- do a check and repair the wiring of the ground signal at the FLT CTL/FAC 2 pushbutton switch (12CC2) pin A/A2 (Ref. ASM 22-65/01).
B. Do the test given in Para. 3.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) On the panel 25VU, set the ANN LT switch to BRT.
Loss of the Reception of the ELAC OWN Bus by the FAC 1 MON or the FAC 1 COM
1. Possible Causes
_______________
- FAC-1 (1CC1)
- wiring of the ELAC OWN bus from the FAC 1 (1CC1) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2)
AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2)
AMM 22-96-00-710-001 Operational Test of the AFS
ASM 22-69/01
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
B. Test
(1) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FAC 1.
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS: FAC1/ELAC1 BUS WIRG:
- replace the FAC-1 (1CC1), (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- do a check and repair the wiring of the ELAC OWN bus from the FAC 1 (1CC1) to the first terminal block (Ref. ASM 22-69/01).
B. Do the test 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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page 253
Feb 01/98 CESR **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
TASK 22-66-00-810-843
Loss of the Reception of the ELAC OPP Bus by the FAC 1 MON or the FAC 1 COM
1. Possible Causes
_______________
- FAC-1 (1CC1)
- wiring of the ELAC OPP bus from the FAC 1 (1CC1) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2)
AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2)
AMM 22-96-00-710-001 Operational Test of the AFS
ASM 22-69/01
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
B. Test
(1) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FAC 1.
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS: FAC1/ELAC2 BUS WIRG:
- replace the FAC-1 (1CC1), (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- do a check and repair the wiring of the ELAC OPP bus from the FAC 1 (1CC1) to the first terminal block (Ref. ASM 22-69/01).
B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page 254
201-299, 401-499, Aug 01/05 CESR **ON A/C ALL
TASK 22-66-00-810-844
Loss of the Reception of the ELAC OWN Bus by the FAC 2 MON or the FAC 2 COM
1. Possible Causes
_______________
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AUTO FLIGHT 自動飛行2(17)
