2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-14-51-000-001 Removal of the Aileron Servo Control AMM 27-14-51-000-003 Removal of the Aileron Servo-Control Servovalve AMM 27-14-51-400-001 Installation of the Aileron Servo Control AMM 27-14-51-400-003 Installation of the Aileron Servo-Control Servovalve 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 27-96-00-710-020 Operational Test of the Side Stick Assembly
 (Activation for the BITE Test) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-93/02
 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).

 4. Fault Isolation
_______________
 A. If the test gives the maintenance message:
 L B AIL SERVO VLV 33CE3

 - replace the servovalve of the servo control 33CE3, (Ref. AMM TASK 27-14-51-000-003) and (Ref. AMM TASK 27-14-51-400-003).
 NOTE : The resistance must be 500 ohms +/- 10 %.
____

 「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 214
 May 01/00 CES

 (1) If the fault continues:

 - do a check of the wiring POS XDCR signal from the servocontrol (33CE3) to the ELAC 1 (2CE1) COM and MON side, (Ref. ASM 27-93/02).

 (2) If the fault continues:

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

 (3) If the fault continues:

 - replace the SERVO CTL-L AILERON, OUTBD B (33CE3), (Ref. AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-400-001).
 B. Do the test given in Para. 3.

 Failure of the Left Blue Aileron Servo Control Solenoid Valve
 CAUTION : DO NOT SWAP FLIGHT CONTROL COMPUTERS. IF THERE IS A SHORT CIRCUIT,
_______ YOU WILL CAUSE DAMAGE TO A SERVICEABLE COMPUTER WHEN YOU SWAP THEM.
 1. Possible Causes
_______________
 - SERVO CTL-L AILERON, OUTBD B (33CE3)

 - ELAC-1 (2CE1)

 - solenoid valve of the servo control (33CE3)

 - wiring of the SOL VLV signal from the servo control (33CE3) to the ELAC1 (2CE1)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-14-51-000-001 Removal of the Aileron Servo Control AMM 27-14-51-000-004 Removal of the Aileron Servo-Control Solenoid Valve AMM 27-14-51-400-001 Installation of the Aileron Servo Control AMM 27-14-51-400-004 Installation of the Aileron Servo-Control Solenoid
 Valve
 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) R AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground R Power Supply
 AMM 29-10-00-864-003  Depressurize the Blue Hydraulic System
 AMM 29-23-00-863-001  Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
 AMM 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump
 AMM 29-24-00-864-001 Depressurize the Yellow Hydraulic System
 ASM 27-93/02

 3. Fault Confirmation
__________________
 A. Job Set-Up
 (1) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-863-003), (Ref. AMM TASK 29-23-00-863-001), (Ref. AMM TASK 29-24-00-863-001).
 「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 216
 May 01/00 CES

 B. Test

 (1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 NOTE : Before you push the line key adjacent to the START GROUND SCAN
　
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