- if there is no continuity, repair the above wiring.
(b) Repair the wiring from the SEC 1 (1CE1) MON part, pins AD/1F, 1G to the first terminal block (Ref. ASM 27-94/07).
B. Do the tests given in Para. 3.
Loss of the Signal of the Left Blue Elevator-Servocontrol Servovalve by the SEC
1. Possible Causes
_______________
- SEC-1 (1CE1)
- XDCR UNIT-ELEV POS, L (49CE1)
- SERVO CTL-L ELEVATOR, OUTBD B (34CE3)
- servovalve of the servocontrol 34CE3
- wiring of SV XDCR V1 signal from the servocontrol (34CE3) to the SEC 1 (1CE1)
- wiring of the SV XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block
- wiring of the POS XDCR MON signal from the transducer unit (49CE1) to the SEC 1 (1CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 27-34-51-000-001 Removal of the Elevator Servo Control AMM 27-34-51-000-008 Removal of the Elevator Servo Control Actuator Servo Valve R AMM 27-34-51-400-001 Installation of the Elevator Servo Control AMM 27-34-51-400-003 Installation of the Elevator Servo Control Actuator Servo Valve AMM 27-92-13-000-001 Removal of the Elevator Servocontrol Position Transducer Unit 49CE1, 49CE2 AMM 27-92-13-400-001 Installation of the Elevator Servocontrol Position
Transducer Unit 49CE1, 49CE2
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
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 27-94/07
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).
NOTE : Before you start the operational test procedure, release the
____ FLT CTL/ELAC 1, FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton
「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 213
Aug 01/03 CES switches (on these pushbutton switches the OFF legends come on).
(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:
SEC1 MON OR WIRING TO L B ELEV SERVO VLV 34CE3
- replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
(a) replace the XDCR UNIT-ELEV POS, L (49CE1) (Ref. AMM TASK 27-92-13-000-001) and (Ref. AMM TASK 27-92-13-400-001).
(2) If the fault continues:
- replace the servovalve of the servocontrol 34CE3 (Ref. AMM TASK 27-34-51-000-008) and (Ref. AMM TASK 27-34-51-400-003).
(3) If the fault continues:
(a) 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).
(4) If the fault continues:
(a) Do a check of the wiring of SV XDCR V1 signal from the servocontrol (34CE3) to the SEC 1 (1CE1) (Ref. ASM 27-94/07):
- if there is continuity, see Para. (b)
- if there is no continuity, repair the above wiring.
(b) Do a check of the wiring of the SV XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block (Ref. ASM 27-94/07):
- if there is continuity, see Para. (c)
- if there is no continuity, repair the above wiring.
R (c) Check and repair the wiring of the POS XDCR MON signal from the R transducer unit (49CE1) to the SEC 1 (1CE1) (Ref. ASM 27-94/07):
B. Do the tests 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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 214
May 01/01 CES Failure of the Left Blue Elevator-Servocontrol Mode-Transducer
1. Possible Causes
_______________
- mode selector valve transducer of the servocontrol (34CE3)
- wiring of the MODE XDCR SPLY signal from the servocontrol (34CE3) to the first terminal block 中國航空網 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(41)
