W DOC AIRBUS | AMM A320F

Inspection/Check of the Thermocouple Probe (APS 3200)


TASK 49-72-15-200-003-A
Inspection/Check of the Thermocouple Probe (APS 3200)


WARNING: DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
1
MEGOHMMETER 100 MOHMS - MEASURING VOLTAGE 45 VDC
No specific
1
OHMMETER MULTIRANGE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 56 and 51 lbf.in (0.63 and 0.58 m.daN ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
315AL, 316AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 49-72-15-000-001-A
Removal of the Thermocouple (APS 3200)
TASK 49-72-15-400-002-A
Installation of the Thermocouple (APS 3200)
TASK 52-41-00-010-001-A
Open the APU Doors for Access
TASK 52-41-00-410-001-A
Close the APU Doors after Access
3. Job Set-up
Subtask 49-72-15-860-065-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
   (2) On panel 25VU, make sure that the APU MASTER SW pushbutton switch is off.
   (3) Put a WARNING NOTICE(S) in position in the cockpit to tell persons not to start the APU.
   (4) Make sure that the ground fire-extinguishing equipment is available.
   (5) Make sure that the hydraulic systems are depressurized (Ref. AMM TASK 29-00-00-864-001).
Subtask 49-72-15-865-069-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
Subtask 49-72-15-010-057-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below APU access doors 315AL and 316AR.
   (2) Open APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
   (3) Set the LIGHT control SW 11LJ to the ON position.
4. Procedure
Subtask 49-72-15-210-052-A ** ON A/C NOT FOR ALL
CAUTION: -YOU MUST NOT INCREASE THE TIGHTENING TORQUE MORE THAN THE MAXIMUM VALUE.
  • APPLY ALL TIGHTENING TORQUES WITH A TORQUE WRENCH OR A CALIBRATED SCREWDRIVER.
A. Inspection/Check of the Thermocouple Probe
NOTE: There are two thermocouples. The procedure is the same for each of them. Long thermocouple TC1 P30 (1) is installed on the right side of the APU and short thermocouple TC2 P31 (2) is installed on the left side of the APU.
   (1) Disconnect long thermocouple TC1 P30 (1) or short thermocouple TC2 P31 (2) from the mount bracket.
   (2) Remove the bolt (3) and disconnect long thermocouple TC1 P30 (1) or short thermocouple TC2 P31 (2) from the exhaust.
   (3) Do a visual check of the thermocouple probe and make sure that:
  • There are no cracks.
  • The thermocouple probe is not bent.
  • There are not kinks.
  • There is no erosion on the tip of the thermocouple probe.
     (a) If you find damage on the thermocouple probe, replace the related thermocouple (1) or (2) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-002).
   (4) Do an insulation resistance test at ambient temperature:
     (a) Connect a MEGOHMMETER 100 MOHMS - MEASURING VOLTAGE 45 VDC to measure the resistance between:
  • Positive pin (pin 1) of the thermocouple connector and the switch assembly housing.
  • Negative pin (pin 2) of the thermocouple connector and the switch assembly housing.
     (b) Make sure that the minimum resistance value is 100 megohms after 60 seconds.
     (c) If the resistance value is less than 100 megohms after 60 seconds, replace the related thermocouple (1) or (2) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-002).
   (5) Do a continuity resistance test:
     (a) Connect an OHMMETER MULTIRANGE between the positive pin (pin 1) and the negative pin (pin 2) of the thermocouple connector.
     (b) Make sure that the resistance is between 0.7 and 3 ohms.
     (c) If the resistance value is not in the specified limits, replace the related thermocouple (1) or (2) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-002).
   (6) Connect long thermocouple TC1 P30 (1) or short thermocouple TC2 P31 (2) to the exhaust with the bolt (3).
   (7) TORQUE the bolt (3) to between 56 and 51 lbf.in (0.63 and 0.58 m.daN ) T.
   (8) Connect long thermocouple TC1 P30 (1) or short thermocouple TC2 P31 (2) to the mount bracket.
5. Close-up
Subtask 49-72-15-410-055-A ** ON A/C NOT FOR ALL
Subtask 49-72-15-865-070-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
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
Subtask 49-72-15-860-068-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 01:32:09 UTC