W DOC AIRBUS | AMM A320F

Installation of the Metric Altimeter


TASK 34-21-25-400-001-A
Installation of the Metric Altimeter


ZONE: 211
FIN: 15FN ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
211
COCKPIT
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 25-13-41-000-002-A
Removal of the Sidewall Panels
TASK 25-13-41-400-002-A
Installation of the Sidewall Panels
TASK 33-13-00-710-001-A
Operational Test of the Instrument and Panel Integral-Lighting
3. Job Set-up
Subtask 34-21-25-865-051-A ** ON A/C NOT FOR ALL
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VULIGHTING/INSTL LT/MAIN INST/PNL AND/PED4LFY04
Subtask 34-21-25-010-051-A ** ON A/C NOT FOR ALL
B. Remove the sidewall panel 211LW (Ref. AMM TASK 25-13-41-000-002).
4. Procedure
Subtask 34-21-25-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Metric Altimeter (15FN)
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Remove the blanking caps from the electrical connectors (3) and (5).
   (4) Make sure that the electrical connectors are clean and in the correct condition.
   (5) Connect the electrical connector (5) to the receptacle (3) of the metric altimeter (2).
   (6) Remove the blanking plugs from the quick-disconnect couplings (4) and (6).
   (7) Connect the quick-disconnect coupling (6) to the receptacle (4) of the metric altimeter (2).
   (8) Make sure that you can see the blue ring on the quick-disconnect coupling.
   (9) Pull the quick-disconnect coupling to be sure that it is correctly attached.
   (10) Make sure that the quick-disconnect coupling is correctly engaged (the pin located on the quick-disconnect male part is fully engaged into the groove located in the quick-disconnect female part).
   (11) Install the metric altimeter (2) in its housing.
   (12) Look behind the metric altimeter and make sure that the position of the flexible hose (static pressure line) is satisfactory (no crushing, kings, crease or folds).
   (13) Tighten the screws (1).
Subtask 34-21-25-865-052-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
122VULIGHTING/INSTL LT/MAIN INST/PNL AND/PED4LFY04
Subtask 34-21-25-710-050-A ** ON A/C NOT FOR ALL
C. Do the operational test of the instrument and panel integral lighting (Ref. AMM TASK 33-13-00-710-001).
5. Close-up
Subtask 34-21-25-410-050-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Install the thermoformed cover on the center instrument panel.
   (2) Install the sidewall panel 211LW (Ref. AMM TASK 25-13-41-400-002).
   (3) Make sure that the work area is clean and clear of tools and other items.
[Rev.10 from 2021] 2026.04.02 07:13:53 UTC