3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (Activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
(2) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
(a) If the ground scanning gives the maintenance message: R Y ELEV pos XDCR 34CE2 COM E2/S2:USE STBY XDCR
- refer to Para. Fault Isolation.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 266
Aug 01/03 CES
(b) If the ground scanning gives at least two maintenance messages of the list below: L G ELEV pos XDCR 34CE1 COM E2/S2:USE STBY XDCR R Y ELEV pos XDCR 34CE2 COM E2/S2:USE STBY XDCR ELAC2 COM OR INPUT OF THS ACTR XDCR1 9CE SEC2 COM OR INPUT OF THS ACTR XDCR3 9CE
- do this trouble shooting procedure (Ref. TASK 27-90-00-810-823).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
R Y ELEV POS XDCR 34CE2 COM E2/S2 : USE STBY XDCR
- deactivate the defective RVDT and connect the spare RVDT (Ref. AMM TASK 27-34-00-040-001) and (Ref. AMM TASK 27-34-00-440-001).
(1) If the fault continues:
- do the trouble shooting procedure (Ref. TASK 31-32-00-810-933) related to the ANI 2-X analog input signal of the ELAC COM and SEC COM (Ref. ASM 27-93/07) and (Ref. ASM 27-94/07).
(2) If the fault continues:
- replace the SERVO CTL-R ELEVATOR, INBD Y (34CE2) (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
NOTE : The resistance of primary and secondary windings must be
____
between 30 ohms and 500 ohms.
(3) If the fault continues:
(a) Do a check of the wiring of the POS RVDT COM SPLY signal from the servocontrol (34CE2) to the first terminal block (Ref. ASM 27-93/08):
- if there is continuity, see Para. (b)
- if there is no continuity, repair the above wiring.
(b) Do a check and repair the wiring of the POS RVDT COM V1, V2 signals from the servocontrol (34CE2) to the first terminal block (Ref. ASM 27-93/08).
B. Do the tests given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 267
Aug 01/00R
CES
Loss of the Signal of the Right Yellow Elevator-Servocontrol Position-Transducer by the SEC 2
1. Possible Causes
_______________
- SEC-2 (1CE2)
- wiring of the POS XDCR COM (ANI 2-2) signal from the SEC 2 (1CE2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-821 Loss of the ACS1 Signal of the SEC2 COM Side
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
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)
ASM 27-94/08
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (Activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
NOTE : Before you start the operational test procedure, release the
____ FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch the OFF legend comes on).
(2) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
(a) If the ground scanning gives the maintenance message: SEC2 OR WIRING FROM R Y ELEV MODE XDCR 34CE2
- refer to Para. Fault Isolation.
(b) If the ground scanning gives at least two maintenance messages of the list below: SEC2 OR WIRING FROM L G ELEV POS XDCR 34CE1 SEC2 OR WIRING FROM R Y ELEV POS XDCR 34CE2 SEC2 COM OR INPUT OF THS ACTR XDCR3 9CE
- do this trouble shooting procedure (Ref. TASK 27-90-00-810-821).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(61)
