W DOC AIRBUS | AMM A320F

Installation of the Mount Fitting at FR14


TASK 53-16-11-400-001-A
Installation of the Mount Fitting at FR14


ZONE: 220
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
220
FWD CAB UTILITY AREAS
 B. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
15
NUTS
AIPC 53-16-01-90-020
17
NUTS
AIPC 53-16-01-90-020
19
NUTS
AIPC 53-16-01-90-020
21
NUTS
AIPC 53-16-01-90-020
8
NUTS
AIPC 53-16-01-90-020
6
NUTS
AIPC 53-16-01-90-050
9
NUTS
AIPC 53-16-01-90-050
15
NUTS
AIPC 53-16-81-90-020
17
NUTS
AIPC 53-16-81-90-020
19
NUTS
AIPC 53-16-81-90-020
21
NUTS
AIPC 53-16-81-90-020
8
NUTS
AIPC 53-16-81-90-020
6
NUTS
AIPC 53-16-81-90-120
9
NUTS
AIPC 53-16-81-90-120
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 23-72-51-000-001-A
Removal of the Anti-Hijack-System Cameras
TASK 23-72-51-400-001-A
Installation of the Anti-Hijack-System Cameras
TASK 25-13-41-000-001-A
Removal of the Ceiling Panels
TASK 25-13-41-400-001-A
Installation of the Ceiling Panels
TASK 25-23-42-000-001-A
Removal of the Ceiling Panels - Forward Utility Area
TASK 25-23-42-400-001-A
Installation of the Ceiling Panels - Forward Utility Area
TASK 52-51-11-000-001-A
Removal of the Cockpit Door
TASK 52-51-11-400-001-A
Installation of the Cockpit Door
3. Job Set-up
Subtask 53-16-11-010-051-A
A. Get Access
   (1) Make sure that the anti-hijack-system camera(s) is(are) removed (Ref. AMM TASK 23-72-51-000-001), if installed.
   (2) Make sure that ceiling panel 221AC is removed (Ref. AMM TASK 25-23-42-000-001).
   (3) Make sure that lining panel 211HC is removed (Ref. AMM TASK 25-13-41-000-001).
   (4) Make sure that the cockpit door is removed (Ref. AMM TASK 52-51-11-000-001).
4. Procedure
Subtask 53-16-11-420-050-A
A. Installation of the Mount Fitting at FR14

   (1) Install the mount fitting (1):
     (a) Put the mount fitting (1) in position and then install the bolts (22), the washers (20) and the new AIPC 53-16-01-90-020 NUTS (21) or the new AIPC 53-16-81-90-020 NUTS (21).
     (b) Tighten the nuts (21).
     (c) Install the bolts (24), the washers (18) and the new
AIPC 53-16-01-90-020 NUTS (19) or the new AIPC 53-16-81-90-020 NUTS (19).
     (d) Tighten the nuts (19).
   (2) Install the plate (4):
     (a) Put the plate (4) in position and then install the bolts (11), the washers (16) and the new
AIPC 53-16-01-90-020 NUTS (17) or the new AIPC 53-16-81-90-020 NUTS (17).
     (b) Tighten the nuts (17).
   (3) Install the web (13):
     (a) Put the web (13) in position and then install the bolts (12) and the new
AIPC 53-16-01-90-020 NUTS (15) or the new AIPC 53-16-81-90-020 NUTS (15).
     (b) Tighten the nuts (15).
     (c) Install the bolts (23), the washers (10) and the new
AIPC 53-16-01-90-050 NUTS (9) or the new AIPC 53-16-81-90-120 NUTS (9).
     (d) Tighten the nuts (9).
   (4) Install the web (7):
     (a) Put the web (7) in position and then install the bolts (3), the washers (5) and the new
AIPC 53-16-01-90-050 NUTS (6) or the new AIPC 53-16-81-90-120 NUTS (6).
     (b) Tighten the nuts (6).
     (c) Install the bolts (14) and the new
AIPC 53-16-01-90-020 NUTS (8) or the new AIPC 53-16-81-90-020 NUTS (8).
     (d) Tighten the nuts (8).
5. Close-up
Subtask 53-16-11-410-050-A
A. Close Access
   (1) Install the cockpit door (
Ref. AMM TASK 52-51-11-400-001).
   (2) Install lining panel 211HC (Ref. AMM TASK 25-13-41-400-001).
   (3) Install ceiling panel 221AC (Ref. AMM TASK 25-23-42-400-001).
   (4) Install the anti-hijack-system camera(s) (Ref. AMM TASK 23-72-51-400-001), if removed.
[Rev.10 from 2021] 2026.04.01 01:51:59 UTC