W DOC AIRBUS | AMM A320F

Installation of the Cables

TASK 36-22-16-400-008-A
Installation of the Cables

WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
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: 25HF
FIN: 41HF
FIN: 52HF
FIN: 68HF
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
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.68 and 0.56 m.daN (60.18 and 49.56 lbf.in ) T
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(Material No.14SBA1)
Textile-Lint free Cotton -
No specific
NSA936809RG0001
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
500
LEFT WING
600
RIGHT WING
FOR [25HF] (CABLE-CONNECTING, L WING LOOP A)
FOR [52HF] (CABLE-CONNECTING, L WING LOOP B)
522EB, 522FB
FOR [41HF] (CABLE-CONNECTING, R WING LOOP A)
FOR [68HF] (CABLE-CONNECTING, R WING LOOP B)
622EB, 622FB
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 36-22-00-710-001-A
Operational Test of the Overheat Detection System
TASK 36-22-00-710-802-A
Operational Test of the Overheat Detection System
ESPM 2043120
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
3. Job Set-up
Subtask 36-22-16-941-060-A
A. Safety Precautions
   (1) Make sure that the SAFETY BARRIER(S) are in position.
   (2) Make sure that the WARNING NOTICE(S) is in position in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-077-A
B. Aircraft Maintenance Configuration
   (1) Make sure that the slats are fully extended (Ref. AMM TASK 27-80-00-866-004).
   (2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever on panel 114VU.
   (3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position below the applicable access panels.
   (4) Make sure that the applicable access panels are removed:
     (a) FOR [25HF] (CABLE-CONNECTING, L WING LOOP A), [52HF] (CABLE-CONNECTING, L WING LOOP B)
panels 522EB 522FB
     (b) FOR [41HF] (CABLE-CONNECTING, R WING LOOP A), [68HF] (CABLE-CONNECTING, R WING LOOP B)
panels 622EB 622FB.
Subtask 36-22-16-865-075-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
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
4. Procedure
Subtask 36-22-16-420-064-A
A. Preparation for Installation
   (1) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Examine the cable assembly (15) and/or (16) for the correct condition.
   (5) Remove the blanking caps from the cable assembly (15) or (16) connectors and examine the connectors for the correct condition. Put the blanking caps on the connectors again.
Subtask 36-22-16-420-056-A
B. Installation 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: 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) Install the cable (15) or (16).
   (2) Remove the blanking caps from the connectors (23) and (24).
   (3) Install the connector (23) in the flanged attachment (21).
   (4) Install the nut (20) on the connector (23).
   (5) TORQUE the nut (20) to between 0.68 and 0.56 m.daN (60.18 and 49.56 lbf.in ) T.
   (6) For the cable 25HF(41HF):
  • connect the connector (24) to the connector (22).
   (7) For the cable 52HF(68HF):
  • connect the connector (19) to the connector (23).
   (8) TORQUE the connectors (19) and (23) to between 0.68 and 0.56 m.daN (60.18 and 49.56 lbf.in ) T.
   (9) Safety the connectors (19), (22), (23) and (24) and the nuts (20) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (10) Cut the cable (15) or (16) to the correct length and connect it to the electrical cable (15) or (16) with the in-line splice NSA936809RG0001 ESPM 2043120.
   (11) Install the cable (15) or (16) in the applicable electrical raceway:

     (a) FOR [25HF] (CABLE-CONNECTING, L WING LOOP A), [41HF] (CABLE-CONNECTING, R WING LOOP A)
in route 1S
     (b) FOR [52HF] (CABLE-CONNECTING, L WING LOOP B), [68HF] (CABLE-CONNECTING, R WING LOOP B)
in route 2S.
   (12) Install the clamps (33) on the cable (15) or (16) and install the bolts (35).
Subtask 36-22-16-865-076-A
C. Remove the safety clip(s) and the tag(s) and close 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
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
** 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 36-22-16-710-056-A ** ON A/C NOT FOR ALL
D. Test
   (1) Do an operational test of the overheat detection system (Ref. AMM TASK 36-22-00-710-001).
Subtask 36-22-16-710-056-B ** ON A/C NOT FOR ALL
D. Operational Test
   (1) Do an operational test of the overheat detection system (Ref. AMM TASK 36-22-00-710-802).
5. Close-up
Subtask 36-22-16-410-056-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the applicable access panels:
     (a) FOR [25HF] (CABLE-CONNECTING, L WING LOOP A), [52HF] (CABLE-CONNECTING, L WING LOOP B)
install 522EB 522FB
     (b) FOR [41HF] (CABLE-CONNECTING, R WING LOOP A), [68HF] (CABLE-CONNECTING, R WING LOOP B)
install 622EB 622FB.
Subtask 36-22-16-865-077-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 36-22-16-860-076-A
C. Aircraft Configuration
   (1) Fully retract the slats (Ref. AMM TASK 27-80-00-866-005).
Subtask 36-22-16-942-056-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 01:17:09 UTC
"Aviabrain" 2025