W DOC AIRBUS | AMM A320F

Removal of the Lower Right Thermocouple Lead Assembly [CFMB]


TASK 77-21-10-000-029-A
Removal of the Lower Right Thermocouple Lead Assembly


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** 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
AR
CAP - BLANKING
No specific
AR
PLUG - BLANKING
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-B
Opening of the Thrust Reverser Doors
3. Job Set-up
Subtask 77-21-10-941-065-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 77-21-10-010-078-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
Subtask 77-21-10-040-076-A ** ON A/C NOT FOR ALL
C. Make sure that the thrust reverser is unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 77-21-10-010-092-A ** ON A/C NOT FOR ALL
D. Open the thrust reverser doors: (Ref. AMM TASK 78-36-00-010-040)
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure
Subtask 77-21-10-020-061-A ** ON A/C NOT FOR ALL
A. Removal of the Lower Right (R/H) Thermocouple Lead Assembly (Lower Right T495 Sector)
   (1) Cut and remove the lockwire.
NOTE: For engine with EGT sensor (thermocouple) probe brackets repaired, you find a bolt which replaces a stud and a nut (10). A lockwire lock the bolt to a locally manufactured washer located on the nut (10).
You can see engraved on the locally manufactured washer marking area, the number of SB 72-0473.
   (2) Disconnect the lower extension lead connector (80) from the lower right T495 sector junction box (parallel junction box) (20).
   (3) Remove the parts which attach the lower right T495 sector as follows:

PRE SB CFM 72-0473

     (a) Remove the nuts (10) from the studs (30) on LPT case, at the 4:15 and the 5:30 o'clock positions (Detail B).

END OF PRE SB CFM 72-0473

POST SB CFM 72-0473

     (b) Remove the bolt (65) from the EGT Sensor (Thermocouple) probe braket assy on LPT case, at the 4:15 and the 5:30 o'clock positions (Detail B).
     (c) Remove the nut (10) and the washer from the stud (30). Keep the bolt and the washer

END OF POST SB CFM 72-0473

     (d) Remove the bolt (60) from the bracket (40) on flange S, at the 6 o'clock position (Detail C).
     (e) Remove the clamp (50).
     (f) Remove the nuts (90) from the flange S, at the 5:15 o'clock position (Detail D).
     (g) Remove the bolt (70).
     (h) Remove the bolt (120) from the bracket (100) on flange S, at the 4:30 o'clock position (Detail E).
     (i) Remove the clamp (110).
   (4) Carefully remove the lower right T495 sector (20) from the LPT holes and from the engine.
   (5) Install the PLUG - BLANKING and CAP - BLANKING on all disconnected parts.
[Rev.10 from 2021] 2026.04.01 03:17:38 UTC