W DOC AIRBUS | AMM A320F

Installation of the Termination Box


TASK 23-73-43-400-001-A
Installation of the Termination Box


FIN: 209RH1 ** ON A/C NOT FOR ALL
FIN: 209RH2 ** ON A/C NOT FOR ALL
FIN: 309RH1 ** ON A/C NOT FOR ALL
FIN: 309RH2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self Explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
STEPLADDER 0.5 M (1.6 FT)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [209RH1] (DEU TERMINATION BOX)
FOR [209RH2] (DEU TERMINATION BOX)
251ZW, 252ZW
FOR [309RH1] (DEU TERMINATION BOX)
FOR [309RH2] (DEU TERMINATION BOX)
261DF
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 23-73-00-740-005-B
Interface and Power-Up Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
TASK 23-73-00-861-001-A
Energize the Cabin Intercommunication Data System (CIDS)
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
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 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 26-10-00-740-801-A
BITE Test of the Smoke Detection Function - System Test
ASM 237305
ASM 237321
FOR [209RH1] (DEU TERMINATION BOX)
FOR [209RH2] (DEU TERMINATION BOX)
TASK 25-23-48-000-001-A
Removal of the Cove Light Panel
TASK 25-23-48-400-001-A
Installation of the Cove Light Panel
FOR [309RH1] (DEU TERMINATION BOX)
FOR [309RH2] (DEU TERMINATION BOX)
TASK 25-23-42-000-002-A
Removal of the Ceiling Panels - Aft Utility Area
TASK 25-23-42-400-002-A
Installation of the Ceiling Panels - Aft Utility Area
3. Job Set-up
Subtask 23-73-43-860-050-C ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
   (1) Make sure that the STEPLADDER 0.5 M (1.6 FT) is below the related access panel.
   (2) FOR [209RH1] (DEU TERMINATION BOX), [209RH2] (DEU TERMINATION BOX)
Make sure that the cove light panels 251ZW and 252ZW (Ref. AMM TASK 25-23-48-000-001) are removed.
   (3) FOR [309RH1] (DEU TERMINATION BOX), [309RH2] (DEU TERMINATION BOX)
Make sure that the aft utility area - ceiling panel 261DF (Ref. AMM TASK 25-23-42-000-002) is removed.
Subtask 23-73-43-860-050-D ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-42-00-861-001)
   (1) Make sure that the EMER EXIT LT switch 4WL on the overhead panel 25VU is in the OFF position.
   (2) Make sure that the STEPLADDER 0.5 M (1.6 FT) is below the related access panel.
   (3) FOR [209RH1] (DEU TERMINATION BOX), [209RH2] (DEU TERMINATION BOX)
Make sure that the cove light panels 251ZW and 252ZW (Ref. AMM TASK 25-23-48-000-001) are removed.
   (4) FOR [309RH1] (DEU TERMINATION BOX), [309RH2] (DEU TERMINATION BOX)
Make sure that the aft utility area - ceiling panel 261DF (Ref. AMM TASK 25-23-42-000-002) is removed.
Subtask 23-73-43-865-051-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DEU B/ESS153RHG03
49VUCOM/CIDS/DEU A ESS/AFT R172RHHA12
49VUCOM/CIDS/DEU A ESS/AFT L179RHHA11
49VUCOM/CIDS/DEU A ESS/FWD R158RHHA10
49VUCOM/CIDS/DEU A ESS/FWD L159RHHA09
** ON A/C NOT FOR ALL
49VUCOM / CIDS / DEU A ESS / MID R196RHG05
49VUCOM / CIDS / DEU A ESS / MID L195RHG04
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DEU B ESS/R420RHG05
49VUCOM/CIDS/DEU B ESS/L419RHG04
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/R AFT168RHM12
121VUCOM NAV/CIDS/DEU A NORM/L AFT167RHM11
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM10
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM09
121VUCOM NAV/CIDS/DEU B/NORM162RHM08
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM11
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM10
121VUCOM / CIDS / DEU B / NORM FWD193RHM09
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU B NORM/R620RHM08
121VUCOM NAV/CIDS/DEU B NORM/L619RHM07
121VUCOM/CIDS/DEU B BAT/R720RHQ11
121VUCOM/CIDS/DEU B BAT/L719RHQ10
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DEU A BAT/FWD R258RHN14
121VUCOM/CIDS/DEU A BAT/L FWD259RHN13
121VUCOM/CIDS/DEU B/BAT143RHN12
121VUCOM/CIDS/DEU A BAT/AFT R272RHQ11
121VUCOM/CIDS/DEU A BAT/AFT L279RHQ10
** ON A/C NOT FOR ALL
121VUDEU A BAT MID R296RHM13
121VUDEU A BAT MID L295RHM12
** ON A/C NOT FOR ALL
2001VUCIDS-DEU B-NORM-AFT194RHC08
2001VUCIDS-DEU A NORM-AFT-RH174RHC07
2001VUCIDS-DEU A NORM-AFT-LH173RHC06
