. Replace the ELAC-2 (2CE2) (Ref. AMM TASK 27-93-34-000-001) (Ref. AMM TASK 27-93-34-400-001).
- If the resistance values are in the specified limits: Replace the ELAC-2 (2CE2) (Ref. AMM TASK 27-93-34-000-001) (Ref. AMM TASK 27-93-34-400-001).
2 If the resistance values are in the specified limits:
_ a Repair the wiring of the SOL VLV signal from the servo
_ control (33CE4) to the ELAC2 (2CE2), (Ref. ASM 27-93/03).
b Replace the ELAC-2 (2CE2), (Ref. AMM TASK 27-93-34-000-001)
_ and (Ref. AMM TASK 27-93-34-400-001).
(b) If the resistance is more than 100 Ohms:
- at the outboard aileron servocontrol (33CE4), do a check of the resistance of the solenoid valve between pin A/H and pin A/T (Ref. ASM 27-93/03).
NOTE : The resistance must be between 40 and 100 Ohms.
____
1 If the resistance values are out of the specified limits:
_ a Replace the solenoid valve of the servo control (33CE4),
_ (Ref. AMM TASK 27-14-51-000-004) and (Ref. AMM TASK 27-14-51-400-004).
b Do again a check of the resistance of the solenoid valve
_ between pin A/H and A/T of the outboard aileron servocontrol (33CE4) (40 to 100 Ohms).
- If the resistance values are out of the specified limits: . Replace the SERVO CTL-R AILERON, OUTBD B (33CE4) (Ref. AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-400-001). . Install the ELAC2 (Ref. AMM TASK 27-93-34-400-001).
- If the resistance values are in the specified limits: Install the ELAC2 (Ref. AMM TASK 27-93-34-400-001).
2 If the resistance values are in the specified limits:
_ a Repair the wiring of the SOL VLV signal from the servo
_ control (33CE4) to the ELAC2 (2CE2), (Ref. ASM 27-93/03).
b Install the ELAC2 (Ref. AMM TASK 27-93-34-400-001).
_
(c) If the resistance values are in the specified limits:
- replace the ELAC-2 (2CE2), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
B. Do the test 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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 269
May 01/04R CES
Loss of the two Aileron Servocontrols on the Left Aileron
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation
__________________
A. Test
Not applicable.
4. Fault Isolation
_______________
A. This warning is shown after the failure of the two aileron servocontrols. To do the trouble shooting, refer to the POST FLIGHT REPORT and start the trouble shooting from the first F/CTL AIL SERVO FAULT warning and its
R related maintenance message. After this step, on the upper ECAM DU the F/CTL L AIL FAULT warning will go out of view and be replaced by the F/CTL AIL SERVO FAULT warning with a related maintenance message. Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001), to know the related maintenance message.
R Do the trouble shooting related to this message.
Loss of the two Aileron Servocontrols on the Right Aileron
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
3. Fault Confirmation
__________________
A. Test
Not applicable.
4. Fault Isolation
_______________
A. This warning is shown after the failure of the two aileron servocontrols. To do the trouble shooting, refer to the POST FLIGHT REPORT and start the trouble shooting from the first F/CTL AIL SERVO FAULT warning and its
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