W DOC AIRBUS | AMM A320F

Deactivation of the Protection Panel(s) for the Decompression Panel(s) at the Forward Partition


TASK 25-54-00-040-801-A
Deactivation of the Protection Panel(s) for the Decompression Panel(s) at the Forward Partition


ZONE: 130
Task Summary
Access Test Specific Tools Mhr E/T Nb Men
NONONO0.50.51
1. Reason for the Job
MMEL 25-50-07A
PROTECTION PANELS OF DECOMPRESSION PANELS AT THE FWD PARTITION WALL OF FWD CARGO COMPARTMENT (IF INSTALLED)
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
130
FWD CARGO COMPT AFT BULKHEAD OF AVNCS COMPT TO FWD PRESSURE BULKHEAD OF WING CENTER BOX
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 25-50-00-200-024-A
Cargo Compartment Linings with Honeycomb Core - General Repair/Protection Information
TASK 25-54-11-000-001-A
Removal of the Forward Cargo-Compartment Partition FR24A
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-002-A
Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
3. Job Set-up
Subtask 25-54-00-860-050-A
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
   (2) Open the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-001).
   (3) Put a ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the opening of the forward cargo-compartment door.
   (4) Set the light switch to on.
   (5) Put a WARNING NOTICE(S) in position on the control panel of the forward cargo-compartment loading-system to tell persons not to use it.
Subtask 25-54-00-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUSEMI AUTO CLS-FWD3MYE08
2000VUSEMI AUTO CLS-FWD2MYE06
4. Procedure
Subtask 25-54-00-040-050-A
A. Deactivation of the Protection Panels
   (1) Identify the protection panel(s) damage limits (Ref. AMM TASK 25-50-00-200-024).
   (2) If the damage prevents correct operation of the decompression panel(s):
     (a) Remove the related protection panel(s) (Ref. AMM TASK 25-54-11-000-001).
     (b) Remove all cargo load between the forward partition at frame 24A and the nearest divider net.
5. Close-up
Subtask 25-54-00-865-051-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
2000VUSEMI AUTO CLS-FWD3MYE08
2000VUSEMI AUTO CLS-FWD2MYE06
Subtask 25-54-00-860-051-A
B. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the WARNING NOTICE(S).
   (3) Set the light switch to off.
   (4) Remove the access platform(s).
   (5) Close the forward cargo-compartment door (Ref. AMM TASK 52-30-00-860-002).
   (6) Make an entry in the logbook.
   (7) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.03.31 23:38:51 UTC