W DOC AIRBUS | TSM A320F

Maintenance Status SMOKE without a Maintenance Message


TASK 26-16-00-810-821-A
Maintenance Status SMOKE without a Maintenance Message


1. Possible Causes

2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 26-10-00-740-802
Ground Scanning of the Cabin Intercommunication Data-System (CIDS) - Smoke Detection Function (SDF)
3. Fault Confirmation
Subtask 26-16-00-865-067-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
49VUAIR COND/CIDS/SDF/DIR2 ESS18WHC06
49VUAIR COND/CIDS/SDF/DIR1 ESS15WHC05
49VUCOM/CIDS/DIR ESS/1150RHG01
** ON A/C NOT FOR ALL
49VUCOM DIR ESS/2157RHG02
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM06
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
121VUCOM NAV/CIDS/DIR NORM/1151RHM05
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DIR 2/BAT146RHP14
121VUCOM/CIDS/DIR 1/BAT147RHP13
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DIR NORM/2156RHM07
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
121VUCOM NAV/CIDS/DIR NORM/1151RHM06
** ON A/C NOT FOR ALL
122VUAIR COND/CIDS/SDF/DIR NORM/214WHT18
122VUAIR COND/CIDS/SDF/DIR NORM/117WHT17
Subtask 26-16-00-710-091-A ** ON A/C NOT FOR ALL
B. Test
   (1) Deactivation of the CIDS Directors
     (a) On the circuit breaker panel 49VU, open the circuit breakers 15WH and 18WH, then open the circuit breakers 150RH and 157RH.
     (b) On the circuit breaker panel 121VU, open the circuit breakers 17WH and 14WH, then open the circuit breakers 151RH and 156RH.
   (2) Reactivation of the CIDS Directors
     (a) After a minimum of 5 seconds from power-down, on circuit breaker panel 121VU, close the circuit breakers 151RH and 156RH.
     (b) On circuit breaker panel 49VU, close the circuit breakers 150RH and 157RH.
NOTE: The CIDS-SDF1 and CIDS-SDF2 must be energized within maximum 30 seconds after CIDS is energized.
     (c) On circuit breaker panel 49VU, close the circuit breakers 15WH and 18WH at the same time.
     (d) On circuit breaker panel 121VU, within maximum 2 seconds after the CIDS-SDF1 and CIDS-SDF2 essential busses are energized, close circuit breakers 17WH and 14WH at the same time.
   (3) After a minimum time of 30 seconds, do the Ground Scanning of the Cabin Intercommunication Data-System (CIDS) - Smoke Detection Function (SDF) AMM 26-10-00-740-802.
4. Fault Isolation
Subtask 26-16-00-810-107-A ** ON A/C NOT FOR ALL
A. If the test gives a different maintenance message:
  • Do the trouble shooting procedure related to the maintenance message.
Subtask 26-16-00-810-108-A ** ON A/C NOT FOR ALL
B. If the test gives the maintenance message TEST OK and if the maintenance status SMOKE goes out of view, no other maintenance action is necessary.
5. Close-up
Subtask 26-16-00-860-070-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:27:19 UTC