W DOC AIRBUS | TSM A320F

FDIMU Receives No Data from the SFCC 1 or SFCC 2


TASK 31-36-00-810-914-A
FDIMU Receives No Data from the SFCC 1 or SFCC 2


1. Possible Causes
  • wiring
  • SLAT/FLAP CONTR.COMP. [21CV]
  • SLAT/FLAP CONTR.COMP. [22CV]
  • DMU/FDIU (FDIMU) [10TV]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 27-54-00-710-001
Operational Test of the Flap System
AMM 31-36-00-740-012
Test of the Flight Data Interface and Management Unit (FDIMU)
AMM 31-36-34-000-002
Removal of the FDIU/DMU (FDIMU)
AMM 31-36-34-400-002
Installation of the FDIU/DMU (FDIMU)
ASM 313701
3. Fault Confirmation
Subtask 31-36-00-740-200-A ** ON A/C NOT FOR ALL
A. Do the FDIMU (10TV) fault monitoring test (AIDS-part) AMM 31-36-00-740-012.
NOTE: Make sure that the circuit breakers 5TV, 7CV, 8CV, 11CV, 12CV, 2CN on the panel 121VU and 1CN, 5CV, 6CV on the panel 49VU and 9CV, 10CV on the panel 122VU are closed during the test.
4. Fault Isolation
Subtask 31-36-00-810-128-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:

  • SFCC1 (21CV) / FDIMU (10TV) or
  • SFCC2 (22CV) / FDIMU (10TV)

   (1) Do the operational test of the slat and flap control computer AMM 27-54-00-710-001.

     (a) If the test gives a different maintenance message, you can find the related trouble shooting procedure in the applicable Page Block 201.

   (2) If the fault continues:
  • do a check and if necessary repair the wiring between the SLAT/FLAP CONTR.COMP. [21CV] or SLAT/FLAP CONTR.COMP. [22CV] and the DMU/FDIU (FDIMU) [10TV] ASM 313701:

    SFCC 1 Connector AB/4E to FDIMU Connector AA/3A
    SFCC 1 Connector AB/4F to FDIMU Connector AA/3B
    SFCC 2 Connector AB/4E to FDIMU Connector AB/3A
    SFCC 2 Connector AB/4F to FDIMU Connector AB/3B

   (3) If the fault continues:
Subtask 31-36-00-740-201-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:30:07 UTC