W DOC AIRBUS | AMM A320F

Removal of the Cables

TASK 36-22-16-000-003-A
Removal of the Cables

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
ZONE: 500
ZONE: 600
FIN: 24HF
FIN: 40HF
FIN: 51HF
FIN: 67HF
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
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
500
LEFT WING
600
RIGHT WING
FOR [24HF] (CABLE-CONNECTING, L WING LOOP A)
FOR [51HF] (CABLE-CONNECTING, L WING LOOP B)
522YB
522AB
FOR [40HF] (CABLE-CONNECTING, R WING LOOP A)
FOR [67HF] (CABLE-CONNECTING, R WING LOOP B)
622AB
622YB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
F Overheat Sensing Elements and Cables - Access Panels ** ON A/C NOT FOR ALL
F Overheat Sensing Elements
F Overheat Sensing Elements and Cables - Access Panels ** ON A/C NOT FOR ALL
F Overheat Sensing Elements
F Overheat Sensing Elements - Typical Assemblies
FOR [24HF] (CABLE-CONNECTING, L WING LOOP A)
FOR [51HF] (CABLE-CONNECTING, L WING LOOP B)
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
FOR [40HF] (CABLE-CONNECTING, R WING LOOP A)
FOR [67HF] (CABLE-CONNECTING, R WING LOOP B)
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
3. Job Set-up
Subtask 36-22-16-941-052-A
A. Safety Precautions
   (1) Put the SAFETY BARRIER(S) in position.
   (2) Put a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-059-A
B. Aircraft Maintenance Configuration
   (1) Extend the slats fully (Ref. AMM TASK 27-80-00-866-004).
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever on panel 114VU.
Subtask 36-22-16-865-052-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-22-16-010-052-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panel.
   (2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004):
     (a) FOR [24HF] (CABLE-CONNECTING, L WING LOOP A), [51HF] (CABLE-CONNECTING, L WING LOOP B)
remove 522AB
     (b) FOR [40HF] (CABLE-CONNECTING, R WING LOOP A), [67HF] (CABLE-CONNECTING, R WING LOOP B)
remove 622AB.
Subtask 36-22-16-010-052-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panel.
   (2) Remove the applicable access panel(s):
     (a) FOR [24HF] (CABLE-CONNECTING, L WING LOOP A), [51HF] (CABLE-CONNECTING, L WING LOOP B)
     (b) FOR [40HF] (CABLE-CONNECTING, R WING LOOP A), [67HF] (CABLE-CONNECTING, R WING LOOP B)
4. Procedure
Subtask 36-22-16-020-052-A
A. Removal of the Cables
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
CAUTION: MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
   (1) Remove the bolts (32) and the clamps (31) from the cable (13) or (18).
   (2) Remove the applicable cable (13) or (18) from the electrical raceway.
   (3) Cut the applicable electrical cable (13) or (18) at the in-line splice connector.
     (a) For the cable 24HF:
  • at the connector 4015VS in route 1S.
     (b) For the cable 40HF:
  • at the connector 4014VS in route 1S.
     (c) For the cable 51HF:
  • at the connector 4023VS in route 2S.
     (d) For the cable 67HF:
  • at the connector 4022VS in route 2S.
   (4) Remove and discard the lockwire from the connectors (19), (23) and (24) and the nut (20).
   (5) For the cable 24HF(40HF):
     (a) Disconnect the connector (19) from the connector (23).
     (b) Remove the nut (20) from the connector (23).
     (c) Remove the connector (23) from the flanged attachment (21).
   (6) For the cable 51HF(67HF):
     (a) Disconnect the connector (24) from the connector (22).
   (7) Remove the applicable cable (13) or (18).
   (8) Put CAP - BLANKING on the disconnected connectors.
[Rev.10 from 2021] 2026.04.01 01:17:05 UTC
"Aviabrain" 2025