Removal of the High Pressure Turbine Clearance Control (HPTCC) Sensor [CFMI]
TASK 73-21-70-000-001-A
Removal of the High Pressure Turbine Clearance Control (HPTCC) Sensor
1. Reason for the Job
The HPTCC Sensor are installed at 3:30 (channel B) and 9 o'clock (channel A) on the compressor discharge nozzle (CDN). The removal/installation procedure for both sensors is the same.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 73-21-70-941-050-A ** ON A/C NOT FOR ALL
Subtask 73-21-70-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:56:56 UTC
Removal of the High Pressure Turbine Clearance Control (HPTCC) Sensor
1. Reason for the Job
The HPTCC Sensor are installed at 3:30 (channel B) and 9 o'clock (channel A) on the compressor discharge nozzle (CDN). The removal/installation procedure for both sensors is the same.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | CAP - BLANKING |
| No specific | AR | PLIERS - JAWED, SOFT |
| No specific | AR | PLUG - BLANKING |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL, 452AR | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL, 462AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-13-00-010-040-A | Opening of the Fan Cowl Doors |
| TASK 78-30-00-481-041-A | Make the Thrust Reverser Unserviceable for Maintenance |
| TASK 78-36-00-010-040-A | Opening of the Thrust Reverser Doors |
Subtask 73-21-70-941-050-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 73-21-70-010-050-A ** ON A/C NOT FOR ALL (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).
B. Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
(1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
Subtask 73-21-70-040-050-A ** ON A/C NOT FOR ALL Subtask 73-21-70-010-051-A ** ON A/C NOT FOR ALL (1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
(2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
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(1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
(2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 73-21-70-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the HPTCC Sensor:
(1) Disconnect the electrical connector (50). Use PLIERS - JAWED, SOFT if necessary.
(2) Put CAP - BLANKING on the electrical connector (50) and the sensor (40).
(3) Cut and remove the lockwire from the bolts (10).
(4) Remove the bolts (10) and the washers (20) that attach the sensor (40) to the Compressor Discharge Nozzle (CDN).
(5) Remove the sensor (40) and gasket (30) from the CDN.
(6) Discard the gasket (30).
(7) Put a CAP - BLANKING on the probe of the sensor (40).
(8) Put a PLUG - BLANKING in the port of the CDN.
(1) Disconnect the electrical connector (50). Use PLIERS - JAWED, SOFT if necessary.
(2) Put CAP - BLANKING on the electrical connector (50) and the sensor (40).
(3) Cut and remove the lockwire from the bolts (10).
(4) Remove the bolts (10) and the washers (20) that attach the sensor (40) to the Compressor Discharge Nozzle (CDN).
(5) Remove the sensor (40) and gasket (30) from the CDN.
(6) Discard the gasket (30).
(7) Put a CAP - BLANKING on the probe of the sensor (40).
(8) Put a PLUG - BLANKING in the port of the CDN.
High Pressure Turbine Clearance Control Sensor