W DOC AIRBUS | AMM A320F

Removal of the Laptop Docking Station (LDS)


TASK 46-26-34-000-001-A
Removal of the Laptop Docking Station (LDS)


ZONE: 122
ZONE: 212
FIN: 39TA1 ** ON A/C NOT FOR ALL
FIN: 39TA2 ** 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
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
122
AVIONICS COMPARTMENT
212
COCKPIT
 C. Referenced Information
REFERENCE
DESIGNATION
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)
3. Job Set-up
Subtask 46-26-34-861-050-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 46-26-34-865-050-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 39TA1 (DOCKING STATIONEFB LAPTOP)
122VUEFB/CAPT41TA1U08
FOR FIN: 39TA2 (DOCKING STATIONEFB LAPTOP)
49VUEFB/F/O41TA2H09
4. Procedure
Subtask 46-26-34-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the EFB LDS
NOTE: The laptop must be removed from the EFB LDS before the removal of the EFB LDS.
   (1) FOR [39TA2] (DOCKING STATION-EFB LAPTOP)
     (a) Get access to the Avionics Compartment.
     (b) Disconnect the connectors P3 (5) and P1 (6).
     (c) Get access to the cockpit.
     (d) Remove the six screws (3) and the plate (4).
     (e) Disconnect the connector P2 (2).
     (f) Remove the eight screws (9) and washers (10) from the EFB LDS (11).
     (g) Pull the harnesses (2), (5) and (6) outside the lateral console.
     (h) Remove the F/O EFB LDS.
   (2) FOR [39TA1] (DOCKING STATION-EFB LAPTOP)
     (a) Get access to the Avionics Compartment.
     (b) Disconnect the connectors P3 (7) and P1 (8).
     (c) Get access to the cockpit.
     (d) Remove the six screws (3) and the plate (4).
     (e) Disconnect the connector P2 (1).
     (f) Remove the eight screws (9) and washers (10) from the EFB LDS (11).
     (g) Pull the harnesses (1), (7) and (8) outside the lateral console.
     (h) Remove the CAPT EFB LDS.
[Rev.10 from 2021] 2026.04.02 06:26:09 UTC