A320 Trouble Shooting Manual 排故手册 导航 NAVIGATION 1(6)

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 3. Fault Confirmation
__________________
 A. Test Do the Interface test of the ADR (system 1) (Ref. AMM TASK 34-13-00-740-002).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ADM4 (19FP4)/ADIRU1 (1FP1):
 - replace the ADM-R STATIC PRESSURE (19FP4) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
 (1) If the fault continues:
 - replace the ADIRU-1 (1FP1) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (a) If the fault continues:
 - do a check and repair the wiring of the ADM BUS 3 INPUT bus from R static pressure ADM (19FP4) to the ADIRU1 (1FP1) (Ref. ASM 34-13/03).
 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 ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 212
 May 01/04R CES

 Loss of the ADM BUS 1 Input Data to the ADIRU 2
 1. Possible Causes
_______________
 - ADM-R TOTAL PRESSURE (19FP2)

 - ADIRU-2 (1FP2)

 - wiring of the ADM BUS 1 INPUT bus from the R total pressure ADM (19FP2) to the ADIRU 2 (1FP2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-11-17-000-001 Removal of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-11-17-400-001 Installation of the Air Data Module
 (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-13-00-740-002 INTERFACE TEST of the ADR ASM 34-13/03
 3. Fault Confirmation
__________________
 A. Test Do the Interface test of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ADM2 (19FP2)/ADIRU2 (1FP2):
 - replace the ADM-R TOTAL PRESSURE (19FP2) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
 (1) If the fault continues:
 - replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (a) If the fault continues:
 - do a check and repair the wiring of the ADM BUS 1 INPUT bus from the R total pressure ADM (19FP2) to the ADIRU 2 (1FP2) (Ref. ASM 34-13/03).
 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 ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 213
 May 01/04R CES

 Loss of the ADM BUS 2 Input Data to the ADIRU 2
 1. Possible Causes
_______________
 - ADM-L STATIC PRESSURE (19FP7)

 - ADIRU-2 (1FP2)

 - wiring of the ADM BUS 2 INPUT bus from the L static pressure ADM (19FP7) to the ADIRU 2 (1FP2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-11-17-000-001 Removal of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-11-17-400-001 Installation of the Air Data Module
 (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-13-00-740-003 SYSTEM TEST of the ADR ASM 34-13/03
 3. Fault Confirmation
__________________
 A. Test Do the System test of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-003).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ADM7 (19FP7)/ ADIRU2 (1FP2):
 - replace the ADM-L STATIC PRESSURE (19FP7) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
 (1) If the fault continues:
 - replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
 (a) If the fault continues:
 - do a check and repair the wiring of the ADM BUS 2 INPUT bus from the L static pressure ADM (19FP7) to the ADIRU 2 (1FP2) (Ref. ASM 34-13/03).
 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 ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 214
　
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