Detailed Inspection of G, E and P Routes Installed in the Lateral Avionic Compartment (EWIS)

TASK 24-92-00-220-008-A
Detailed Inspection of G, E and P Routes Installed in the Lateral Avionic Compartment (EWIS)

ZONE: 125
ZONE: 126

1. Reason for the Job
Refer to the MPD TASK: 200125-06
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED IN THE LATERAL AVIONIC COMPARTMENT (EWIS)

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
TASK 53-00-00-000-801-A	Removal of the Floor Panels in the Cabin from FR12 to FR70
TASK 53-00-00-000-801-A-01	Removal of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Removal Procedure - Dry Sealing Concept)
TASK 53-00-00-000-801-A-02	Removal of the Cabin Floor Panels from FR12 to FR70 (Alternative Removal Procedure with the Skyflex Option)
TASK 53-00-00-400-801-A	Installation of the Floor Panels in the Cabin from FR12 to FR70
TASK 53-00-00-400-801-A-01	Installation of the Floor Panels in the Cabin from FR12 to FR70 (Alternative Installation Procedure - Dry Sealing Concept)
TASK 53-00-00-400-801-A-02	Installation of the Cabin Floor Panels from FR12 to FR70 (Alternative Installation Procedure with the Skyflex Option)
TASK 53-12-11-000-001-A	Removal of the Cockpit Floor Panels from FR1 thru FR12
TASK 53-12-11-400-001-A	Installation of the Cockpit Floor Panels from FR1 thru FR12
ESPM 2052120
AWM 942106
AWM 942120
AWM 942305
TASK 06-41-53-00	FUSELAGE-DESCRIPTION AND OPERATION
Lateral Avionic Compartment - Inspection Area - Zones 125-126

3. Job Set-up
Subtask 24-92-00-010-154-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 24-92-00-862-140-A

B. Make sure that the aircraft electrical circuits are de-energized
(Ref. AMM TASK 24-41-00-862-002).

4. Procedure
Subtask 24-92-00-410-169-A

A. Preparation for Detailed Inspection
(1) Remove the cockpit and cabin floor panels from FR9 to FR16 (Ref. AMM TASK 53-12-11-000-001) and (Ref. AMM TASK 53-00-00-000-801), (Ref. AMM D/O 06-41-53-00).

Subtask 24-92-00-220-058-A

B. Detailed Inspection of G, E and P Routes Installed in the Lateral Avionic Compartment
(1) Do a detailed inspection of the wiring to make sure that there is no signs of ageing, alteration, overheating, scaling and deformation ESPM 2052120:
(a) On the AC/DC feeder routes: 1G, 2G AWM 942305, 4G, 6G AWM 942106.
(b) On the AC/DC power-distribution routes: 1P, 2P and 6P AWM 942305, AWM 942106 and AWM 942120.
(c) On the generator excitation routes: 1E, 2E, 3E and 6E. AWM 942305, AWM 942106 and AWM 942120.

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 24-92-00-410-152-A

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the cockpit and cabin floor panels from FR9 to FR16 (Ref. AMM TASK 53-12-11-400-001) and (Ref. AMM TASK 53-00-00-400-801), (Ref. AMM D/O 06-41-53-00).
(3) Close the access door 813, if installed.
(4) Close the access doors 812 822 824 (Ref. AMM TASK 52-41-00-410-002).
(5) Close the forward passenger/crew door 831 (Ref. AMM TASK 52-10-00-410-001).
(6) Remove the access platform(s).

[Rev.10 from 2021] 2026.03.31 23:26:44 UTC