Burner Pressure High Range Sensor Signal Disagreement

TASK 73-21-00-810-865-A
Burner Pressure High Range Sensor Signal Disagreement

1. Possible Causes

SENSOR - P3 [4085KS]
W04 HARNESS [4088KS]
W03 HARNESS [4087KS]
[4000KS]

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	MULTIMETER - STANDARD
No specific	1	PLIERS - JAWED, SOFT

B. Referenced Information

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 24-41-00-861-002	Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002	De-energize the Aircraft Electrical Circuits Supplied from the External Power
AMM 70-70-00-910-803	SPOP 6 - Cleaning of the Contact Points and Wiring Harnesses
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 73-21-23-000-801	Removal of the Burner Pressure Sensor
AMM 73-21-23-400-801	Installation of the Burner Pressure Sensor
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 73-21-64-000-802	Removal of the Electronic Engine Control (EEC) Wiring Harness (W04)
AMM 73-21-64-400-802	Installation of the Electronic Engine Control (EEC) Wiring Harness (W04)
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
EEC Wiring Harnesses
W03/W04 Harness Interconnect
Burner Pressure Sensor Wiring Harness
Burner Pressure Sensor Wiring Schematic

3. Fault Confirmation
Subtask 73-21-00-710-116-A ** ON A/C NOT FOR ALL

A. Energize the FADEC of the engine that has a fault report.
(1) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
(2) On the ENG section of maintenance panel 50VU:
(a) Release the FADEC GND PWR/1(2) pushbutton switch (the ON legend 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 Multipurpose Control and Display Unit (MCDU) screen, check if the fault is displayed on ground scanning report.

NOTE: The Electronic Engine Control (EEC) has detected the high pressure transducer circuits for the burner pressure sensor do not agree in channel A and B. The burner pressure sensor is attached to the compressor intermediate case bulkhead, located at the 10 o'clock position.

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 fault (Ref. TSM TASK 71-00-00-810-835).

(4) If the maintenance message does not come back, examine the harnesses and electrical connectors as described in the component and harness intermittent fault isolation procedure (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.
(5) If the maintenance message comes back (hard fault), go to Para. Fault Isolation.

4. Fault Isolation

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 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 73-21-00-810-137-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 W04 (4088KS) and W03 (4087KS) harnesses, connectors P3 (4000KS-P3) and P4 (4000KS-P4) - EEC (4000KS), interconnect J107 (4101VC)/P107 (4101VC-A) and connector P39 (4085KS-P39) - burner pressure sensor (4085KS), for problems which are possible between the EEC (4000KS) and the burner pressure sensor (4085KS).
(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 W04 HARNESS (4088KS) AMM 73-21-64-000-802 and AMM 73-21-64-400-802, or
2 Replace W03 HARNESS (4087KS) AMM 73-21-63-000-802 and AMM 73-21-63-400-802.
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 connectors P3 (4000KS-P3) and P4 (4000KS-P4) from the EEC (4000KS), interconnect J107 (4101VC)/P107 (4101VC-A) and connector P39 (4085KS-P39) from the burner pressure sensor (4085KS).
(a) Examine the pins, sockets (contacts) and lugs 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 connector face AMM 70-70-00-910-803.
(c) Reconnect the electrical connectors P3 (4000KS-P3) and P4 (4000KS-P4) from EEC (4000KS), interconnect J107 (4101VC)/P107 (4101VC-A) and connector P39 (4085KS-P39) from the burner pressure sensor (4085KS).
(d) Do the test given in Para. 3.
(4) If the fault continues:
(a) Replace SENSOR - P3 [4085KS] AMM 73-21-23-000-801 and AMM 73-21-23-400-801.
(b) Do the test given in Para. 3.
(5) If the fault continues:
(a) Disconnect the electrical connectors P3 (4000KS-P3) and P4 (4000KS-P4) from the EEC (4000KS), interconnect J107 (4101VC)/P107 (4101VC-A) and connector P39 (4085KS-P39) from the burner pressure sensor (4085KS). Use a MULTIMETER - STANDARD to test the burner pressure sensor high pressure transducer channel A and channel B circuits in the harnesses. Refer to Table 1 and Table 2. 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: Burner Pressure Sensor High Pressure Transducer Channel A Connector Contacts

W04 (4088KS) Harness P3 (4000KS P3) EEC (4000KS) Connector Contacts	W04 (4088KS) Harness J107 (4101VC) Connector Contacts	W03 (4087KS) Harness P107 (4101VC-A) Connector Contacts	W03 (4087KS) Harness P39 (4085KS-P39) Burner Pressure Sensor (4085KS) Connectors Contact
D	14	14	2
E	15	15	1
F	16	16	8
f	17	17	9

Table 2: Burner Pressure Sensor High Pressure Transducer Channel B Connector Contacts

W03 (4087KS) Harness P4 (4000KS-P4) EEC (4000KS) Connector Contacts	W03 (4087KS) Harness P39 (4085KS-P39) PB Sensor (4085KS) Connector Contacts
D	3
E	10
F	12
f	11

(b) If a problem is found with the harnesses or connectors:
1 Replace W04 HARNESS [4088KS] AMM 73-21-64-000-802 and AMM 73-21-64-400-802, or
2 Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802.
3 Do the test given in Para. 3.
(6) If the fault continues:
(a) Replace [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
Subtask 73-21-00-860-057-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.
(b) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.

[Rev.8 from Aug 2018] 2026.04.04 04:36:39 UTC