曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

 A. Test
 (1) Do the Interface test of the IR (system 3) (Ref. AMM TASK 34-14-00-740-001).
 **ON A/C ALL
 4. Fault Isolation
_______________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. If the test gives the maintenance message GPSSU1 (1SN1):
 - read the POST FLIGHT REPORT for other GPSSU1 (1SN1) maintenance messages (ATA 34-58-31 source IR1, IR2).
 NOTE : In this case the GPSSU1 message is for the GPS part of the MMR1.
____
 (1) If there is a minimum of one maintenance message:
 - replace the MMR-1 (40RT1) (Ref. AMM TASK 34-36-31-000-002) and (Ref. AMM TASK 34-36-31-400-002).
 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 ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 217
 May 01/05 CES

 TASK 34-58-00-810-810
 Loss of the GPSSU2 Input on the ADIRU3

 1. Possible Causes
_______________
 - MMR-2 (40RT2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 34-14-00-740-001 Interface Test of the IR
 AMM 34-36-31-000-002 Removal of the Multi Mode Receiver (40RT1, 40RT2)
 AMM 34-36-31-400-002 Installation of the Multi Mode Receiver (40RT1,

 40RT2)
 3. Fault Confirmation
__________________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. Test
 (1) Do the Interface test of the IR (system 3) (Ref. AMM TASK 34-14-00-740-001).
 **ON A/C ALL
 4. Fault Isolation
_______________ **ON A/C ALL R Post SB 34-1147 For A/C 001-004,051-060,
 A. If the test gives the maintenance message GPSSU2 (1SN2):
 - read the POST FLIGHT REPORT for other GPSSU2 (1SN2) maintenance messages (ATA 34-58-31 source IR1, IR2).
 NOTE : In this case the GPSSU2 message is for the GPS part of the MMR2.
____
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 218
 May 01/05 CES (1) If there is a minimum of one maintenance message:

 - replace the MMR-2 (40RT2) (Ref. AMM TASK 34-36-31-000-002) and (Ref. AMM TASK 34-36-31-400-002).
 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 ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 219
 May 01/05R
 CES

 INTENTIONALLY BLANK

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R ∞∞34-58-00∞∞∞∞∞∞∞∞∞∞Page 220

 **ON A/C ALL
 TASK 34-58-00-810-811
 Loss of the GPSSU1 Data on the ADIRU3
 1. Possible Causes_______________ 
R R  - GPSSU-1 (1SN1) - ADIRU-3 (1FP3) - wiring from the GPSSU1 to the ADIRU3
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R  AMM AMM AMM AMM AMM ASM  34-12-34-000-001 34-12-34-400-001 34-14-00-740-001 34-58-31-000-001 34-58-31-400-001 34-58/01 Removal of the ADIRU (1FP1, 1FP2, 1FP3)Installation of the ADIRU (1FP1, 1FP2, 1FP3)Interface Test of the IR Removal of the GPSSU (1SN1,1SN2) Installation of the GPSSU (1SN1,1SN2) 
3. Fault Confirmation__________________ 
R
 A. Test
 (1) Do the Interface test of the IR (system 3) (Ref. AMM TASK 34-14-00-740-001).

 

R
 4. Fault Isolation_______________ 
R  A. If the test gives the maintenance message GPSSU1 (1SN1)/ADIRU3 (1FP3): 
R  - replace the GPSSU-1 (1SN1) (Ref. AMM TASK 34-58-31-000-001) and (Ref. 
R  AMM TASK 34-58-31-400-001). 
R  (1) If the fault continues: 
R  - replace the ADIRU-3 (1FP3) (Ref. AMM TASK 34-12-34-000-001) and 
R  (Ref. AMM TASK 34-12-34-400-001). 
R  (a) If the fault continues: 
R  - do a check and repair the wiring from the GPSSU1 to the ADIRU3: 
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 導(dǎo)航 NAVIGATION 3(173)