W DOC AIRBUS | TSM A320F

ENG Page not automatically displayed on the lower ECAM DU during Engine start or Engine crank sequence


TASK 31-63-82-810-863-A
ENG Page not automatically displayed on the lower ECAM DU during Engine start or Engine crank sequence


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 71-00-00-810-831-A
ENG page not automatically displayed on the lower ECAM unit during engine start or engine crank sequence
AMM 31-53-34-000-001
Removal of the Flight Warning Computer (FWC)
AMM 31-53-34-400-001
Installation of the Flight Warning Computer (FWC)
AMM 31-63-34-000-001
Removal of the DMC
AMM 31-63-34-400-001
Installation of the DMC
3. Fault Confirmation
Subtask 31-63-82-710-058-A ** ON A/C NOT FOR ALL
A. Not applicable, the fault is evident.
4. Fault Isolation
Subtask 31-63-82-810-156-A ** ON A/C NOT FOR ALL
A. Do the procedure as follows:
   (1) On the ECAM control panel, make sure that no system key (ENG, BLEED, PRESS, FUEL, APU,etc...) is lighted.
   (2) If yes, release the related key.
   (3) If the fault continues:
  • set the the EIS DMC selector switch (18WT) on the panel 8VU from NORM position to F/O/3 position.
     (a) If the fault stops:
     (b) If the fault continues:
       1 If the fault stops:
       2 If the fault continues:
         a If the fault stops:
         b If the fault continues:
Subtask 31-63-82-810-156-D ** ON A/C NOT FOR ALL
A. Do the procedure as follows:
   (1) On the ECAM control panel, make sure that no system key (ENG, BLEED, PRESS, FUEL, APU,etc...) is lighted.
   (2) If yes, release the related key.
   (3) If the fault continues:
  • set the the EIS DMC selector switch (18WT) on the panel 8VU from NORM position to CAPT/3 position.
     (a) If the fault stops:
     (b) If the fault continues:
       1 If the fault stops:
       2 If the fault continues:
         a If the fault stops:
         b If the fault continues:
[Rev.8 from Aug 2018] 2026.04.04 04:31:18 UTC