「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 217
Nov 01/99 CESR - do this trouble shooting procedure (Ref. TASK 27-90-00-810-R 822).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
SEC2 OR WIRING FROM L B ELEV MODE XDCR 34CE3
- replace the SEC-2 (1CE2) (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 B SERVO CTL MODE POS (ANI 7-1) from the SEC 2 (1CE2) MON part to the first terminal block (Ref. ASM 27-94/08).
B. Do the tests given in Para. 3.
Loss of the Signal of the Left Blue Elevator-Servocontrol Solenoid Valve by the SEC 2
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
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- SERVO CTL-L ELEVATOR, OUTBD B (34CE3)
- SEC-2 (1CE2)
- solenoid valve of the servocontrol 34CE3
- wiring of the SOL VLV2 signal from the servocontrol (34CE3) to the SEC2 (1CE2)
- wiring from the SEC2 (1CE2) COM part to the SEC2 MON part
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 27-34-51-000-001 Removal of the Elevator Servo Control
AMM 27-34-51-000-005 Removal of the Elevator Servo Control Actuator R Solenoid Valve R AMM 27-34-51-400-001 Installation of the Elevator Servo Control
AMM 27-34-51-400-004 Installation of the Elevator Servo Control Actuator
R Solenoid Valve 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 27-94/08
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).
NOTE : Before you start the operational test procedure, release the
____ FLT CTL/ELAC 1 and FLT CTL/ELAC 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).
「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 219
Aug 01/03 CES
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
SEC2 MON OR WIRING TO L B ELEV SOL VLV 34CE3
(1) Remove the SEC2 (Ref. AMM TASK 27-94-34-000-001).
(2) At the SEC2 receptacle, do a check of the resistance between the pin AB/14D and the pin AE/14G (Ref. ASM 27-94/08).
NOTE : The resistance must be between 40 and 100 Ohms.
____
(a) If the resistance is less than 40 Ohms:
- at the outboard elevator servocontrol (34CE3), do a check of the resistance of the solenoid valve between the pin C/J and the pin C/U (Ref. ASM 27-94/08).
NOTE : The resistance must be between 40 and 100 Ohms.
____
1 If the resistance values are out of the specified limits:
_ a Replace the solenoid valve of the servocontrol 34CE3 (Ref.
_ AMM TASK 27-34-51-000-005) and (Ref. AMM TASK 27-34-51-400-004).
b Do again a check of the resistance of the solenoid valve
_ between the pin C/J and the pin C/U of the outboard elevator servocontrol (34CE3) (40 to 100 Ohms).
- If the resistance values are out of the specified limits: . 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). . Replace the SEC-2 (1CE2) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
- If the resistance values are in the specified limits: Replace the SEC-2 (1CE2) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
2 If the resistance values are in the specified limits:
_ a Repair the wiring of the SOL VLV2 signal from the
_ servocontrol (34CE3) to the SEC2 (1CE2), from the pin C/J to the pin AB/14D and from the pin C/U to the pin AE/14G (Ref. ASM 27-94/08): 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 飞行操纵 1(43)
