault IsolationNOTE: The Electronic Engine Control (EEC) has detected the circuit for the oil filter differential pressure sensor is out of range or rate in channel B. The oil filter differential pressure sensor is mounted on the lubrication and scavenge oil pump, located at the 9 o'clock position.
(1) If the maintenance message does not come back, examine the harness and electrical connectors as described in the component and harness intermittent fault isolation procedure (Ref. TSM TASK 71-00-00-810-835). - Refer to the general troubleshooting guidelines for additional troubleshooting information (Ref. TSM TASK 71-00-00-810-834).
- Refer to the component and harness intermittent troubleshooting procedure for guidance troubleshooting intermittent faults (Ref. TSM TASK 71-00-00-810-835).
(a) If no problems are found, return the engine to service. Monitor the engine for reoccurring maintenance message.
(2) If the maintenance message comes back (hard fault) in channel B, go to the Para. Fault Isolation.
WARNING:
BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE AND ENGINE OIL CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS WARNING, INJURY CAN OCCUR.
WARNING:
REFER TO THE MSDS FOR ALL MATERIAL USED AND THE MANUFACTURER'S SAFETY INSTRUCTIONS FOR ALL EQUIPMENT USED. IF YOU DO NOT OBEY THIS WARNING, INJURY CAN OCCUR.
CAUTION:
MAKE SURE YOU REMOVE ELECTRICAL POWER FROM THE EEC BEFORE YOU REMOVE THE ELECTRICAL CONNECTORS. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.
Subtask 79-33-00-810-089-A ** ON A/C NOT FOR ALL A. If there is confirmation of the fault:
(1) Open the thrust reverser cowl-doors AMM 78-36-00-010-802.
(2) Examine the W03 (4087KS) and WC10 (4011KS) harnesses and connector P6 (4000KS-P6) - EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) - oil filter differential pressure sensor (4077KS), for problems which are possible between the EEC (4000KS) and the oil filter differential pressure sensor (4077KS).
(a) Inspect for harness damage.
(b) Inspect for loose or damaged connectors.
1 Replace W03 HARNESS(4087KS) AMM 73-21-63-000-802 and AMM 73-21-63-400-802, or
2 Replace WC10 HARNESS-CORE(4011KS) AMM 73-21-69-000-802 and AMM 73-21-69-400-802.
3 Do the test given in Para. 3.
(3) If no problems are found with the harnesses, use a PLIERS - JAWED, SOFT to disconnect electrical connector P6 (4000KS-P6) from the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) from the oil filter differential pressure sensor (4077KS).
(a) Examine the pins and sockets (contacts) for alignment and damage. Look for contacts pushed rearward into the connector face. Replace parts as necessary.
(b) Clean the contacts with contact cleaner and clean cloth per SPOP 6. Blow dry with air (at less than 30 psi) across the connector face AMM 70-70-00-910-803.
(c) Reconnect electrical connector P6 (4000KS-P6) to the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) to the oil filter differential pressure sensor (4077KS).
(d) Do the test given in Para. 3.
(4) If the fault continues:
(a) Replace OIL FILTER DIFFERENTIAL PRESSURE SENSOR [4077KS] AMM 79-33-23-000-801 and AMM 79-33-23-400-801.
(b) Do the test given in Para. 3.
(5) If the fault continues:
(a) Disconnect electrical connector P6 (4000KS-P6) from the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) from the oil filter differential pressure sensor (4077KS). Use a MULTIMETER - STANDARD to test the oil filter differential pressure sensor (4077KS) circuits in the harnesses. Refer to Table 1. Look for:
1 Wire-to-wire shorts
2 Shorts to ground
3 Continuity (less than 5 ohms resistance).
(b) If a problem is found with the harnesses or connectors:
1 Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802, or
2 Replace WC10 HARNESS-CORE [4011KS] AMM 73-21-69-000-802 and AMM 73-21-69-400-802.
3 Do the test given in Para. 3.
(6) If the fault continues:
(a) Replace the [4000KS] AMM 73-21-01-000-801 and AMM 73-21-01-400-801.
