Electrical Test of the Turbine Rear Frame Vibration Sensor [CFMB]
TASK 77-31-30-760-001-A
Electrical Test of the Turbine Rear Frame Vibration Sensor
1. Reason for the Job
To make sure of the serviceability of the Turbine Rear Frame (TRF) vibration sensor before fan trim balance or vibration check operation.
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 77-31-30-941-055-A ** ON A/C NOT FOR ALL
Subtask 77-31-30-760-050-A ** ON A/C NOT FOR ALL
Subtask 77-31-30-410-059-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:37:44 UTC
Electrical Test of the Turbine Rear Frame Vibration Sensor
1. Reason for the Job
To make sure of the serviceability of the Turbine Rear Frame (TRF) vibration sensor before fan trim balance or vibration check operation.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 1M(3 FT) |
| No specific | AR | MEGOHMMETER 100 MOHMS |
| No specific | AR | PLIERS - CONNECTOR, JAW, SOFT |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR, 451AL | |
| FOR [1000EM2] (ENGINE-2) | |
| 447AL, 448AR, 461AL | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 71-13-00-010-040-B | Opening of the Fan Cowl Doors |
| TASK 71-13-00-410-040-B | Closing of the Fan Cowl Doors |
| TASK 77-31-30-000-002-A | Removal of the Turbine Rear Frame Vibration Sensor |
| TASK 77-31-30-210-002-A | Visual Inspection of the TRF Vibration Sensor |
| TASK 77-31-30-400-002-A | Installation of the Turbine Rear Frame Vibration Sensor |
| TASK 78-30-00-081-041-B | Make the Thrust Reverser Serviceable after Maintenance |
| 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 |
| TASK 78-36-00-410-040-B | Closing of the Thrust Reverser Doors |
Subtask 77-31-30-941-055-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 77-31-30-010-061-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. 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
(2) Put the ACCESS PLATFORM 1M(3 FT) in position.
Subtask 77-31-30-040-054-A ** ON A/C NOT FOR ALL Subtask 77-31-30-010-062-A ** ON A/C NOT FOR ALL (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
(2) Put the ACCESS PLATFORM 1M(3 FT) in position.
D. Open the left thrust reverser door (Ref. AMM TASK 78-36-00-010-040):
(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL
4. Procedure(1) FOR [1000EM1] (ENGINE-1)
451AL
(2) FOR [1000EM2] (ENGINE-2)
461AL
Subtask 77-31-30-760-050-A ** ON A/C NOT FOR ALL
A. Electrical Test of the TRF Vibration Sensor
(2) Visually inspect the TRF vibration sensor (Ref. AMM TASK 77-31-30-210-002).
(3) Measure the insulation resistance with a MEGOHMMETER 100 MOHMS set to the 50 volts DC scale between:
(5) Connect the EVMU harness to the TRF vibration sensor connector. Fully tighten by hand. Use PLIERS - CONNECTOR, JAW, SOFT only if necessary.
(6) Make sure that the aircraft harness connector is fully engaged and does not move.
5. Close-upNOTE: If the TRF vibration sensor is not serviceable at the end of this test, replace the TRF vibration sensor per (Ref. AMM TASK 77-31-30-000-002) and (Ref. AMM TASK 77-31-30-400-002).
(1) Disconnect the EVMU harness from the TRF vibration sensor connector at one o'clock. Use PLIERS - CONNECTOR, JAW, SOFT only if necessary. (2) Visually inspect the TRF vibration sensor (Ref. AMM TASK 77-31-30-210-002).
(3) Measure the insulation resistance with a MEGOHMMETER 100 MOHMS set to the 50 volts DC scale between:
- pins 1 and 2
- pins 1 and 3
- pins 2 and 3
- pin 2 and connector body
- pin 3 and connector body.
The insulation resistance must be higher than 20 megohms.
(5) Connect the EVMU harness to the TRF vibration sensor connector. Fully tighten by hand. Use PLIERS - CONNECTOR, JAW, SOFT only if necessary.
(6) Make sure that the aircraft harness connector is fully engaged and does not move.
Subtask 77-31-30-410-059-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) Close the left thrust reverser door (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL
(b) FOR [1000EM2] (ENGINE-2)
461AL
(3) Remove the access platform(s).
Subtask 77-31-30-440-053-A ** ON A/C NOT FOR ALL Subtask 77-31-30-410-060-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the left thrust reverser door (Ref. AMM TASK 78-36-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
451AL
(b) FOR [1000EM2] (ENGINE-2)
461AL
(3) Remove the access platform(s).
Check of the TRF Vibration Sensor