W DOC AIRBUS | AMM A320F

Special Detailed Inspection (ROTO) of AFT Cargo Compartment Door Skin Underneath Hinge Fittings at Selected Bolt Holes


TASK 52-32-11-200-003-A
Special Detailed Inspection (ROTO) of AFT Cargo Compartment Door Skin Underneath Hinge Fittings at Selected Bolt Holes


ZONE: 826
1. Reason for the Job
Refer to the MPD TASK: 523116-01
SPECIAL DETAILED INSPECTION (ROTO) OF AFT CARGO COMPARTMENT DOOR SKIN UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES
NOTE: The effectivity of this task is "ALL". To know if this task is applicable for your aircraft, refer to the MPD task applicability and the weight variant data given in the SRM introduction.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
826
AFT CARGO COMPARTMENT DOOR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 51-78-00-916-001-A
Application of Temporary Protection System (TPS)
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
TASK 52-32-11-100-001-A
Cleaning/Painting of AFT Cargo-Compartment Door
TASK 52-32-13-000-001-A
Removal of the Lining and Insulation
TASK 52-32-13-400-001-A
Installation of the Lining and Insulation
SRM 511100
NTM 523116
SRM 51730000
(for corrective action)
SRM 51740000
(for corrective action)
SRM 52300000
(for corrective action)
3. Job Set-up
Subtask 52-32-11-860-055-A
A. Aircraft Maintenance Configuration
   (1) Open the AFT cargo door and safety it with the support struts (Ref. AMM TASK 52-30-00-860-001).
   (2) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below the opened cargo door.
Subtask 52-32-11-865-054-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
122VUDOORS/CARGO1MJT12
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 52-32-11-010-052-A
C. Get Access
   (1) Remove the lining and the insulation of the cargo door (Ref. AMM TASK 52-32-13-000-001) to get access to the internal cargo door structure.
   (2) Remove the nuts, the washers and the countersunk-screws from the holes of the piano hinges that you must examine NTM 523116.
Subtask 52-32-11-860-064-A
D. Preparation of the Inspection Area
   (1) Make sure that the hinge fittings and their internal attachment areas are clean.
   (2) If necessary, clean the hinge fittings and their internal attachment areas (Ref. AMM TASK 52-32-11-100-001).
   (3) Do a visual inspection of the inspection area and look for damage.
   (4) Make sure that the holes for the removed countersunk-screws are clean and smooth.
4. Procedure
Subtask 52-32-11-250-050-A
A. Special Detailed Inspection (ROTO) of AFT Cargo Compartment Door Skin Underneath Hinge Fittings at Selected Bolt Holes
   (1) Do the eddy current test to inspect the selected holes of the hinge fittings and the door structure NTM 523116.
   (2) If you find damage:
     (a) Do an analysis of the damage SRM 511100 and record the direction and depth of the damage.
     (b) If possible, remove the corrosion SRM 51740000.
     (c) If possible, remove the minor damage SRM 51730000.
     (d) If the removal of the damage is not possible, repair the effected component SRM 52300000.
Subtask 52-32-11-916-054-A
B. Do the procedure for the application of the temporary protection system (Ref. AMM TASK 51-78-00-916-001).
5. Close-up
Subtask 52-32-11-410-052-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the removed countersunk-screws, the washers and the nuts at the inspected holes of the piano hinges.
   (3) Install the lining and the insulation of the cargo door (Ref. AMM TASK 52-32-13-400-001).
Subtask 52-32-11-865-055-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
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
122VUDOORS/CARGO1MJT12
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 52-32-11-860-056-A
C. Put the aircraft back to the serviceable condition.
   (1) Remove the support struts and close the AFT cargo door (Ref. AMM TASK 52-30-00-860-002).
   (2) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.02 06:27:58 UTC