Downstream NAI Wraparound Solenoid Signal Failure on Channel B

TASK 30-21-00-810-820-A
Downstream NAI Wraparound Solenoid Signal Failure on Channel B

1. Possible Causes

W03 HARNESS [4087KS]
NAI SOLENOID BLOCK [4190KS]
[4000KS]

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

REFERENCE	QTY	DESIGNATION
No specific	1	PLIERS - JAWED, SOFT

B. Referenced Information

REFERENCE	DESIGNATION
TSM TASK 71-00-00-810-835-A	Component and Harness Intermittent Troubleshooting Procedure for Guidance Troubleshooting Intermittent Faults
AMM 30-21-21-000-801	Removal of the Nacelle Anti-Ice Solenoid-Manifold
AMM 30-21-21-400-801	Installation of the Nacelle Anti-Ice Solenoid-Manifold
AWM 715134
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 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

3. Fault Confirmation
Subtask 30-21-00-730-057-A ** ON A/C NOT FOR ALL

A. Test
Do the EEC system test AMM 73-21-00-710-806.
(1) If the maintenance message does not come into view again, do the component and harness intermittent for guidance troubleshooting intermittent faults (Ref. TSM TASK 71-00-00-810-835).
(a) If you find no fault, send the engine back to service and monitor the engine to make sure that the maintenance message does not come into view again.
(2) If the maintenance message comes into view again (hard fault) for Channel B, go to the 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.

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 30-21-00-810-069-A ** ON A/C NOT FOR ALL

A. If there is confirmation of the fault:
(1) Open the right thrust-reverser cowl-door AMM 78-36-00-010-802.
(2) Make sure that electrical connector P59 of the NAI downstream-valve solenoid-block is engaged in socket of the NAI downstream-valve solenoid-block.
(a) If it is not correctly engaged, engage it.

Do the test given in Para. 3.

(b) If the fault continues, disconnect the electrical connector P59 and do a visual inspection of the electrical connector P59 and of the receptacle J59 of the NAI downstream-valve solenoid-block for bent pins, contamination, corrosion or visual signs of damage.
1 If you find no damage on electrical connector P59:

Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802.
Do the test given in Para. 3.

2 If you find damage on the receptacle J59:

Replace NAI SOLENOID BLOCK [4190KS] AMM 30-21-21-000-801 and AMM 30-21-21-400-801.
Do the test given in Para. 3.

3 If you find no damage on the receptacle J59 and on the electrical connector P59:

Do a resistance check AWM 715134 between pin J59/1 and J59/2 of the NAI downstream-valve solenoid-block.

a If the resistance is not between 2 ohm and 2.6 kohm:

Replace NAI SOLENOID BLOCK [4190KS] AMM 30-21-21-000-801 and AMM 30-21-21-400-801.
Do the test given in Para. 3.

b If the resistance is between 2 ohm and 2.6 kohm or if fault continues:

Use PLIERS - JAWED, SOFT to disconnect electrical connectors P14 of the EEC.

(3) Do a visual inspection on the electrical connector P14 of the EEC for bent pins, contamination, corrosion or visual signs of damage.
(a) If you find damage on electrical connector P14:

Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802.
Do the test given in Para. 3.

(b) If there is no damage or if fault continues, do a continuity check AWM 715134 of the W03 harness between:
. Pin P59/1 of the NAI downstream-valve solenoid-block and pin P14/t of the EEC
. Pin P59/2 of the NAI downstream-valve solenoid-block and pin P14/u of the EEC.

If there is no continuity:
Replace W03 HARNESS [4087KS] AMM 73-21-63-000-802 and AMM 73-21-63-400-802.
Do the test given in Para. 3.

(4) If fault continues:

Replace [4000KS] AMM 73-21-01-000-801 and AMM 73-21-01-400-801.
Do the test given in Para. 3.

5. Close-up
Subtask 30-21-00-942-061-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 right thrust-reverser cowl-door AMM 78-36-00-410-802.

[Rev.8 from Aug 2018] 2026.04.04 04:29:32 UTC