Installation of the Power Supply Unit
TASK 33-48-37-400-001-A
Installation of the Power Supply Unit
Self explanatory
2. Job Set-up Information
A. Consumable Materials
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 33-48-37-860-051-A
Subtask 33-48-37-420-050-A
Subtask 33-48-37-410-050-A
[Rev.10 from 2021]
2026.04.01 00:56:44 UTC
Installation of the Power Supply Unit
FIN: 4LV
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Consumable Materials
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.04QAB2) | Coating_- Flexible Structure |
| No specific | lockwire - corrosion resistant steel 0.6mm (0.24 in.) dia. |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 191HB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| TASK 33-48-00-710-001-A | Operational Test of the Anti-Collision Lighting |
| TASK 53-35-13-400-002-A | Installation of the Quick-Release Access Panels on the Belly Fairing Structure |
Subtask 33-48-37-860-051-A
A. Aircraft Maintenance Configuration
(1) Make sure that switch 2LV BEACON ON-OFF on overhead panel 25VU is in the OFF position.
(2) Make sure that access panel 191HB at the belly fairing is removed.
Subtask 33-48-37-865-051-A (1) Make sure that switch 2LV BEACON ON-OFF on overhead panel 25VU is in the OFF position.
(2) Make sure that access panel 191HB at the belly fairing is removed.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | LIGHTING/EXT LT/BEACON/LOWER | 5LV | U03 |
Subtask 33-48-37-420-050-A
A. Installation of the Power Supply Unit
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Put the power supply unit (1) in position on the fuselage.
(4) Install the washers (3) and the screws (4) and (6).
(5) Apply a thin layer of Coating_- Flexible Structure (Material No.04QAB2) on the screw (6) (Ref. AMM TASK 20-28-00-912-802).
(6) Remove the CAP-BLANKING from each electrical connector and receptacle.
(7) Connect the electrical connectors (2) and (5) to the power supply unit (1).
Subtask 33-48-37-865-052-A (1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Put the power supply unit (1) in position on the fuselage.
(4) Install the washers (3) and the screws (4) and (6).
(5) Apply a thin layer of Coating_- Flexible Structure (Material No.04QAB2) on the screw (6) (Ref. AMM TASK 20-28-00-912-802).
(6) Remove the CAP-BLANKING from each electrical connector and receptacle.
(7) Connect the electrical connectors (2) and (5) to the power supply unit (1).
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.
CAUTION:
MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.
(8) Safety the electrical connector (5) with lockwire - corrosion resistant steel 0.6mm (0.24 in.) dia.NOTE: It is not necessary to safety the connector with the lockwire, if it is a self-locking connector.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 33-48-37-710-050-A 5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | LIGHTING/EXT LT/BEACON/LOWER | 5LV | U03 |
Subtask 33-48-37-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install access panel 191HB on the belly fairing (Ref. AMM TASK 53-35-13-400-002).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install access panel 191HB on the belly fairing (Ref. AMM TASK 53-35-13-400-002).
Power Supply Unit 4LV