(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 256
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 R B ELEV SERVO VLV 34CE4
- 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, R (49CE2) (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 34CE4 (Ref. AMM TASK 27-34-51-000-008) and (Ref. AMM TASK 27-34-51-400-003).
(3) If the fault continues:
- Replace the SERVO CTL-R ELEVATOR, OUTBD B (34CE4) (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 the LVDT SV V1 signal from the servocontrol (34CE4) 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 LVDT SV SPLY signal from the servocontrol (34CE4) 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.
(c) Repair the wiring of the POS RVDT MON signal from the transducer unit (49CE2) 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 257
Aug 01/00R CES
Failure of the Right Blue Elevator-Servocontrol Mode-Transducer
1. Possible Causes
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- mode selector valve transducer of the servocontrol (34CE4)
- wiring of the MODE XDCR SPLY signal from the servocontrol (34CE4) to the first terminal block
- wiring of the MODE XDCR V1 signal from the servocontrol (34CE4) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-824 Loss of the ACS1 Signal of the ELAC2 MON Side and
SEC2 MON Side 31-32-00-810-933 Failure of the Analog Links AMM 27-34-51-000-006 Removal of the Elevator Servo Control Actuator Mode
Selector Valve Transducer MSVT AMM 27-34-51-400-005 Installation of the Elevator Servo Control Actuator Mode Selector Valve Transducer MSVT 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) R ASM 27-93/08 R ASM 27-94/08
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). 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(57)
