Installation of the Contactor
TASK 24-35-55-400-001-A
Installation of the 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 24-35-55-860-051-A
Subtask 24-35-55-420-050-A ** ON A/C NOT FOR ALL
Subtask 24-35-55-410-050-A
[Rev.10 from 2021]
2026.04.01 05:53:49 UTC
Installation of the 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 | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 41.6 and 33.63 lbf.in (0.47 and 0.38 m.daN ) ![]() |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 212 | COCKPIT |
| 121AL |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-32-00-710-001-A | Operational Test of the DC Generation Switching |
| TASK 25-11-41-000-001-A | Removal of the Third Occupant Seat |
| TASK 25-11-41-400-001-A | Installation of the Third Occupant Seat |
Subtask 24-35-55-860-051-A
A. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position at the access door 121AL.
(2) Make sure that the access door 121AL is open.
(3) Make sure that the external power connector is not connected to the aircraft receptacle.
(4) Make sure that, on the access door 121AL, there is a WARNING NOTICE(S) to tell persons not to connect the external power connector.
(5) In the cockpit, on the overhead panel 35VU, make sure that these pushbutton switches are released:
(8) In the cockpit, make sure that the third occupant seat is removed (Ref. AMM TASK 25-11-41-000-001).
(9) In the cockpit, make sure that the front panel on the bottom right side of the panel 120VU is removed.
4. Procedure(1) Make sure that the access platform is in position at the access door 121AL.
(2) Make sure that the access door 121AL is open.
(3) Make sure that the external power connector is not connected to the aircraft receptacle.
(4) Make sure that, on the access door 121AL, there is a WARNING NOTICE(S) to tell persons not to connect the external power connector.
(5) In the cockpit, on the overhead panel 35VU, make sure that these pushbutton switches are released:
- BAT 1, BAT 2,
- APU GEN,
- GEN 1, GEN 2,
- EXT PWR.
- 21VU (EMER ELEC PWR),
- 35VU (ELEC).
(8) In the cockpit, make sure that the third occupant seat is removed (Ref. AMM TASK 25-11-41-000-001).
(9) In the cockpit, make sure that the front panel on the bottom right side of the panel 120VU is removed.
Subtask 24-35-55-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Contactor
(2) TORQUE the captive screws (3) to between 41.6 and 33.63 lbf.in (0.47 and 0.38 m.daN )
.
(3) Remove the CAP-BLANKING from each electrical connector and receptacle.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Connect the electrical connector (4) to the contactor (5).
Subtask 24-35-55-420-050-B ** ON A/C NOT FOR ALL CAUTION:
MAKE SURE THAT THE CONTACTOR LOCATING PIN IS CORRECTLY ENGAGED IN ITS RECESS LOCATED IN ONE POWER TERMINAL.
THIS PREVENTS DAMAGE TO THE LOCATING PIN WHEN YOU APPLY THE TORQUE.
(1) Install the contactor (5) on the tapped barrels (6) of the connecting base (1). (2) TORQUE the captive screws (3) to between 41.6 and 33.63 lbf.in (0.47 and 0.38 m.daN )
. (3) Remove the CAP-BLANKING from each electrical connector and receptacle.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Connect the electrical connector (4) to the contactor (5).
A. Installation of the Contactor
(2) TORQUE the captive screws (3) to between 41.6 and 33.63 lbf.in (0.47 and 0.38 m.daN )
.
(3) Remove the blanking caps from the electrical connector (4) and the electrical receptacle.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Connect the electrical connector (4) to the contactor (5).
Subtask 24-35-55-710-050-A CAUTION:
MAKE SURE THAT THE CONTACTOR LOCATING PIN IS CORRECTLY ENGAGED IN ITS RECESS LOCATED IN ONE POWER TERMINAL.
THIS PREVENTS DAMAGE TO THE LOCATING PIN WHEN YOU APPLY THE TORQUE.
(1) Install the contactor (5) on the module 13PN (14PN) (1). (2) TORQUE the captive screws (3) to between 41.6 and 33.63 lbf.in (0.47 and 0.38 m.daN )
. (3) Remove the blanking caps from the electrical connector (4) and the electrical receptacle.
(4) Make sure that all the electrical connections are clean and in the correct condition.
(5) Connect the electrical connector (4) to the contactor (5).
B. Operational Test of DC Generation Switching
(1) Do the operational test of DC Generation Switching (Ref. AMM TASK 24-32-00-710-001).
5. Close-up(1) Do the operational test of DC Generation Switching (Ref. AMM TASK 24-32-00-710-001).
Subtask 24-35-55-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the front panel on the bottom right side of the panel 120VU.
(3) Install the Third Occupant seat (Ref. AMM TASK 25-11-41-400-001).
(4) Remove the WARNING NOTICE(S).
(5) Close the access door 121AL.
(6) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the front panel on the bottom right side of the panel 120VU.
(3) Install the Third Occupant seat (Ref. AMM TASK 25-11-41-400-001).
(4) Remove the WARNING NOTICE(S).
(5) Close the access door 121AL.
(6) Remove the access platform(s).
Contactors