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
Refer to the MPD TASK: 523116-01
SPECIAL DETAILED INSPECTION (ROTO) OF AFT CARGO COMPARTMENT DOOR SKIN UNDERNEATH HINGE FITTINGS AT SELECTED BOLT HOLES
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 52-32-11-860-055-A
Subtask 52-32-11-250-050-A
Subtask 52-32-11-410-052-A
[Rev.10 from 2021]
2026.04.02 06:27:58 UTC
Special Detailed Inspection (ROTO) of AFT Cargo Compartment Door Skin Underneath Hinge Fittings at Selected Bolt Holes
ZONE: 826
1. Reason for the JobRefer 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 InformationA. 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 |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 826 | AFT CARGO COMPARTMENT DOOR |
| 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) |
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 (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.
B. Open, safety and tag this(these) circuit breaker(s):
Subtask 52-32-11-010-052-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| ** ON A/C ALL | |||
| 122VU | DOORS/CARGO | 1MJ | T12 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
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 (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.
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(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.
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 (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.
B. Do the procedure for the application of the temporary protection system (Ref. AMM TASK 51-78-00-916-001).
5. Close-upSubtask 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 (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).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 52-32-11-860-056-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| ** ON A/C ALL | |||
| 122VU | DOORS/CARGO | 1MJ | T12 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
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).
(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).
Inspection of the External Attachment Area of the Piano Hinge Fittings