W DOC AIRBUS | TSM A320F

Disagree between LGCIU1 and LGCIU2 for the SEC


TASK 27-94-00-810-894-A
Disagree between LGCIU1 and LGCIU2 for the SEC


1. Possible Causes
  • SEC-3 [1CE3]
  • SEC-2 [1CE2]
  • SEC-1 [1CE1]
  • LGCIU-1 [5GA1]
  • LGCIU-2 [5GA2]
  • PROX SNSR-R L/G EXT, SYS 1 [20GA]
  • PROX SNSR-L L/G EXT, SYS 1 [21GA]
  • PROX SNSR-R L/G EXT, SYS 2 [22GA]
  • PROX SNSR-L L/G EXT, SYS 2 [23GA]
  • PROX SNSR-NLG UPLK, SYS 1 [12GA]
  • PROX SNSR-NLG UPLK, SYS 2 [13GA]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 27-94-34-000-001
Removal of the SEC
AMM 27-94-34-400-001
Installation of the SEC
AMM 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
AMM 32-00-00-860-002
Ground Configuration after Flight Configuration with Electrical Power
AMM 32-31-71-000-001
Removal of the LGCIU
AMM 32-31-71-400-001
Installation of the LGCIU
AMM 32-31-73-000-001
Removal of the MLG Proximity-Sensors
AMM 32-31-73-000-005
Removal of the NLG Proximity-Sensors
AMM 32-31-73-400-001
Installation of the MLG Proximity-Sensors
AMM 32-31-73-400-005
Installation of the NLG Proximity-Sensors
AMM 32-69-00-860-001
Simulation of Flight (With Aircraft on Ground)
3. Fault Confirmation
Subtask 27-94-00-860-077-A
A. Test
   (1) Do the simulation of flight, with the aircraft on the ground AMM 32-69-00-860-001.
Subtask 27-94-00-740-156-A
B. Test
   (1) Do the BITE test of the EFCS (ground scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-94-00-865-050-A
A. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
Subtask 27-94-00-810-145-A
B. If the test doesn' t confirm the fault and if the maintenance message LGCIU BUS DISAGREE was shown after landing gear free-fall extension:
  • no maintenance action is necessary.
Subtask 27-94-00-810-131-A
C. If the BITE test gives the maintenance message:
LGCIU BUS DISAGREE
  • open the circuit breaker (21CE1) on the panel 49VU and the circuit breaker (22CE) on the panel 105VU for the SEC1
  • open the circuit breaker (21CE2) on the panel 121VU for the SEC2 and do the test given in Para. 3. (only the SEC3 is supplied).
   (1) Close the circuit breaker (21CE2).
   (2) Open the circuit breaker (21CE3) on the panel 121VU for the SEC3 and do the test given in Para. 3. (only the SEC2 is supplied).
   (3) Close the circuit breakers (21CE1) and (22CE).
   (4) Open the circuit breaker (21CE2) on the panel 121VU for the SEC2 and do the test given in Para. 3. (only the SEC1 is supplied).
   (5) Close the circuit breakers (21CE2) and (21CE3).
     (a) If the message is shown only when the SEC3 is supplied:
     (b) If the message is shown only when the SEC2 is supplied:
     (c) If the message is shown only when the SEC1 is supplied:
       1 If the fault continues:
       2 If the fault continues:
     (d) If the message is shown when the SEC2 is supplied and when the SEC3 is supplied:
       1 If the fault continues:
     (e) If the message is shown when the SEC1 is supplied, when the SEC2 is supplied and when the SEC3 is supplied:
       1 If the fault continues:
       2 If the fault continues:
       3 If the fault continues:
       4 If the fault continues:
       5 If the fault continues:
       6 If the fault continues:
       7 If the fault continues:
Subtask 27-94-00-740-157-A
D. Do the test given in Para. 3.
5. Close-up
Subtask 27-94-00-860-078-A
A. Do the ground configuration after the flight configuration AMM 32-00-00-860-002.
[Rev.8 from Aug 2018] 2026.04.04 04:28:20 UTC