- replace the FMGC-2 (1CA2) (Ref. AMM TASK 22-83-34-000-001) and (Ref. AMM TASK 22-83-34-400-001).
(2) If the fault continues:
- do a check and repair the wiring of the ADC ADIRS OWN and the IRS ADIRS OWN bus from the FMGC 2 (1CA2) to the first terminal block (Ref. ASM 22-86/01).
E. 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 276
May 01/04R CES
Loss of the Reception of the ADIRU 3 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
- wiring of the ADC ADIRS 3 and the IRS ADIRS 3 bus from the FAC 1 (1CC1) to the first terminal block
- wiring of the ADC ADIRS 3 and the IRS ADIRS 3 bus from the FAC 2 (1CC2) to the first terminal block
- wiring of the ADC ADIRS 3 and the IRS ADIRS 3 bus from the FMGC 1 (1CA1) to the first terminal block
- wiring of the ADC ADIRS 3 and the IRS ADIRS 3 bus from the FMGC 2 (1CA2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-861 Different Angle of Attack Value on the three ADIRUs 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 22-83-34-000-001 Removal of the FMGC (1CA1,1CA2) AMM 22-83-34-400-001 Installation of the FMGC (1CA1,1CA2) AMM 22-91-00-710-001 Ground Scanning of the AFS AMM 34-13-00-720-009 Functional Test of the Altitude and Airspeed Data ASM 22-69/01 ASM 22-86/01
「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 277
May 01/04R
CES
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU NAV PROBES/ADIRU3/PWR/SWTG 8FP F09
**ON A/C 001-049, 051-061, 101-105, 201-203,
121VU ADIRS/ADIRU/3PWR/SWTG 9FP N10 121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N08 121VU ADIRS/ADIRU/3/115VAC 4FP3 N06 121VU ADIRS/ADIRU/3/28VDC 6FP3 N04
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
121VU ADIRS/ADIRU/3PWR/SWTG 9FP N09 121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N07 121VU ADIRS/ADIRU/3/115VAC 4FP3 N05 121VU ADIRS/ADIRU/3/28VDC 6FP3 N03
**ON A/C ALL
B. Test
(1) Do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS: ADIRU3 (ISSUED BY: FAC1):
- do the Functional Check of the Altitude/Airspeed Data (Ref. AMM TASK 34-13-00-720-009) to check if there is rejection of ADR parameters due to excessive offset.
(1) If the fault continues:
- replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(2) If the fault continues:
- do the monitoring of the AOA sensors (Ref. TASK 34-11-00-810-861).
(3) If the fault continues:
- do a check and repair the wiring of the ADC ADIRS 3 and the IRS ADIRS 3 bus from the FAC 1 (1CC1) to the first terminal block (Ref. ASM 22-69/01).
「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 278
Aug 01/05 CES B. If the test gives the maintenance message AFS: ADIRU3 (ISSUED BY: FAC2):
- do the Functional Check of the Altitude/Airspeed Data (Ref. AMM TASK 34-13-00-720-009) to check if there is rejection of ADR parameters due to excessive offset.
(1) If the fault continues:
- replace the FAC-2 (1CC2) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
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(26)
