TSM Lavatory Smoke Detection Failed A320

1.  Possible Causes:

-DIR-CIDS, 1 (101RH)

-DIR-CIDS, 2 (102RH)

-wiring

2.  Job Set-up Information

A.           Referenced Information

REFERENCEDESIGNATION
Ref. AMM 23-73-00-740-005BITE-Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
Ref. ASM 23-73-01
Ref. AMM 23-73-34-000-001Removal of the Cabin Intercommunication Data System (CIDS) Director
Ref. AMM 23-73-34-400-001Installation of the Cabin Intercommunication Data System (CIDS) Director

3. Fault Confirmation

SUBTASK 26-17-00-710-094-A

A.           Test

(1)          Do the CIDS Interface and Power-Up Test via the CFDS Ref. AMM 23-73-00-740-005.

4. Fault Isolation

SUBTASK 26-17-00-810-130-A

A.           If the test gives a different maintenance message:

—              Do the trouble shooting procedure related to the maintenance message.

SUBTASK 26-17-00-810-131-A

B.            If the test gives the maintenance message

CIDS(102RH)-SDF2 BUS / CIDS(101RH)-SDF1 or CIDS(101RH)-SDF1 BUS / CIDS(102RH)-SDF2 or NO LAV DATA/CIDS(101RH)-SDF1 BUS/CIDS(102RH)-SDF2 or NO LAV DATA/CIDS(102RH)-SDF2 BUS/CIDS(101RH)-SDF1:

(1)          Replace the DIR-CIDS, 1 (101RH) Ref. AMM 23-73-34-000-001 and Ref. AMM 23-73-34-400-001.

(2)          If the fault continues:

—              Replace the DIR-CIDS, 2 (102RH) Ref. AMM 23-73-34-000-001 and Ref. AMM 23-73-34-400-001.

(3)          If the fault continues:

—              Do a check and repair the wiring between the CIDS-SDF1 (AA15C and AA15H) and CIDS-SDF2 (AA11J and AA11K) Ref. ASM 23-73-01.

(4)          If the fault continues:

—              Do a check and repair the wiring between the CIDS-DIR1 (AA13A and AA13B) and CIDS-DIR2 (AA13E and AA13F) Ref. ASM 23-73-01.

SUBTASK 26-17-00-710-095-A

C.            Do the test as given in the Para. 3.

5. Close-up

SUBTASK 26-17-00-860-071-A

A.           Put the aircraft back to its initial configuration.

Read me first

All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

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