W DOC AIRBUS | TSM A320F

Loss of the ENG1 N2 Indication on the Upper ECAM DU Detected by the DMC1


TASK 31-63-81-810-814-A
Loss of the ENG1 N2 Indication on the Upper ECAM DU Detected by the DMC1


1. Possible Causes
  • DMC-1 [1WT1]
  • 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 31-63-81-740-076-A ** ON A/C NOT FOR ALL
A. Test
Do the EIS input test AMM 31-60-00-740-002.
4. Fault Isolation
Subtask 31-63-81-810-066-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
DMC1: ENG1 N2 DSPLY ERR
  • on the ECAM control panel, set the UPPER DISPLAY potentiometer to OFF and do the test given in Para. 3.
   (1) If this test gives the maintenance message:
DMC1: ENG1 N2 DSPLY ERR
     (a) If the fault continues:
  • do a check of the wiring from DMC1 (1WT1) 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 DMC1 (1WT1) pins AB/11D, 11E to the first terminal block ASM 316104.
   (2) If this test gives no maintenance message:
     (a) If the fault continues:
  • do a check of the wiring from upper ECAM DU (4WT1) pins AA/35, 36 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/38, 39 to the first terminal block ASM 316104.
Subtask 31-63-81-740-077-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:30:54 UTC