W DOC AIRBUS | AMM A320F

Installation of the Support Strut


TASK 53-43-11-400-001-A
Installation of the Support Strut


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
NOTE: Applicable to FR50 and FR51, FR56 and FR57, FR61 and FR62 left side and the partition center support strut at FR65.
ZONE: 150
ZONE: 160
ZONE: 170
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Consumable Materials
REFERENCE
DESIGNATION
(Material No.06AAC1)
Polysulfide Sealant-General Purpose Interfay -
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
150
AFT CARGO COMPARTMENT FWD PRESS BULKHEAD TO AFT BULKHEAD OF AFT CARGO COMPARTMENT
160
BULK CARGO COMPARTMENT AFT BULKHEAD OF AFT CARGO COMPARTMENT TO AFT BULKHEAD OF BULK CARGO COMPARTMENT
170
AFT CAB U/FLOOR COMPT AFT BHD OF BULK
161DW, 162DW
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
TASK 25-55-12-400-001-A
Installation of the Aft Cargo-Compartment Partition at FR65
TASK 25-55-12-400-003-A
Installation of the Sidewall Panels in the Aft Cargo Compartment - FR59/FR65
TASK 52-30-00-860-002-A
Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
F Removable Support Struts ** ON A/C NOT FOR ALL
F Support Strut ** ON A/C NOT FOR ALL
F Support Strut ** ON A/C NOT FOR ALL
F Removable Support Struts ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 53-43-11-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft is in the same configuration as for the removal task.
   (2) Clean the support struts (1) and the mating surfaces with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Do an inspection of the component interfaces and the adjacent area.
Subtask 53-43-11-860-050-B ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the aircraft is in the same configuration as for the removal task.
   (2) Clean the applicable support strut (5) or (12) and the mating surfaces with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (3) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Do an inspection of the component interfaces and the adjacent area.
4. Procedure
Subtask 53-43-11-916-050-A ** ON A/C NOT FOR ALL
A. Preparation for Installation:
   (1) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) to:
     (a) The contact surfaces of the support struts (1).
     (b) The threads of the screws (3) and the bolts (4).
Subtask 53-43-11-420-050-A ** ON A/C NOT FOR ALL
B. Installation of the Support Struts
   (1) Put the support struts (1) in position.
   (2) Install the screws (3), the bolts (4), the nuts (5) and the washers (6).
   (3) Put the support struts (2) in position.
   (4) Install the quick release pins (7).
   (5) Seal all the bolts (4), the nuts (5) and the attachment area of the support struts (1) with Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) .
   (6) Install any attach items removed from the support struts (1).
Subtask 53-43-11-916-050-B ** ON A/C NOT FOR ALL
C. Preparation for Installation:
   (1) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) to:
     (a) The contact surfaces of the support strut (5)
     (b) The threads of the screw (1) and the bolts (6).
Subtask 53-43-11-420-050-B ** ON A/C NOT FOR ALL
D. Installation of the Support Strut
   (1) For the strut (5):
     (a) Put the support strut (5) in position.
     (b) Install the bolts (6), the washers (3) and the nuts (4).
     (c) Tighten the nuts (4).
     (d) Install the screw (1) and the washer (2).
     (e) Tighten the screw (1).
     (f) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) to the heads of the bolts (6), the nuts (4) and the attachment area of the support strut (5).
     (g) If applicable, install all the removed items to the support strut (5).
   (2) For the strut (12):
     (a) Put the support strut (12) in position.
     (b) Install the bolts (10), the washers (9) and (8) and the nuts (7).
     (c) Tighten the nuts (7).
     (d) Install the screws (17), the washers (18) and the nuts (11).
     (e) Tighten the nuts (11).
     (f) Install the bolts (13), the washers (14) and the nuts (16).
     (g) Tighten the nuts (16).
     (h) For the two bolts (10):
       1 Measure clearances A between the support strut (12) and the upper fitting (19).
       2 Make sure that clearance A is 0.5 mm (0.02 in.).
       3 Measure clearances B between the washers (8) and the nuts (7).
       4 Make sure that clearance B is 0.2 -0 mm or +0.4 mm (0.01 +0.00 in. or +0.02 in.).
     (i) For the two bolts (13):
       1 Measure clearances A between the support strut (12) and the lower fitting (15).
       2 Make sure that clearance A is 0.5 mm (0.02 in.).
       3 Measure clearances B between the washers (14) and the nuts (16).
       4 Make sure that clearance B is 0.2 -0 mm or +0.4 mm (0.01 +0.00 in. or +0.02 in.).
     (j) Put the bonding strap (22) in position and install the screw (20) and the washer (21) (Ref. AMM TASK 20-28-00-912-802).
     (k) Tighten the screw (20).
5. Close-up
Subtask 53-43-11-410-050-A
A. Make sure that the work area is clean and clear of tools and other items.
   (1) Install the left sidewall linings (Ref. AMM TASK 25-55-12-400-003).
   (2) Install the partition panels 161DW 162DW at FR65 (Ref. AMM TASK 25-55-12-400-001).
   (3) Remove the access platform(s).
   (4) Close the AFT cargo-compartment door. (Ref. AMM TASK 52-30-00-860-002).
   (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 06:24:15 UTC