Installation of the AC ESS BUS Contactor
TASK 24-24-55-400-002-A
Installation of the AC ESS BUS 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 24-24-55-860-053-A
Subtask 24-24-55-420-051-A
Subtask 24-24-55-410-051-A
[Rev.10 from 2021]
2026.03.31 23:22:46 UTC
Installation of the AC ESS BUS 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 | AR | 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, 822 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-24-00-710-001-A | Operational Check of Emergency Generating System |
| TASK 24-28-00-710-001-A | Operational Test of the Static Inverter when the Aircraft Electrical Circuits are Energized from the External Power |
| TASK 24-28-00-710-001-A-01 | Operational Test of the Static Inverter when the Aircraft Electrical Circuits are Energized from the APU |
Subtask 24-24-55-860-053-A
A. Aircraft Maintenance Configuration
(1) In the cockpit, on the overhead panel 35VU, make sure that these pushbutton switches are released:
(4) Make sure that there is a WARNING NOTICE(S) on the access door 121AL to tell persons not to connect the external power connector.
(5) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE are in position at the access doors 812 and 822.
(6) Make sure that the access doors 812 and 822 are open.
(7) In the avionics compartment, make sure that the access panel (13) of the AC/DC emergency power center 106VU is open.
Subtask 24-24-55-865-054-A (1) In the cockpit, on the overhead panel 35VU, make sure that these pushbutton switches are released:
- BAT 1, BAT 2,
- GEN 1(2), APU GEN,
- EXT PWR.
- 21VU (EMER ELEC PWR),
- 35VU (ELEC).
(4) Make sure that there is a WARNING NOTICE(S) on the access door 121AL to tell persons not to connect the external power connector.
(5) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE are in position at the access doors 812 and 822.
(6) Make sure that the access doors 812 and 822 are open.
(7) In the avionics compartment, make sure that the access panel (13) of the AC/DC emergency power center 106VU is open.
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 | |||
| 106VU | AC ESS/BUS/EMER/CNTOR/SPLY | 15PC | C08 |
| 106VU | AC ESS BUS/EMER/STBY/CNTOR/SPLY | 10XE | C06 |
Subtask 24-24-55-420-051-A
A. Installation of the Contactor
(2) Install the washers (1) and the nuts (12). Tighten the nuts.
(3) Install the crimped lugs (10) with the shunts (11).
(4) Install the retaining washers (9).
(5) Install the power supply wires (8).
(6) Install the washers (7) and the nuts (6). Tighten the nuts (6).
(7) TORQUE the nuts (6) to between 0.176 and 0.147 m.daN (15.58 and 13.01 lbf.in )
.
(8) Remove the CAP-BLANKING from each electrical connector and receptacle.
(9) Make sure that all the electrical connections are clean and in the correct condition.
(10) Connect the two electrical connectors (5).
Subtask 24-24-55-865-055-A 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.
(1) Put the contactor (2) in position on the studs (3). (2) Install the washers (1) and the nuts (12). Tighten the nuts.
(3) Install the crimped lugs (10) with the shunts (11).
(4) Install the retaining washers (9).
(5) Install the power supply wires (8).
(6) Install the washers (7) and the nuts (6). Tighten the nuts (6).
(7) TORQUE the nuts (6) to between 0.176 and 0.147 m.daN (15.58 and 13.01 lbf.in )
. (8) Remove the CAP-BLANKING from each electrical connector and receptacle.
(9) Make sure that all the electrical connections are clean and in the correct condition.
(10) Connect the two electrical connectors (5).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 24-24-55-710-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 106VU | AC ESS/BUS/EMER/CNTOR/SPLY | 15PC | C08 |
| 106VU | AC ESS BUS/EMER/STBY/CNTOR/SPLY | 10XE | C06 |
C. Operational Tests
(1) Do the operational test of the emergency generation system (Ref. AMM TASK 24-24-00-710-001).
(2) Do the operational test of the static inverter (Ref. AMM TASK 24-28-00-710-001).
5. Close-up(1) Do the operational test of the emergency generation system (Ref. AMM TASK 24-24-00-710-001).
(2) Do the operational test of the static inverter (Ref. AMM TASK 24-28-00-710-001).
Subtask 24-24-55-410-051-A
Contactor