W DOC AIRBUS | AMM A320F

General Visual Inspection of EWIS Installed in the Lateral Avionic Compartment (EWIS)


TASK 24-92-00-210-808-A
General Visual Inspection of EWIS Installed in the Lateral Avionic Compartment (EWIS)


ZONE: 125
ZONE: 126
1. Reason for the Job
Refer to the MPD TASK: 200125-03
NOTE: This is an EWIS (Electrical Wiring Interconnection System) procedure. EWIS is defined in ESPM 20-33-11.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
AR
FLASHLIGHT
No specific
AR
MIRROR - INSPECTION, FLEXIBLE
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
125
LATERAL AVIONIC COMPARTMENT
126
LATERAL AVIONIC COMPARTMENT
812, 813, 822, 824
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 52-10-00-010-001-A
Opening of the Passenger/Crew Door
TASK 52-10-00-410-001-A
Closing of the Passenger/Crew Door
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
ESPM 2052110
3. Job Set-up
Subtask 24-92-00-010-153-A
A. Get Access
   (1) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position.
   (2) Open the forward passenger/crew door 831 (Ref. AMM TASK 52-10-00-010-001).
   (3) Open the access doors 812 822 824 (Ref. AMM TASK 52-41-00-010-002).
   (4) Open the access door 813, if installed.
Subtask 24-92-00-862-139-A
B. Make sure that the aircraft electrical circuits are de-energized
(Ref. AMM TASK 24-41-00-862-002).
4. Procedure
Subtask 24-92-00-210-108-A
A. General Visual Inspection of All Wiring Installed in the Lateral Avionic Compartment
   (1) Do a visual inspection of the wiring to make sure that there is no signs of ageing, alteration, overheating, scaling and deformation ESPM 2052110:
     (a) On the AC/DC feeder routes: 1G, 2G, 4G and 6G.
     (b) On the AC/DC power-distribution routes: 1P, 2P and 6P.
     (c) On the flight control wiring.
     (d) On the engine control routes: 1S and 2S.
     (e) On the other routes: 1M, 2M and 6M.
     (f) On the audio route: 1R.
     (g) On the coaxial wiring routes: 3T and 4T.
     (h) On the generator excitation routes: 1E, 2E, 3E and 6E.
NOTE: Use a FLASHLIGHT or a MIRROR - INSPECTION, FLEXIBLE if necessary.
   (2) Make sure that there is no dust, lint or hydraulic contamination.
5. Close-up
Subtask 24-92-00-410-151-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 813, if installed.
   (3) Close the access doors 812 822 824 (Ref. AMM TASK 52-41-00-410-002).
   (4) Close the forward passenger/crew door 831 (Ref. AMM TASK 52-10-00-410-001).
   (5) Remove the access platform(s).
[Rev.8 from Aug 2017] 2026.03.31 23:26:57 UTC