- wiring of the SV signal from the servo control (33CE2) to the ELAC 1 (2CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-14-51-000-003 Removal of the Aileron Servo-Control Servovalve 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)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/02
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).
「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 241
Aug 01/05 CES 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.
(2) On the EWD, if the F/CTL AIL SERVO FAULT warning stays in view:
- replace the servovalve of the servocontrol (33CE2), (Ref. AMM TASK 27-14-51-000-003) and (Ref. AMM TASK 27-14-51-400-003).
(3) On the panel 23VU, release and push the FLT CTL/ELAC 1 pushbutton switch.
(4) On the EWD, if the F/CTL AIL SERVO FAULT warning stays in view:
- do a check and repair the wiring of the SV signal from the servo control (33CE2) to the ELAC 1 (2CE1), (Ref. ASM 27-93/02).
**ON A/C 301-399,
A. If the test confirms the fault:
- 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.
(2) On the EWD, if the F/CTL AIL SERVO FAULT warning stays in view:
- replace the servovalve of the servocontrol (33CE2), (Ref. AMM TASK 27-14-51-000-003) and (Ref. AMM TASK 27-14-51-400-003).
(3) On the panel 23VU, release and push the FLT CTL/ELAC 1 pushbutton switch.
(4) On the EWD, if the F/CTL AIL SERVO FAULT warning stays in view:
- do a check and repair the wiring of the SV signal from the servo control (33CE2) to the ELAC 1 (2CE1), (Ref. ASM 27-93/02).
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 242
Aug 01/05 CES TASK 27-10-00-810-822
Loss of the Mode Transducer Signal for the Right Green Aileron Servo Control
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- MODE XDCR of the servo control (33CE2)
- wiring of the MODE XDCR SPLY signal from the servo control (33CE2) to the first terminal block
- wiring of the MODE XDCR VS1, VS2 signal from the servo control (33CE2) to the ELAC 1 (2CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-809 Loss of the ACS2 Signal of the ELAC1 MON Side AMM 27-14-51-000-005 Removal of the Linear Variable-Differential Transformer (LVDT) of the Aileron- Servo Control AMM 27-14-51-400-005 Installation of the Linear Variable-Differential
Transformer (LVDT) of the Aileron Servo-Control
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 27-93/02
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本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 1(15)
