3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
B. Test
(1) Do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).
4. Fault Isolation
_______________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
A. If the test gives the maintenance message AFS: SFCC1-FAC1 CKT:
- 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 SLATS EXTD discrete from the FAC 1 (1CC1) to the first terminal block (Ref. ASM 22-68/01).
「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 267
Aug 01/05 CES
R **ON A/C 301-399,
R A. If the test gives the maintenance message AFS: FAC1-SFCC1 CKT:
R - replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM
R TASK 22-66-34-400-002).
R (1) If the fault continues:
R - do a check and repair the wiring of the SLATS EXTD discrete from
R the FAC 1 (1CC1) to the first terminal block (Ref. ASM 22-68/01).
R **ON A/C ALL
B. Do the test given in Para. 3.
Loss of the Reception of the SFCC 2 SLATS EXTD Discrete by the FAC 2
1. Possible Causes
_______________
- FAC-2 (1CC2)
- wiring of the SLATS EXTD discrete from the FAC 2 (1CC2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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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 22-91-00-710-001 Ground Scanning of the AFS
ASM 22-68/01
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
B. Test
(1) Do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).
4. Fault Isolation
_______________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
A. If the test gives the maintenance message AFS: SFCC2-FAC2 CKT:
- replace the FAC-2 (1CC2) (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 SLATS EXTD discrete from the FAC 2 (1CC2) to the first terminal block (Ref. ASM 22-68/01).
「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 269
Aug 01/05 CES
R **ON A/C 301-399,
R A. If the test gives the maintenance message AFS: FAC2-SFCC2 CKT:
R - replace the FAC-2 (1CC2) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM
R TASK 22-66-34-400-002).
R (1) If the fault continues:
R - do a check and repair the wiring of the SLATS EXTD discrete from
R the FAC 2 (1CC2) to the first terminal block (Ref. ASM 22-68/01).
R **ON A/C ALL
B. Do the test given in Para. 3
Loss of the Reception of the ADIRU 1 Bus by One FAC or One FMGC
1. Possible Causes
_______________
- FAC-1 (1CC1)
- FAC-2 (1CC2)
- FMGC-1 (1CA1)
- FMGC-2 (1CA2)
- rejection of ADR parameters due to excessive offset 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 AUTO FLIGHT 自動飛行2(23)
