W DOC AIRBUS | AMM A320F

Removal of the Safety Support Equipment


TASK 52-30-00-080-001-A
Removal of the Safety Support Equipment


ZONE: 130
ZONE: 150
ZONE: 825
ZONE: 826
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
98D52307515000
1
SAFETY LOCK-ACTUATOR,CARGO DOORS
98D52307524000
1
STRUT-SUPPORT,CARGO DOORS
 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
150
AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT
825
FORWARD CARGO COMPARTMENT DOOR
826
AFT CARGO COMPARTMENT DOOR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
3. Job Set-up
Subtask 52-30-00-010-065-A
A. Get Access
   (1) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position at the open forward or aft cargo door.
4. Procedure
Subtask 52-30-00-080-050-A
A. Removal of the Safety Support Equipment
   (1) Remove the 98D52307515000 SAFETY LOCK-ACTUATOR,CARGO DOORS from the door actuator as follows:
     (a) If necessary, fully open the applicable cargo door to make sure that the door actuator piston does not cause a blockage of the 98D52307515000 SAFETY LOCK-ACTUATOR,CARGO DOORS (Ref. AMM TASK 52-30-00-860-001).
     (b) Hold the safety lock and remove the knurled screws.
     (c) Open the safety lock and remove it from the door actuator piston.
     (d) Close the safety lock and install the knurled screws.
   (2) If installed, remove the 98D52307524000 STRUT-SUPPORT,CARGO DOORS from the fuselage frame and the cargo door as follows:
NOTE: The 98D52307524000 STRUT-SUPPORT,CARGO DOORS contains two support struts 98D52307524040.
     (a) Make sure that there is no load on the support struts.
     (b) If necessary, open the applicable cargo door to remove the load from the support struts (Ref. AMM TASK 52-30-00-860-001).
     (c) Pull the ring of the pip pin and remove the long support strut-end from the lateral edge members of the cargo door.
     (d) Pull the ring of the pip pin and remove the short support strut-end from the fuselage frame.
5. Close-up
Subtask 52-30-00-410-060-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 01:40:39 UTC