W DOC AIRBUS | AMM A320F

Installation of the Pack-Inlet Pressure Sensor


TASK 21-51-13-400-001-A
Installation of the Pack-Inlet Pressure Sensor


FIN: 23HB1 ** ON A/C NOT FOR ALL
FIN: 24HB1 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
Torque wrench: range to between 0.11 and 0.09 m.daN (9.73 and 7.96 lbf.in ) T
No specific
Torque wrench: range to between 0.38 and 0.32 m.daN (33.63 and 28.32 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03FAB1)
Mineral Oil base Grease-- Vaseline or Petrolatum -
(Material No.03PBB1)
Lubricant-Anti Seize High Temp. -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [23HB1] (SENSOR-PRESS INLET,PACK 1)
191KB
FOR [24HB1] (SENSOR-PRESS INLET,PACK 2)
192KB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
10
PACKING-PREFORMED
AIPC 21-51-13-02-010
5
WASHER
AIPC 21-51-51-04-090
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-33-21-618-001-A-01
Pre-conditioning through the HP Ground Connection
TASK 12-33-21-618-001-A-02
Pre-conditioning with the APU
TASK 21-51-00-710-002-A
Operational Test of the Flow Control and Indicating System
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
TASK 53-35-13-400-002-A
Installation of the Quick-Release Access Panels on the Belly Fairing Structure
3. Job Set-up
Subtask 21-51-13-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that:
     (a) The aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
     (b) The access panel is removed (Ref. AMM TASK 53-35-13-000-002),
       1 FOR [23HB1] (SENSOR-PRESS INLET,PACK 1)
191KB,
       2 FOR [24HB1] (SENSOR-PRESS INLET,PACK 2)
192KB.
Subtask 21-51-13-865-051-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 23HB1 (SENSORPRESS INLET,PACK 1)
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
FOR FIN: 24HB1 (SENSORPRESS INLET,PACK 2)
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
4. Procedure
Subtask 21-51-13-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Pressure Sensor
   (1) Lubrication of the PACKING
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
     (a) Apply a small amount of Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) to the new AIPC 21-51-13-02-010 PACKING-PREFORMED (10).
   (2) Preparation of the Screws
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
     (a) Apply a small amount of Lubricant-Anti Seize High Temp. - (Material No.
03PBB1) to the threads of the screws (1) and (6).
   (3) Put the packing (10) in position on the sensor boss (9).
   (4) Make sure that the air-transfer hole in the sensor boss (9) is free from grease and other contamination.
   (5) Connect the electrical connector (7)
   (6) Put the sensor (8) in position and insert the sensor boss (9) into the sensor mount (11).
   (7) Push the sensor (8) in a forward direction until a stop is made between the sensor flange (12) and the sensor mount (11).
   (8) Insert the washers (2) and the screws (1).
   (9) TORQUE the screws (1) to between 0.38 and 0.32 m.daN (33.63 and 28.32 lbf.in ) T
NOTE: Make sure that there is no gap between the sensor flange (12) and the sensor mount (11)
   (10) Put the clamp (4) in position and install the new
AIPC 21-51-51-04-090 WASHER (5) and the screws (6).
   (11) TORQUE the screws (6) to between 0.11 and 0.09 m.daN (9.73 and 7.96 lbf.in )
T.
Subtask 21-51-13-865-052-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
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
122VUAIR COND/TEMP CTL SYS 2/CHAN A/115VAC53HHW22
122VUAIR COND/TEMP CTL SYS 2/CHAN A/28VDC55HHW21
122VUAIR COND/TEMP CTL SYS 1/CHAN A/115VAC49HHX22
122VUAIR COND/TEMP CTL SYS 1/CHAN A/28VDC51HHX21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/28VDC56HHY21
122VUAIR COND/TEMP CTL SYS 2/CHAN B/115VAC54HHY20
122VUAIR COND/TEMP CTL SYS 1/CHAN B/115VAC50HHY18
Subtask 21-51-13-710-050-A ** ON A/C NOT FOR ALL
C. Test
   (1) Do the pre-conditioning through the HP ground connector (
Ref. AMM TASK 12-33-21-618-001) or with the APU (Ref. AMM TASK 12-33-21-618-001).
   (2) Do a leak check at the sensor flange (12) and the sensor mount (11).
NOTE: Leaks are not permitted.
   (3) After approx. 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) or (Ref. AMM TASK 12-33-21-618-001).
   (4) Do the operational test of the flow control and indicating system (Ref. AMM TASK 21-51-00-710-002).
5. Close-up
Subtask 21-51-13-410-050-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the access panel (Ref. AMM TASK 53-35-13-400-002):
     (a) FOR [23HB1] (SENSOR-PRESS INLET,PACK 1)
191KB,
     (b) FOR [24HB1] (SENSOR-PRESS INLET,PACK 2)
192KB.
Subtask 21-51-13-862-050-A ** ON A/C NOT FOR ALL
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.05 10:34:31 UTC