- if the wiring is not correct, repair the above wiring.
14 Do a check of the wiring of the DSI 17 signal from the ELAC1
__ (2CE1) COM part to the MON part (Ref. ASM 27-92/44).
- if the wiring is correct, see Para. 15_.
- if the wiring is not correct, repair the above wiring.
15 Do a check of the wiring of the PIN PROGRAM ELAC1 signal from
__ the ELAC1 (2CE1) COM part and MON part to the ground terminal (Ref. ASM 27-92/40).
(d) If the fault continues:
1 Do a check of the wiring of the PWR SPLY + 28VDC signal from
_ the ELAC1 (2CE1) COM part and MON part to the first terminal block (Ref. ASM 27-92/02).
- if there is continuity, see Para. 2_.
- if there is no continuity repair the above wiring.
2 Do a check of the wiring of the PWR SPLY GND signal from the
_ ELAC1 (2CE1) COM part and MON part to the ground terminal (Ref. ASM 27-92/02).
- if there is continuity, see Para. 3_.
- if there is no continuity, repair the above wiring.
3 Do a check of the wiring of the CTL + 28VDC and ELAC1 ENGAGED
_ (DSI 50) signals from the ELAC1 (2CE1) COM part and MON part to the pushbutton switch (6CE1) (Ref. ASM 27-92/02).
- if there is continuity, see Para. 4_.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B208
201-299, 401-499, Aug 01/05 CES
- if there is no continuity, repair the above wiring.
4 Do a check of the wiring from the pushbutton switch (6CE1) pin
_ A/C3 to the first terminal block (Ref. ASM 27-92/02).
- if there is continuity, see Para. 5_.
- if there is no continuity, repair the above wiring.
5 Replace the P/BSW-FLT CTL/ELAC 1 (6CE1) (Ref. IPC 27920802).
_
R **ON A/C 301-399,
R A. If the test confims the fault:
R - Do the operational test of the ELACs (Ref. AMM TASK 27-93-00-710-001)
R to make sure that the ELAC 1 servoes its associated surfaces.
R (1) If the flight controls move according to the ELAC 1 servoing:
R (a) Remove the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001).
R (b) At the ELAC 1 receptacle, do a check of the resistance between
R pin AB/11J and pin AE/14C (Ref. ASM 27-92/03).
R 1_ If the resistance is less than 280 ohms:
R a_ Remove the RELAY-ELAC 1 ANN SPLY (40CE1) (Ref. IPC
R 27920803).
R b_ Do a check of the resistance of the relay between pin X1
R and pin X2.
R - If the resistance is less than 280 ohms:
R . replace the RELAY-ELAC 1 ANN SPLY (40CE1) (Ref. IPC
R 27920803)
R . replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-400-R 001).
R - If the resistance is between 280 and 400 ohms:
R . do a check and repair the wiring of the RLY ELAC FAULT
R signal from the relay to the ELAC 1 (Ref. ASM 27-92/03)
R . install the relay
R . replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-400-R 001).
R 2_ If the resistance is more than 400 ohms:
R a_ Remove the relay 40CE1.
R b_ Do a check of the resistance of the relay between pins X1
R and X2.
R - If the resistance is more than 400 ohms:
R . replace the RELAY-ELAC 1 ANN SPLY (40CE1) (Ref. IPC R 27920803)
R . install the ELAC 1 (Ref. AMM TASK 27-93-34-400-001).
「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 B209
May 01/04 CESR - If the resistance is between 280 and 400 ohms:
R . do a check and repair the wiring of the RLY ELAC FAULT R signal from the relay to the ELAC 1. (Ref. ASM 27-92/03)
R . install the relay
R . install the ELAC 1 (Ref. AMM TASK 27-93-34-400-001).
R 3_ If the resistance is between 280 and 400 ohms:
R a_ Remove the FCDC-1 (3CE1) (Ref. AMM TASK 27-95-34-000-001).R - if the warning ELAC1 stays:
R . install the FCDC-1 (3CE1) (Ref. AMM TASK 27-95-34-400-R 001).
R . continue the trouble shooting at Para. b_.
R - if the warning ELAC1 goes off, replace the FCDC-2 (3CE2)
R (Ref. AMM TASK 27-95-34-000-001) and (Ref. AMM TASK 27-R 95-34-400-001).
R - install the ELAC 1 (Ref. AMM TASK 27-93-34-400-001).
R b_ Remove the FCDC-2 (3CE2) (Ref. AMM TASK 27-95-34-000-001).R - if the warning ELAC1 stays:
R . install the FCDC-2 (3CE2) (Ref. AMM TASK 27-95-34-400-R 001). 中國(guó)航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 3(58)
