W DOC AIRBUS | TSM A320F

Loss of the Weather Radar Picture detected by DMC 2 when the ND is shown on the F/O PFD DU


TASK 31-63-81-810-893-A
Loss of the Weather Radar Picture detected by DMC 2 when the ND is shown on the F/O PFD DU


1. Possible Causes
  • DMC-2 [1WT2]
  • PFD-F/O [2WT2]
  • XCVR-WEATHER RADAR, 1 [1SQ1]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
AMM 31-60-00-740-004
EIS System Test
ASM 316100
ASM 316200
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
AMM 34-10-00-860-002
ADIRS Start Procedure
AMM 34-10-00-860-005
ADIRS Stop Procedure
ASM 344100
AMM 34-41-33-000-004
Removal of the Weather Radar Transceiver
AMM 34-41-33-400-003
Installation of the Weather Radar Transceiver
3. Fault Confirmation
WARNING: MAKE SURE THAT:
  • NO PERSON IS IN THE AREA MADE BY AN ARC OF 135° ON EACH SIDE OF THE AIRCRAFT CENTERLINE. -THERE IS A MINIMUM SAFETY DISTANCE OF 5 METERS (16.4FT) BETWEEN THE AIRCRAFT AND ANY OBSTACLE IN THE AREA MADE BY AN ARC OF 90° ON EACH SIDE OF THE AIRCRAFT CENTERLINE.
Subtask 31-63-81-860-058-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
AMM 24-41-00-861-002
   (2) Do the ADIRS start procedure AMM 34-10-00-860-002
   (3) On the EFIS control panel of the FCU:
  • set the mode selector switches to ARC
   (4) on the center pedestal, on the WEATHER RADAR CONTROL-UNIT (3SQ), start the weather radar system.
   (5) On the FO EFIS switching panel 500VU:
  • push the PFD/ND/XFR pushbutton switch until the FO ND comes into view on the FO PFD DU
  • make sure that the FO PFD potentiometer (8WT1) is in the center position.
Subtask 31-63-81-865-057-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUCOM NAV/RADAR/15SQ1K13
Subtask 31-63-81-740-232-A ** ON A/C NOT FOR ALL
C. Test
Do the EIS system test AMM 31-60-00-740-004
Subtask 31-63-81-860-059-A ** ON A/C NOT FOR ALL
D. Put the aircraft back to its initial configuration.
   (1) Do the ADIRS stop procedure AMM 34-10-00-860-005
   (2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002
4. Fault Isolation
Subtask 31-63-81-810-153-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message WXR1(1SQ1)/DU PFD FO(2WT2)/DMC2 (1WT2):
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
     (a) Check the wiring of the WXR1 OUTPUT BUS from the DMC2 (1WT2) pins AB/14B, 14C to the FO PFD DU (2WT2) ASM 316100
     (b) Check the wiring between the DMC2 (1WT2) and the WEATHER RADAR-XCVR 1 (1SQ1) ASM 316200 ASM 344100
Subtask 31-63-81-740-233-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:31:02 UTC