(6) On the SD, the symbol G of the R aileron is in amber:
- replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(a) If the fault continues:
- do a check and repair the wiring from the SEC 1 (1CE1) COM and MON to the terminal block (DSI 17) (Ref. ASM 27-92/27).
(1) Do the trouble shooting procedure (Ref. TASK 27-95-00-810-834).
R K. If during the test, with the takeover and priority pushbutton switch pushed, the legends on panel 130VU or 131VU, does not operate:
R L. Do the test given in Para. 3.
R TASK 27-96-00-810-802
R Operational Test of the THS Actuator Electrical Control not OK
R 1. Possible Causes_______________
R 2. Job Set-up Information______________________
R A. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R AMM 27-96-00-710-022 Operational Test of the THS Actuator Electrical
R Control (Activation for BITE Test)
R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
R 3. Fault Confirmation__________________
R A. Do the Operational Test of the THS Actuator Electrical Control (Ref. AMM
R TASK 27-96-00-710-022).
R 4. Fault Isolation_______________
R A. Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-
R 740-001):
R - refer to 27 ECAM (P. Block 101) for the related maintenace message
R - do the related trouble shooting procedure.
