W DOC AIRBUS | TSM A320F

Loss of the ENG2 N1 Indication on the Upper ECAM DU by the DMC2


TASK 31-63-81-810-887-A
Loss of the ENG2 N1 Indication on the Upper ECAM DU by the DMC2


1. Possible Causes
  • DMC-2 [1WT2]
  • wiring
  • DU-ECAM, UPPER [4WT1]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 31-60-00-740-002
Perform Electronic Instrument System (EIS) Input Test
ASM 316104
AMM 31-63-22-000-001
Removal of the Display Unit
AMM 31-63-22-400-001
Installation of the Display Unit
AMM 31-63-34-000-001
Removal of the DMC
AMM 31-63-34-400-001
Installation of the DMC
3. Fault Confirmation
Subtask 31-63-81-740-220-A ** ON A/C NOT FOR ALL
A. Test
Do the EIS input test AMM 31-60-00-740-002.
4. Fault Isolation
Subtask 31-63-81-810-143-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message DMC2 : ENG2 N1 DSPLY ERR:
  • on the ECAM control panel (6WT), set the UPPER DISPLAY potentiometer to OFF
  • do the test given in Para. 3.
   (1) If this test gives the maintenance message DMC2 : ENG2 N1 DSPLY ERR:
     (a) If the fault continues:
  • do a check of the wiring from DMC2 (1WT2) pins AB/11B, 11C to the first terminal block ASM 316104.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
  • do a check and repair the wiring from DMC2 (1WT2) pins AB/11D, 11E to the first terminal block.
   (2) If this test does not give a maintenance message:
     (a) If the fault continues:
  • do a check of the wiring from upper ECAM DU (4WT1) pins AA/21, 22 to the first terminal block ASM 316104.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
  • do a check and repair the wiring from upper ECAM DU (4WT1) pins AA/23, 24 to the first terminal block.
Subtask 31-63-81-740-221-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:31:02 UTC