Failure of the THS Actuator Servo Motor 2 for the ELAC 1
TASK 27-93-00-810-845-A
Failure of the THS Actuator Servo Motor 2 for the ELAC 1
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 27-93-00-700-102-A
Subtask 27-93-00-810-094-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:58 UTC
Failure of the THS Actuator Servo Motor 2 for the ELAC 1
1. Possible Causes
- RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2]
- ELAC-1 [2CE1]
- SEC-1 [1CE1]
- Electronic Module 2
wiring of K3-1 signal from the ELAC 1 (2CE1) to the first terminal block wiring of the DSI-49 signal from the ELAC 1 (2CE1) to the ELAC 1 (2CE1) wiring of the K3-1B signal from the ELAC 1 (2CE1) to the first terminal block wiring of the relay (36CE2) to the ELAC 1 (2CE1) and to the THS actuator (9CE) wiring of the fault signal from the ELAC 1 (2CE1) to the first terminal block
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 31-32-00-810-932-A | Failure of the Discrete Links |
| TSM TASK 31-32-00-810-933-A | Failure of the Analog Links |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 27-44-57-000-002 | Removal of the Electronic Modules of the Pitch Trim Actuator |
| AMM 27-44-57-400-002 | Installation of the Electronic Modules of the Pitch Trim Actuator |
| AIPC 27920803 | |
| ASM 279312 | |
| ASM 279313 | |
| AMM 27-93-34-000-001 | Removal of the ELAC |
| AMM 27-93-34-400-001 | Installation of the ELAC |
| ASM 279412 | |
| ASM 279413 | |
| AMM 27-94-34-000-001 | Removal of the SEC |
| AMM 27-94-34-400-001 | Installation of the SEC |
| AMM 27-96-00-740-001 | BITE Test of the EFCS (Ground Scanning) |
| AMM 29-10-00-864-001 | Depressurize the Green Hydraulic System |
| AMM 29-10-00-864-002 | Depressurize the Yellow Hydraulic System |
| AMM 29-10-00-864-003 | Depressurize the Blue Hydraulic System |
Subtask 27-93-00-700-102-A
A. Test
(1) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(2) Make sure that the Green, Blue and Yellow hydraulic systems are not pressurized AMM 29-10-00-864-001, AMM 29-10-00-864-003 and AMM 29-10-00-864-002.
(3) On the panel 23VU:
(5) On the panel 23VU:
4. Fault Isolation(1) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(2) Make sure that the Green, Blue and Yellow hydraulic systems are not pressurized AMM 29-10-00-864-001, AMM 29-10-00-864-003 and AMM 29-10-00-864-002.
(3) On the panel 23VU:
- release the FLT CTL/ELAC1 pushbutton switch.(On this pushbutton switch, the OFF legend comes on).
(5) On the panel 23VU:
- push the FLT CTL/ELAC1 pushbutton switch.(On this pushbutton switch, the OFF legend goes off).
NOTE: Wait 60 seconds before you start the BITE test.
Subtask 27-93-00-810-094-A
A. If the BITE test gives the maintenance message:
THS ACTR SERVO MOT2 9CE OF ELAC1
(1) Remove the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2] AIPC 27920803.
(2) Do a check of the resistance between pin X1 and X2 of the relay.
(a) if the resistance is less than 280 ohms:
(b) If there is continuity:
2 If there is continuity:
b If there is continuity:
Subtask 27-93-00-700-103-A THS ACTR SERVO MOT2 9CE OF ELAC1
(1) Remove the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2] AIPC 27920803.
(2) Do a check of the resistance between pin X1 and X2 of the relay.
(a) if the resistance is less than 280 ohms:
- replace the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2] .
- replace the ELAC-1 [2CE1] AMM 27-93-34-000-001 AMM 27-93-34-400-001.
- replace the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2] .
- install the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2]
- see Para (3).
- replace the ELAC-1 [2CE1] , AMM 27-93-34-000-001 and AMM 27-93-34-400-001.
- do the trouble shooting procedure (Ref. TSM TASK 31-32-00-810-932) related to the DSI 24 discret input signal of the ELAC 1 and SEC 1 ASM 279312 ASM 279313 ASM 279412 ASM 279413 and
- do the trouble shooting procedure (Ref. TSM TASK 31-32-00-810-933) related to the ANI 2-3 analog input signal of the ELAC 1 and SEC 1 ASM 279312 and ASM 279412.
- replace the SEC-1 [1CE1] , AMM 27-94-34-000-001 and AMM 27-94-34-400-001.
- replace the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY [36CE2] Ref. IPC 27920803.
- replace the Electronic Module 2 , AMM 27-44-57-000-002 and AMM 27-44-57-400-002.
- do a check of the
wiring of K3-1 signal from the ELAC 1 (2CE1) to the first terminal block COM part and MON part ASM 279312.
(b) If there is continuity:
- do a check of the
wiring of the DSI-49 signal from the ELAC 1 (2CE1) to the ELAC 1 (2CE1) COM part and MON part ASM 279312.
2 If there is continuity:
- do a check of the
wiring of the K3-1B signal from the ELAC 1 (2CE1) to the first terminal block , ASM 279312.
b If there is continuity:
- do a check and repair the
wiring of the relay (36CE2) to the ELAC 1 (2CE1) and to the THS actuator (9CE) ,wiring of the fault signal from the ELAC 1 (2CE1) to the first terminal block , ASM 279312.
B. Do the tests given in Para. 3.