W DOC AIRBUS | AMM A320F

Installation of the Proximity Switches of the Avionics Compartment Doors


TASK 52-71-14-400-001-A
Installation of the Proximity Switches of the Avionics Compartment Doors


ZONE: 120
ZONE: 125
ZONE: 126
ZONE: 128
FIN: 23WV
FIN: 36WV
FIN: 38WV
FIN: 40WV
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
CAP - BLANKING
FOR [23WV] (PROX SW-FRAME, L AVIONICS COMPT DOOR)
FOR [36WV] (PROX SW-FRAME, FWD AVIONICS COMPT DOOR)
FOR [38WV] (PROX SW-FRAME, R AVIONICS COMPT DOOR)
No specific
Torque wrench: range to between 6.3 and 5.7 m.N (55.75 and 50.44 lbf.in ) T
FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
No specific
Torque wrench: range to between 5.3 and 4.7 m.N (46.90 and 41.59 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.14QDB1)
Wire-Locking Dia: 0.5 mm (0.020 inch) CRES Nickel Alloy -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
120
AVIONICS COMPARTMENT
125
LATERAL AVIONIC COMPARTMENT
126
LATERAL AVIONIC COMPARTMENT
128
REAR AVIONIC COMPARTMENT
811, 812, 822, 824
FOR [23WV] (PROX SW-FRAME, L AVIONICS COMPT DOOR)
812
FOR [36WV] (PROX SW-FRAME, FWD AVIONICS COMPT DOOR)
811
FOR [38WV] (PROX SW-FRAME, R AVIONICS COMPT DOOR)
822
FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
128EG, 824
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 52-41-00-010-002-A
Open the Avionics Compartment Doors for Access
TASK 52-41-00-410-002-A
Close the Avionics Compartment Doors after Access
TASK 52-71-00-710-001-A
Operational Test of the Door Warning System
TASK 52-71-00-820-008-A
Adjustment of the Proximity Switches of the Avionics Compartment Doors 811, 812 and 824
TASK 52-71-00-820-011-A
Adjustment of the Proximity Switch of the Avionics Compartment Door 822
FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
TASK 53-12-13-400-001-A
Installation of the avionics compartment floor panels
3. Job Set-up
Subtask 52-71-14-860-051-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ground service network is energized (Ref. AMM TASK 24-42-00-861-001).
   (2) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position in front of avionics compartment door 811, 812, 822 or 824.
   (3) Make sure that the applicable avionics compartment door is open (Ref. AMM TASK 52-41-00-010-002):
     (a) FOR [36WV] (PROX SW-FRAME, FWD AVIONICS COMPT DOOR)
811
     (b) FOR [23WV] (PROX SW-FRAME, L AVIONICS COMPT DOOR)
812
     (c) FOR [38WV] (PROX SW-FRAME, R AVIONICS COMPT DOOR)
822
     (d) FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
824.
Subtask 52-71-14-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUAIR COND/AVNCS VENT/CTL6HQD06
121VUEIS/SDAC1 AND 2/DOOR/DET/AVNCS46WVP02
4. Procedure
Subtask 52-71-14-420-050-A
A. Installation of the Proximity Switch
   (1) Install the proximity switch (2) on the support (3).
   (2) Install the washer (4) and the nut (5).
   (3) TORQUE the nut (5) as follows:
     (a) FOR [36WV] (PROX SW-FRAME, FWD AVIONICS COMPT DOOR), [23WV] (PROX SW-FRAME, L AVIONICS COMPT DOOR), [38WV] (PROX SW-FRAME, R AVIONICS COMPT DOOR)
TORQUE the nut (5) to between 6.3 and 5.7 m.N (55.75 and 50.44 lbf.in ) T.
     (b) FOR [
40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
TORQUE the nut (5) to between 5.3 and 4.7 m.N (46.90 and 41.59 lbf.in ) T.
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
   (4) Safety the nut (5) with the 14QDB1Wire-Locking Dia: 0.5 mm (0.020 inch) CRES Nickel Alloy -.
   (5) Remove the CAP - BLANKING from the electrical connector (1).
   (6) Connect the electrical connector (1) to the proximity switch (2).
   (7) Adjust the proximity switch (2) (
Ref. AMM TASK 52-71-00-820-008) or (Ref. AMM TASK 52-71-00-820-011).
Subtask 52-71-14-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SDAC1 AND 2/DOOR/DET/AVNCS46WVP02
Subtask 52-71-14-720-050-A
C. Operational Test
   (1) Do an operational test of the warning system of the avionics compartment doors (Ref. AMM TASK 52-71-00-710-001).
5. Close-up
Subtask 52-71-14-420-052-B
A. Installation of Components
   (1) FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
Install access panel 128EG (Ref. AMM TASK 53-12-13-400-001).
Subtask 52-71-14-865-053-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUAIR COND/AVNCS VENT/CTL6HQD06
Subtask 52-71-14-410-051-A
C. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the applicable avionics compartment door (Ref. AMM TASK 52-41-00-410-002):
     (a) FOR [36WV] (PROX SW-FRAME, FWD AVIONICS COMPT DOOR)
811
     (b) FOR [23WV] (PROX SW-FRAME, L AVIONICS COMPT DOOR)
812
     (c) FOR [38WV] (PROX SW-FRAME, R AVIONICS COMPT DOOR)
822
     (d) FOR [40WV] (PROX SW-FRAME, AFT AVIONICS COMPT DOOR)
824.
   (3) Remove the access platform(s).
Subtask 52-71-14-860-052-A
D. Aircraft Maintenance Configuration
   (1) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.02 07:24:13 UTC