(Activation for the BITE Test)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/07
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).
「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page A217
Feb 01/03 CES
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
A. If the test gives the maintenance message:
ELAC 1 COM OR WIRING TO L B ELEV SERVO VLV 34CE3
- replace the ELAC-1 (2CE1) (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 (Ref. AMM TASK 27-34-51-000-008) and (Ref. AMM TASK 27-34-51-400-003).
(2) If the fault continues:
(a) Do a check of the wiring of the L ELEV SV (ANO 1) signal from the ELAC 1 (2CE1) COM part, pins AB/2E, 2D to the ELAC 1 COM part, pins AA/2H, 2G (Ref. ASM 27-93/07):
- if there is continuity see Para. (b)
- if there is no continuity repair the above wiring.
(b) Do a check of the wiring from the ELAC 1 (2CE1) COM part to the MON part from pins AA/2J, 2K to pins AD/3A, 4A (Ref. ASM 27-93/07):
- if there is continuity see Para. (c)
- if there is no continuity repair the above wiring.
(c) Do a check of the wiring from the ELAC 1 (2CE1) MON part, pins AD/3C, 4C to the first terminal block (Ref. ASM 27-93/07).
- if there is continuity see Para. (d)
- if there is no continuity repair the above wiring.
(d) Do a check of the wiring of the LVDT SV SPLY signal, from the servocontrol (34CE3) to the first terminal block (Ref. ASM 27-93/07).
- if there is continuity see Para. (e)
- if there is no continuity repair the above wiring.
(e) Do a check of the wiring of the LVDT POS (ANI 3-1) signal, from the ELAC 1 (2CE1) MON part to the servocontrol (34CE3) (Ref. ASM 27-93/07).
- if there is continuity see Para. (3)
- if there is no continuity repair the above wiring.
(3) Replace the SERVO CTL-L ELEVATOR, OUTBD B (34CE3) (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
R **ON A/C 106-149, 215-299, 301-399, 401-499,
A. If the test gives the maintenance message:
ELAC 1 COM OR WIRING TO L B ELEV SERVO VLV 34CE3
- replace the ELAC-1 (2CE1) (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 of the wiring of the L ELEV SV (ANO 1) signal from the ELAC 1 (2CE1) COM part, pins AB/2E, 2D to ELAC 1 COM part pins AA/2H, 2G (Ref. ASM 27-93/07):
- if there is continuity see Para. (b)
- if there is no continuity repair the above wiring.
(b) Do a check of the wiring from the ELAC 1 (2CE1) COM part to the MON part from pins AA/2J, 2K to pins AD/3A, 4A (Ref. ASM 27-93/07):
- if there is continuity see Para. (c)
- if there is no continuity repair the above wiring.
(c) Repair the wiring from the ELAC 1 (2CE1) MON part, pins AD/3C, 4C to the first terminal block (Ref. ASM 27-93/07).
**ON A/C ALL
B. Do the test given in Para. 3.
Loss of the Signal of the Left Blue Elevator-Servocontrol Servovalve by the ELAC 1
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- XDCR UNIT-ELEV POS, L (49CE1)
- SERVO CTL-L ELEVATOR, OUTBD B (34CE3)
- servovalve
- wiring of the POS XDCR (ANI 3-1) signal from the ELAC 1 (2CE1) to the first terminal block
- wiring of the POS XDCR MON signal from the transducer unit (49CE1) to the ELAC 1 (2CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 3(24)
