B. Do the operational test and the BITE test given in Para. 3.

 Loss of the Accelerometer 1 Signal for the ELAC 1
 1. Possible Causes
_______________
 - ELAC-1 (2CE1)

 - ACCLRM-1 (12CE1)

 - wiring of the ANI 4-1 signal from the ELAC 1 (2CE1) to the accelerometer (12CE1)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-92-16-000-001 Removal of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) AMM 27-92-16-400-001 Installation of the Flight Control Accelerometer
 (12CE1,12CE2,12CE3,12CE4)
 AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
 AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)

R  AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/24
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 ELAC1 COM OR WIRING FROM ACCLRM1 12CE1
 or
 ELAC1 MON OR WIRING FROM ACCLRM1 12CE1

 - replace the ELAC-1 (2CE1), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) If the fault continues:

 - replace the ACCLRM-1 (12CE1), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).

 (2) If the fault continues:

 - do a check and repair the wiring of the ANI 4-1 signal from the ELAC 1 (2CE1) to the accelerometer (12CE1) ELAC 1 COM part or MON part as shown in the maintenance message (Ref. ASM 27-92/24).
 「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page 227
 Aug 01/99 CES

 B. Do the test given in Para.3.

 Loss of the Accelerometer 2 Signal for the ELAC 1
 1. Possible Causes
_______________
 - ELAC-1 (2CE1)
 - ACCLRM-2 (12CE2) R - wiring of the ANI 4-2 signal from the ELAC 1 (2CE1) to the accelerometer 2 R (12CE2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 27-92-16-000-001 Removal of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) AMM 27-92-16-400-001 Installation of the Flight Control Accelerometer
 (12CE1,12CE2,12CE3,12CE4)
 AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
 AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
 AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 ASM 27-92/24

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 ELAC 1 COM OR WIRING FROM ACCLRM 2 12CE2
 or
 ELAC 1 MON OR WIRING FROM ACCLRM 2 12CE2

 - replace the ELAC-1 (2CE1), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) If the fault continues:

 - replace the ACCLRM-2 (12CE2), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).

 (2) If the fault continues:

 - do a check and repair the wiring of the ANI 4-2 signal from the ELAC 1 (2CE1) to the accelerometer 2 (12CE2) ELAC 1 COM part or MON part as shown in the maintenance message (Ref. ASM 27-92/24).
 「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page 229
 Feb 01/04 CES

 B. Do the test given in Para. 3.

 Loss of the Accelerometer 3 Signal for the ELAC 2
 1. Possible Causes
_______________
 - ELAC-2 (2CE2)

 - ACCLRM-3 (12CE3)

 - wiring of the ANI 4-1 signal from the ELAC 2 (2CE2) to the accelerometer 3 (12CE3)

 2. Job Set-up Information
______________________
 A. Referenced Information
　
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