Installation of the AC Essential Bus Switching Contactor
TASK 24-25-55-400-001-A
Installation of the AC Essential Bus Switching Contactor
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 24-25-55-860-050-A
Subtask 24-25-55-420-050-A
Subtask 24-25-55-410-050-A
[Rev.10 from 2021]
2026.03.31 23:22:51 UTC
Installation of the AC Essential Bus Switching Contactor
WARNING:
MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT ELECTRICAL CIRCUITS.
THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 0.176 and 0.147 m.daN (15.58 and 13.01 lbf.in ) ![]() |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 125 | LATERAL AVIONIC COMPARTMENT |
| 812 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-25-00-710-001-A | Operational Check of AC ESS Generation Switching |
Subtask 24-25-55-860-050-A
A. Aircraft Maintenance Configuration
(1) In the cockpit, on the overhead panel 35VU, make sure that these puhbutton switches are released:
(4) On the access door 121AL, make sure that the WARNING NOTICE(S) is in position to tell persons not to connect the external power connector.
(5) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 812.
(6) Make sure that the access door 812 is open.
(7) In the avionics compartment, make sure that the access door (14) is removed from the panel 106VU.
Subtask 24-25-55-865-050-A (1) In the cockpit, on the overhead panel 35VU, make sure that these puhbutton switches are released:
- BAT 1, BAT 2,
- GEN 1, GEN 2,
- EXT A.
- 35VU (ELEC),
- 21VU (EMER ELEC PWR).
(4) On the access door 121AL, make sure that the WARNING NOTICE(S) is in position to tell persons not to connect the external power connector.
(5) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 812.
(6) Make sure that the access door 812 is open.
(7) In the avionics compartment, make sure that the access door (14) is removed from the panel 106VU.
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 | |||
| 105VU | ELEC/CSM/G /EV AUTO/SPLY | 7XE | C01 |
| 106VU | CSM/G /EV/MAN/SPLY | 6XE | B04 |
| 106VU | ESS TR/SPLY | 4PE | C01 |
| 122VU | ELEC/CNTOR/ESS/DC BUS/TIE | 3PC | W26 |
| 123VU | AC ESS/BUS ON/BUS 1 | 1XC | AC12 |
| 123VU | AC ESS/BUS ON/BUS 2 | 2XC | AC01 |
Subtask 24-25-55-420-050-A
A. Installation of the Contactor
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Put the contactor (8) in position on the studs (11).
(4) Install the washers (9) and the nuts (7), then tighten the nuts.
(5) Install the electrical wires:
(b) Install the plates (5) and (10), the spring washers (4) and the nuts (3),
(c) TORQUE the nuts (3) to between 0.176 and 0.147 m.daN (15.58 and 13.01 lbf.in )
.
(6) Remove the CAP-BLANKING from each electrical connector and receptacle.
(7) Make sure that all the electrical connections are clean and in the correct condition.
(8) Connect the 2 electrical connectors (1, 2).
Subtask 24-25-55-865-051-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 contactor (8) in position on the studs (11).
(4) Install the washers (9) and the nuts (7), then tighten the nuts.
(5) Install the electrical wires:
CAUTION:
REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU CONNECT THE ELECTRICAL WIRES.
INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
(a) Install the electrical power-supply wires (6). (b) Install the plates (5) and (10), the spring washers (4) and the nuts (3),
(c) TORQUE the nuts (3) to between 0.176 and 0.147 m.daN (15.58 and 13.01 lbf.in )
. (6) Remove the CAP-BLANKING from each electrical connector and receptacle.
(7) Make sure that all the electrical connections are clean and in the correct condition.
(8) Connect the 2 electrical connectors (1, 2).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 24-25-55-710-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 105VU | ELEC/CSM/G /EV AUTO/SPLY | 7XE | C01 |
| 106VU | CSM/G /EV/MAN/SPLY | 6XE | B04 |
| 106VU | ESS TR/SPLY | 4PE | C01 |
| 122VU | ELEC/CNTOR/ESS/DC BUS/TIE | 3PC | W26 |
| 123VU | AC ESS/BUS ON/BUS 1 | 1XC | AC12 |
| 123VU | AC ESS/BUS ON/BUS 2 | 2XC | AC01 |
C. Do an operational test of the AC essential generation switching (Ref. AMM TASK 24-25-00-710-001).
5. Close-upSubtask 24-25-55-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the access door (14) on the panel 106VU.
(3) Remove the WARNING NOTICE(S).
(4) Close the access door 812.
(5) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the access door (14) on the panel 106VU.
(3) Remove the WARNING NOTICE(S).
(4) Close the access door 812.
(5) Remove the access platform(s).
Contactor