(b) Do the test given in Para. 3.
5. Close-up(1) Open the thrust reverser cowl-doors AMM 78-36-00-010-802.
(2) Examine the W03 (4087KS) and WC10 (4011KS) harnesses and connector P6 (4000KS-P6) - EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) - oil filter differential pressure sensor (4077KS), for problems which are possible between the EEC (4000KS) and the oil filter differential pressure sensor (4077KS).
(a) Inspect for harness damage.
(b) Inspect for loose or damaged connectors.
NOTE: Loose connectors must be disconnected and examined for further wear or damage.
(c) If a problem is found with the harnesses or connectors: 1 Replace W03 HARNESS(4087KS) AMM 73-21-63-000-802 and AMM 73-21-63-400-802, or
2 Replace WC10 HARNESS-CORE(4011KS) AMM 73-21-69-000-802 and AMM 73-21-69-400-802.
3 Do the test given in Para. 3.
(3) If no problems are found with the harnesses, use a PLIERS - JAWED, SOFT to disconnect electrical connector P6 (4000KS-P6) from the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) from the oil filter differential pressure sensor (4077KS).
(a) Examine the pins and sockets (contacts) for alignment and damage. Look for contacts pushed rearward into the connector face. Replace parts as necessary.
(b) Clean the contacts with contact cleaner and clean cloth per SPOP 6. Blow dry with air (at less than 30 psi) across the connector face AMM 70-70-00-910-803.
(c) Reconnect electrical connector P6 (4000KS-P6) to the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) to the oil filter differential pressure sensor (4077KS).
(d) Do the test given in Para. 3.
(4) If the fault continues:
(a) Replace OIL FILTER DIFFERENTIAL PRESSURE SENSOR [4077KS] AMM 79-33-23-000-801 and AMM 79-33-23-400-801.
(b) Do the test given in Para. 3.
(5) If the fault continues:
(a) Disconnect electrical connector P6 (4000KS-P6) from the EEC (4000KS), interconnect J110 (4110VC)/P110 (4110VC-A) and connector P35 (4077KS-P35) from the oil filter differential pressure sensor (4077KS). Use a MULTIMETER - STANDARD to test the oil filter differential pressure sensor (4077KS) circuits in the harnesses. Refer to Table 1. Look for:
1 Wire-to-wire shorts
2 Shorts to ground
3 Continuity (less than 5 ohms resistance).
NOTE: A short to ground is found when the resistance is less than 100 000 (100K) ohms.
Table 1: Oil Filter Differential Pressure Sensor Channel B Connector Contacts | W03 (4087KS) Harness P6 (4000KS-P6) EEC (4000KS) Connector Contacts | W03 (4087KS) Harness J110 (4110VC) Connector Contacts | WC10 (4011KS) Harness P110 (4110VC-A) Connector Contacts | WC10 (4011KS) Harness P35 (4077KS-P35) Oil Filter Differential Pressure Sensor(4077KS) Connector Contacts |
|---|---|---|---|
| BB | 21 | 21 | 9 |
| P | 22 | 22 | 8 |
| m | 23 | 23 | 7 |
| n | 24 | 24 | 6 |
1 Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802, or
2 Replace WC10 HARNESS-CORE [4011KS] AMM 73-21-69-000-802 and AMM 73-21-69-400-802.
3 Do the test given in Para. 3.
(6) If the fault continues:
(a) Replace the
(b) Do the test given in Para. 3.
Subtask 79-33-00-860-063-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(a) Close the thrust reverser cowl-doors AMM 78-36-00-410-802.
(1) Make sure that the work area is clean and clear of tools and other items.
(a) Close the thrust reverser cowl-doors AMM 78-36-00-410-802.
EEC Wiring Harnesses