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 (a) If the fault continues:
 - do a check and repair the wiring from the SEC 2 (1CE2) COM and MON to the terminal block (DSI 19) (Ref. ASM 27-92/27).

 (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.

　
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