R Y ELEV MODE XDCR 34CE2
THS ACTR XDCR2 MON 9CE
- do this trouble shooting procedure (Ref. TASK 27-90-00-810-820).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
L G ELEV MODE XDCR 34CE1
- do the trouble shooting procedure (Ref. TASK 31-32-00-810-933) related R to the ANI 7-X analog input signal of the ELAC MON and SEC MON (Ref. R ASM 27-93/07) and (Ref. ASM 27-94/07).
(1) If the fault continues:
- replace the mode selector valve transducer of the servocontrol (34CE1) (Ref. AMM TASK 27-34-51-000-006) and (Ref. AMM TASK 27-34-51-400-005).
NOTE : The resistance of primary and secondary windings must be
____
between 30 ohms and 500 ohms.
(2) If the fault continues:
(a) Do a check of the wiring of the MODE XDCR SPLY signal from the servocontrol (34CE1) to the first terminal block (Ref. ASM 27-93/07):
- if there is continuity, see Para. (b)
- if there is no continuity, repair the above wiring.
(b) Repair the wiring of the MODE XDCR V1 signal from the servocontrol (34CE1) to the first terminal block (Ref. ASM 27-93/07).
B. Do the tests given in Para. 3.
Loss of the Left Green Elevator-Servocontrol Mode-Transducer by the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- wiring of the L G SERVO CTL MODE POS (ANI 7-1) from SEC 1 (1CE1) MON part to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-818 Loss of the ACS1 Signal of the SEC1 MON Side
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 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).
(a) If the ground scanning gives the maintenance message: SEC1 OR WIRING FROM L G ELEV MODE XDCR 34CE1
- refer to Para. Fault Isolation.
(b) If the ground scanning gives at least two maintenance messages of the list below: SEC1 OR WIRING FROM L ELEV POS MON XDCR SEC1 OR WIRING FROM R ELEV POS MON XDCR SEC1 MON OR WIRING FROM THS ACTR XDCR2 9CE SEC1 OR WIRING FROM L G ELEV MODE XDCR 34CE1 SEC1 OR WIRING FROM R Y ELEV MODE XDCR 34CE2
「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 238
Aug 01/00R CES
- do this trouble shooting procedure (Ref. TASK 27-90-00-810-818).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
SEC1 OR WIRING FROM L G ELEV MODE XDCR 34CE1
- 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:
- do a check and repair the wiring of the L G SERVO CTL MODE POS (ANI 7-1) from SEC 1 (1CE1) MON part to the first terminal block (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 239
Aug 01/00R
CES Loss of the Signal of the Left Green Elevator-Servocontrol Solenoid Valve by the SEC 1
CAUTION : DO NOT SWAP FLIGHT CONTROL COMPUTERS. IF THERE IS A SHORT CIRCUIT,
_______ YOU WILL CAUSE DAMAGE TO A SERVICEABLE COMPUTER WHEN YOU SWAP THEM.
1. Possible Causes
_______________
- SERVO CTL-L ELEVATOR, INBD G (34CE1)
- SEC-1 (1CE1)
- solenoid valve of the servocontrol 34CE1
- wiring of the SOL VLV2 signal from the servocontrol (34CE1) to the SEC1 (1CE1) 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 1(50)