2001VUCIDS-DEU A NORM-MID-RH198RHC05
2001VUCIDS-DEU A NORM-MID-LH197RHC04
4. Procedure
Subtask 23-73-43-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Termination Box
F Termination Box DEU Type A/B ** ON A/C NOT FOR ALL
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Connect the termination box (3) to the DEU (1) and tighten the nylatches (4).
   (4) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (5) Make sure that all the electrical connections are clean and in the correct condition.
   (6) Make sure that the coding switches are in the positions recorded during the removal procedure. For the correct position of the DEU coding switches, please refer to ASM 237305 ASM 237321.
NOTE: It is mandatory to set the position of the coding switches correctly. An incorrect position of the coding switches causes incorrect CIDS operation. Because of this, there can be fault messages related to the CIDS and/or the related DEU. When there are no fault messages you cannot be sure that all coding switches are in the correct position.
   (7) Connect the electrical connector (2) to the termination box (3).
   (8) Safety the electrical connector (2).
CAUTION: MAKE SURE THAT THE SPRING LATCHES CORRECTLY HOLD THE CONNECTOR IN THE FULLY ENGAGED POSITION. THE SPRING LATCHES PREVENT UNWANTED MOVEMENT OF THE CONNECTOR, AND THUS THE RISK OF ARCING, WHICH CAN CAUSE DAMAGE TO THE UNIT.
     (a) Safety the electrical connector (2) with the spring latches (5).
Subtask 23-73-43-865-052-A ** ON A/C NOT FOR ALL
B. Remove the safety clips and tags and close these circuit breakers in this sequence:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2001VUCIDS-DEU A NORM-MID-RH198RHC05
2001VUCIDS-DEU A NORM-MID-LH197RHC04
2001VUCIDS-DEU B-NORM-AFT194RHC08
121VUCOM / CIDS / DEU B / NORM FWD193RHM09
2001VUCIDS-DEU A NORM-AFT-RH174RHC07
2001VUCIDS-DEU A NORM-AFT-LH173RHC06
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/R AFT168RHM12
121VUCOM NAV/CIDS/DEU A NORM/L AFT167RHM11
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM11
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/R FWD164RHM10
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM10
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU A NORM/L FWD163RHM09
121VUCOM NAV/CIDS/DEU B/NORM162RHM08
** ON A/C NOT FOR ALL
121VUCOM NAV/CIDS/DEU B NORM/L619RHM07
121VUCOM NAV/CIDS/DEU B NORM/R620RHM08
** ON A/C NOT FOR ALL
49VUCOM / CIDS / DEU A ESS / MID R196RHG05
49VUCOM / CIDS / DEU A ESS / MID L195RHG04
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DEU A ESS/AFT L179RHHA11
49VUCOM/CIDS/DEU A ESS/AFT R172RHHA12
49VUCOM/CIDS/DEU A ESS/FWD L159RHHA09
49VUCOM/CIDS/DEU A ESS/FWD R158RHHA10
49VUCOM/CIDS/DEU B/ESS153RHG03
** ON A/C NOT FOR ALL
49VUCOM/CIDS/DEU B ESS/L419RHG04
49VUCOM/CIDS/DEU B ESS/R420RHG05
** ON A/C NOT FOR ALL
121VUDEU A BAT MID R296RHM13
121VUDEU A BAT MID L295RHM12
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DEU A BAT/AFT L279RHQ10
121VUCOM/CIDS/DEU A BAT/AFT R272RHQ11
121VUCOM/CIDS/DEU A BAT/L FWD259RHN13
121VUCOM/CIDS/DEU A BAT/FWD R258RHN14
121VUCOM/CIDS/DEU B/BAT143RHN12
** ON A/C NOT FOR ALL
121VUCOM/CIDS/DEU B BAT/L719RHQ10
121VUCOM/CIDS/DEU B BAT/R720RHQ11
Subtask 23-73-43-869-050-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
   (2) Do the BITE test of the Cabin Intercommunication Data System (CIDS) through the CFDS
(Ref. AMM TASK 23-73-00-740-005).
Subtask 23-73-43-740-050-A ** ON A/C NOT FOR ALL
D. Do the BITE test of the smoke detection function - system test
(Ref. AMM TASK 26-10-00-740-801).
5. Close-up
Subtask 23-73-43-410-050-B ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) FOR [209RH1] (DEU TERMINATION BOX), [209RH2] (DEU TERMINATION BOX)
Install the cove light panels 251ZW and 252ZW (Ref. AMM TASK 25-23-48-400-001).
   (3) FOR [309RH1] (DEU TERMINATION BOX), [309RH2] (DEU TERMINATION BOX)
Install the aft utility area - ceiling panel 261DF (Ref. AMM TASK 25-23-42-400-002).
   (4) Remove the STEPLADDER 0.5 M (1.6 FT).
Subtask 23-73-43-862-050-A ** ON A/C NOT FOR ALL
B. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.04.02 06:12:34 UTC