R . Replace the SERVO CTL-R AILERON, INBD G (33CE2) (Ref. R AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-R 400-001).

R . Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001). R - If the resistance values are in the specified limits: R Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001).

R 2_ If the resistance values are in the specified limits:
R a_ Repair the wiring of the SOL VLV signal from the servoR control (33CE2) to the ELAC1 (2CE1) (Ref. ASM 27-93/02).
R b_ Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001).
R (c) If the resistance values are in the specified limits: R - See para. (2).
R (2) At the ELAC1 receptacle, do a check of the insulation between pin R AA/7J (pin AD/10A) and the ground.
R NOTE : The resistance must be more than 100 Megohms
____

R (a) If the resistance is more than 100 Megohms:
R - replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and
R (Ref. AMM TASK 27-93-34-400-001).

R 1_ If the fault continues:
R - replace the solenoid valve (Ref. AMM TASK 27-14-51-000-004)
R and (Ref. AMM TASK 27-14-51-400-004).

R 2_ If the fault continues:
R - replace the SERVO CTL-R AILERON, INBD G (33CE2) (Ref. AMM
R TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-400-001).

R 3_ If the fault continues:
R - Do a check of the wiring from the ELAC-1 (2CE1) MON part
R from pin AE/14E to the first terminal block.
R - Do a check and repair the wiring from the ELAC-1 (2CE1) COM
R part from pin AA/6J to the ground.

R (b) If the resistance is less than 100 Megohms:
R - at the SERVO CTL-R AILERON, INBD G (33CE2), do a check of the
R insulation of the solenoid valve between pin A/H (pin A/T) and
R the ground.

R 1_ If the resistance is less than 100 Megohms:
R - replace the solenoid valve (Ref. AMM TASK 27-14-51-000-004)
R and (Ref. AMM TASK 27-14-51-400-004).

R a_ do again a check of the insulation of the solenoid valve
R between pin A/H (pin A/T) and the ground.
R - If the resistance is less than 100 Megohms:

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 301-399, ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 254
 May 01/04 CES

R  . Replace the SERVO CTL-R AILERON, INBD G (33CE2) (Ref. 
R  AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-
R  400-001). 
R  . Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-
R  001) and (Ref. AMM TASK 27-93-34-400-001). 
R  2_  If the resistance is more tahn 100 Megohms:
R  a_  Repair the wiring of the solenoid valve signal from the
R  SERVO CTL-R AILERON, INBD G (33CE2) to the ELAC-1 (2CE1). 
R  b_  Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001)
R  and (Ref. AMM TASK 27-93-34-400-001). 
R  B. Do the test given in para. 3.

 TASK 27-10-00-810-825
 Loss of the Right Aileron Changeover Signal for the ELAC 1

 1. Possible Causes
_______________
 - ELAC-1 (2CE1)

 - wiring between the COM part and the MON part of the ELAC 1, from DS O3 (COM) to DSI 34 (MON) and from DS O3 (MON) to DSI 34 (COM)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
 AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 ASM 27-92/36

 3. Fault Confirmation
__________________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 A. Test
 Not applicable, you cannot confirm this fault on the ground.
 **ON A/C 301-399,

 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
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 A. Replace the ELAC-1 (2CE1), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
 (1) On the panel 23VU, release and push the FLT CTL/ELAC 1 pushbutton switch.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(20)