Failure of the Left Blue Aileron Servo Control Position Transducer
TASK 27-10-00-810-804-A
Failure of the Left Blue Aileron Servo Control Position Transducer
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 27-10-00-700-055-A
Subtask 27-10-00-810-053-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:26 UTC
Failure of the Left Blue Aileron Servo Control Position Transducer
1. Possible Causes
- SERVO CTL-L AILERON, OUTBD B [33CE3]
wiring of the POS XDCR SPLY signal from the servo control (33CE3) to the first terminal block wiring of the POS XDCR, V11, V12, V21, V22 signal from the servo control (33CE3) to the first terminal block
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 27-90-00-810-807-A | Loss of the ACS2 Signal of the ELAC1 COM Side |
| AMM 27-14-51-000-001 | Removal of the Aileron Servo Control |
| AMM 27-14-51-400-001 | Installation of the Aileron Servo Control |
| ASM 279302 | |
| AMM 27-96-00-710-020 | Operational Test of the Side Stick Assembly (Activation for the BITE Test) |
| AMM 27-96-00-740-001 | BITE Test of the EFCS (Ground Scanning) |
Subtask 27-10-00-700-055-A
A. Test
(1) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(2) Do the BITE test of the EFCS (Ground Scanning) AMM 27-96-00-740-001.
4. Fault Isolation(1) Do the operational test of the side stick assembly (activation for the BITE test) AMM 27-96-00-710-020.
(2) Do the BITE test of the EFCS (Ground Scanning) AMM 27-96-00-740-001.
NOTE: If the POST FLIGHT REPORT (PFR) gives also the maintenance message:
R G AIL POS XDCR 33CE2
do this procedure (Ref. TSM TASK 27-90-00-810-807).
R G AIL POS XDCR 33CE2
do this procedure (Ref. TSM TASK 27-90-00-810-807).
Subtask 27-10-00-810-053-A
A. If the test gives the maintenance message:
L B AIL POS XDCR 33CE3
(a) Do a check of thewiring of the POS XDCR SPLY signal from the servo control (33CE3) to the first terminal block , ASM 279302:
wiring of the POS XDCR, V11, V12, V21, V22 signal from the servo control (33CE3) to the first terminal block , ASM 279302.
Subtask 27-10-00-700-056-A L B AIL POS XDCR 33CE3
- replace the SERVO CTL-L AILERON, OUTBD B [33CE3] , AMM 27-14-51-000-001 and AMM 27-14-51-400-001.
NOTE: The resistance of primary (pins A/B and A/C) and secondary (pins A/A and A/P, pins A/R and A/D) windings of the transducer must be between 30 ohms and 500 ohms. The insulation must be more than 10 Mohms.
These values are given for information only. You can use these values to do checks of the component electrical part or of the wiring before you replace the component. But by this procedure, the check of the component mechanical part is not done.
For primary winding (power supply):
(1) If the fault continues: These values are given for information only. You can use these values to do checks of the component electrical part or of the wiring before you replace the component. But by this procedure, the check of the component mechanical part is not done.
For primary winding (power supply):
- if you do the resistance check from the avionics compartment, you must disconnect the transducer of the Right Green Aileron Servo Control.
(a) Do a check of the
- if there is no continuity, repair the wiring
- if there is continuity, see Para. (b).
B. Do the test given in Para. 3.