(Activation for the BITE Test)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/03
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:
ELAC 2 COM OR WIRING FROM R B AIL POS XDCR 33CE4
or
ELAC 2 MON OR WIRING FROM R B AIL POS XDCR 33CE4
- replace the ELAC-2 (2CE2), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) If the fault continues:
(a) Do a check and repair the wiring of the ANI 2-4, POS SV R AIL signal from the ELAC 2 (2CE2) to the first terminal block, COM or MON part as shown in the maintenance message (Ref. ASM 27-93/03).
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 260
May 01/04R CES
Loss of the Servovalve Signal for the Right Blue Aileron Servo Control
1. Possible Causes
_______________
- ELAC-2 (2CE2)
- servovalve of the servo control (33CE4)
- wiring of the SV signal from the servo control (33CE4) to the ELAC 2 (2CE2)
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 27-93/03
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:
R B AIL SERVO VLV 33CE4 OR OUTPUT FROM ELAC 2
- replace the ELAC-2 (2CE2), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) If the fault continues:
- replace the servovalve of the servo control (33CE4), (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 261
May 01/04R CES
(2) If the fault continues:
- do a check and repair the wiring of the SV signal from the servo control (33CE4) to the ELAC 2 (2CE2), (Ref. ASM 27-93/03).
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 262
May 01/04R
CES Loss of the Mode Transducer Signal for the Right Blue Aileron Servo Control
1. Possible Causes
_______________
- ELAC-2 (2CE2)
- MODE XDCR of the servo control (33CE4)
- wiring of the MODE XDCR SPLY signal from the servo control (33CE4) to the first terminal block
- wiring of the MODE XDCR VS1, VS2 signal from the servo control (33CE4) to the ELAC 2 (2CE2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-810 Loss of the ACS2 Signal of the ELAC2 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
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 1(22)
