Failure of the Left Blue Elevator-Servocontrol Mode-Transducer
TASK 27-30-00-810-809-A
Failure of the Left Blue Elevator-Servocontrol Mode-Transducer
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 27-30-00-700-062-A
Subtask 27-30-00-810-056-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:31 UTC
Failure of the Left Blue Elevator-Servocontrol Mode-Transducer
1. Possible Causes
- SERVO CTL-L ELEVATOR, OUTBD B [34CE3]
wiring of the MODE XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block wiring of the MODE XDCR V1 signal from the servocontrol (34CE3) to the first terminal block
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 27-90-00-810-824-A | Loss of the ACS1 Signal of the ELAC2 MON Side and SEC2 MON Side |
| TSM TASK 31-32-00-810-933-A | Failure of the Analog Links |
| AMM 27-34-51-000-006 | Removal of the Elevator Servo Control Actuator Mode Selector Valve Transducer MSVT |
| AMM 27-34-51-400-005 | Installation of the Elevator Servo Control Actuator Mode Selector Valve Transducer MSVT |
| ASM 279308 | |
| ASM 279408 | |
| 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 27-30-00-700-062-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.
(a) If the ground scanning gives the maintenance message:
L B ELEV MODE XDCR 34CE3
L B ELEV MODE XDCR 34CE3
L ELEV POS MON XDCR OF ELAC2/SEC2
R B ELEV MODE XDCR 34CE4
R Y ELEV POS MON XDCR OF ELAC2/SEC2
ELAC2 MON OR INPUT OF THS ACTR XDCR1 9CE
SEC2 MON OR INPUT OF THS ACTR XDCR3 9CE
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.
(a) If the ground scanning gives the maintenance message:
L B ELEV MODE XDCR 34CE3
- refer to Para. Fault Isolation.
L B ELEV MODE XDCR 34CE3
L ELEV POS MON XDCR OF ELAC2/SEC2
R B ELEV MODE XDCR 34CE4
R Y ELEV POS MON XDCR OF ELAC2/SEC2
ELAC2 MON OR INPUT OF THS ACTR XDCR1 9CE
SEC2 MON OR INPUT OF THS ACTR XDCR3 9CE
- do this trouble shooting procedure (Ref. TSM TASK 27-90-00-810-824).
Subtask 27-30-00-810-056-A
A. If the test gives the maintenance message:
L B ELEV MODE XDCR 34CE3
(a) Do a check of thewiring of the MODE XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block ASM 279308:
wiring of the MODE XDCR V1 signal from the servocontrol (34CE3) to the first terminal block ASM 279308.
Subtask 27-30-00-700-063-A L B ELEV MODE XDCR 34CE3
- do the trouble shooting procedure (Ref. TSM TASK 31-32-00-810-933) related to the ANI 7-X analog input signal of the ELAC MON and SEC MON ASM 279308 and ASM 279408.
- replace the SERVO CTL-L ELEVATOR, OUTBD B [34CE3] AMM 27-34-51-000-006 and AMM 27-34-51-400-005.
NOTE: The resistance of the primary winding of the elevator servocontrol mode-transducer (pins C/K and C/L) must be 96 ohms +/- 10 ohms, and the resistance of the secondary winding of the elevator servocontrol mode-transducer (pins (C/U and C/J) must be 700 ohms +/- 70 ohms. The insulation must be more than 10 Mohms.
(2) If the fault continues: - These values are given for information only. You can use these values to do a check of the component electrical part 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 Blue Elevator Servo Control.
(a) Do a check of the
- if there is continuity, see Para. (b)
- if there is no continuity, repair the above wiring.
B. Do the tests given in Para. 3.