B. After the subsequent flight, if the fault continues:
 - replace the ADM-STBY STATIC PRESSURE (19FP8) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).
 C. After the subsequent flight, if the fault continues:
 - replace the ADM-L STATIC PRESSURE (19FP5).
 D. After the subsequent flight, if the fault continues:
 - replace the ADM-R STATIC PRESSURE (19FP4).
 E. After the subsequent flight, if the fault continues:
 - replace the ADM-L STATIC PRESSURE (19FP7).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 204-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 266
 401-499, Aug 01/05 CES

 F. After the subsequent flight, if the fault continues:
 - replace the ADM-R STATIC PRESSURE (19FP6).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 204-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 267
 401-499, Aug 01/05 CES

 Different Average Static Pressure on the ADIRU 2 and the ADIRU 3
 1. Possible Causes
_______________
 - ADM-L STATIC PRESSURE (19FP7)

 - ADM-R STATIC PRESSURE (19FP6)

 - ADM-STBY STATIC PRESSURE (19FP8)

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific ARINC Reader
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-10-00-170-002 Flushing of the Principal Static Pressure Lines AMM 34-10-00-170-003 Draining and Flushing of Standby Pneumatic Circuits AMM 34-10-00-860-002 ADIRS Start Procedure AMM 34-11-16-000-001 Removal of the Static Probe
 (7DA1,7DA2,7DA3,8DA1,8DA2,8DA3) AMM 34-11-16-400-002 Installation of the Static Probe (7DA1,7DA2,7DA3,8DA1,8DA2,8DA3) 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 34-13-00-790-002 Leak Test of the Principal Static and Total Air Data System ASM 34-13/01
 3. Fault Confirmation
__________________
 A. Test
 Not applicable, you cannot confirm this fault on the ground.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 204-299, 301-399, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page 268
 401-499, Aug 01/05 CES

 4. Fault Isolation
_______________

 A. If the POST FLIGHT REPORT gives the maintenance message ADIRU2 (1FP2)/ ADIRU3 (1FP3):
 - do a visual check of the static probes.
 (1) If one static probe is damaged :

 - replace the defective static probe (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).

 (2) If the static probes are not damaged:

 - do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002)

 - connect the ARINC Reader to the test connector 198VC on the panel 188VU and to the test connector 199VC on the panel 187VU (Ref. ASM 34-13/01)

 - compare the static ADM pressure read on these labels:

 (a) If one value is different:

 - replace the defective static pressure ADM (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001).

 (b) If the values are the same:

 - do the flushing of the static pressure line of the air data module (ADM 6, ADM 7) (Ref. AMM TASK 34-10-00-170-002)

 - do the draining and flushing of the standby static and standby total pressure line of the air data module (Ref. AMM TASK 34-10-00-170-003)

 - do the leak test of the main air data system (CAPT and F/O) (Ref. AMM TASK 34-13-00-790-002).

 ADIRU 2  198VC  |  19FP6  LABEL 177
 pins GG, HH  |  19FP7  LABEL 176
 |
 ADIRU 3  199VC  |  19FP8  LABEL 245
 pins y, z  |
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 1(27)