W DOC AIRBUS | AMM A320F

Removal of the Temperature Sensors


TASK 21-63-17-000-001-A
Removal of the Temperature Sensors


FIN: 21HK
FIN: 22HK
FIN: 23HK
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [22HK] (TEMP SENSOR FWD CAB)
231DC
FOR [23HK] (TEMP SENSOR AFT CAB)
251CC
251EC
 C. Referenced Information
REFERENCE
DESIGNATION
FOR [21HK] (SENSOR-TEMPERATURE, COCKPIT or TEMP SENSOR CKPT)
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)
FOR [22HK] (TEMP SENSOR FWD CAB)
FOR [23HK] (TEMP SENSOR AFT CAB)
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 25-23-41-000-001-A
Removal of the Ceiling Panels
3. Job Set-up
Subtask 21-63-17-861-050-B
A. Aircraft Maintenance Configuration

   (1) FOR [21HK] (SENSOR-TEMPERATURE, COCKPIT or TEMP SENSOR CKPT)
Make sure the aircraft electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
     (a) Put a warning notice in position to tell persons not to energize the aircraft electrical
circuits.
   (2) FOR [22HK] (TEMP SENSOR FWD CAB), [23HK] (TEMP SENSOR AFT CAB)
Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 21-63-17-865-053-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 23HK (TEMP SENSOR AFT CAB) FOR FIN: 22HK (TEMP SENSOR FWD CAB)
49VUAIR COND/TEMP CTL/SYS 1 CHAN B/28VDC52HHD08
** ON A/C NOT FOR ALL
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS24HKV20
122VUAIR COND/ZONE TEMP CTL/28VDC/SYS13HKV19
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS22HKV18
122VUAIR COND/ZONE TEMP CTL/115VAC/SYS11HKV17
** ON A/C NOT FOR ALL
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 21-63-17-010-050-B ** ON A/C NOT FOR ALL
C. Get Access
   (1) For the Cockpit Temperature Sensor

     (a) FOR [21HK] (SENSOR-TEMPERATURE, COCKPIT or TEMP SENSOR CKPT)
       1 Remove the screws (5) and the grill (6).
WARNING: MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
       2 Open the circuit breaker panel (1) 121VU.
   (2) For the Cabin Temperature Sensors

     (a) FOR [22HK] (TEMP SENSOR FWD CAB), [23HK] (TEMP SENSOR AFT CAB)
       1 Remove the cabin ceiling panels (Ref. AMM TASK 25-23-41-000-001),

         a FOR [22HK] (TEMP SENSOR FWD CAB)
231DC.

         b FOR [23HK] (TEMP SENSOR AFT CAB)
251CC.
Subtask 21-63-17-010-050-D ** ON A/C NOT FOR ALL
C. Get Access
   (1) For the Cockpit Temperature Sensor

     (a) FOR [21HK] (SENSOR-TEMPERATURE, COCKPIT or TEMP SENSOR CKPT)
       1 Remove the screws (5) and the grill (6).
WARNING: MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
     (b) Open the circuit breaker panel (1) 121VU.
   (2) For the Cabin Temperature Sensors

     (a) FOR [22HK] (TEMP SENSOR FWD CAB), [23HK] (TEMP SENSOR AFT CAB)
       1 Remove the cabin ceiling panels (Ref. AMM TASK 25-23-41-000-001),

         a FOR [22HK] (TEMP SENSOR FWD CAB)
231DC.

         b FOR [23HK] (TEMP SENSOR AFT CAB)
251EC.
4. Procedure
Subtask 21-63-17-020-053-B
A. Removal of the Cockpit Temperature Sensor 21HK
   (1) Disconnect the electrical connector (2).
   (2) Remove the isolation material (8).
   (3) Put blanking caps on the disconnected electrical connectors.
   (4) Remove the screws (3) and the sensor (4).
Subtask 21-63-17-020-050-B
B. Removal of the Cabin Temperature Sensor

   (1) FOR [22HK] (TEMP SENSOR FWD CAB), [23HK] (TEMP SENSOR AFT CAB)
     (a) Disconnect the electrical connector (26).
     (b) Put blanking caps on the disconnected electrical connectors.
     (c) Release the quick-release fasteners (29) and remove the front panel (24) together with the temperature sensor (27).
     (d) Remove the nuts (22), the washers (23), the screws (25), the temperature sensor (27) and the gasket (28).
[Rev.10 from 2021] 2026.04.01 04:52:58 UTC