CONTROL AND MONITORING ((GTCP 36-300)) - FAULT ISOLATION PROCEDURES
___________________________________________________________________ R **ON A/C 001-003, 051-099, 401-499,
TASK 49-61-00-810-801
ECB 59KD Fault (GTCP 36-300)
1. Possible Causes
_______________
- ECB (59KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)
3. Fault Confirmation
__________________
A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
4. Fault Isolation
_______________
**ON A/C 001-003, 051-062,
A. If the test gives the maintenance message ECB 59KD:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
R **ON A/C 063-099, 401-499,
A. If the test gives the maintenance message ECB 59KD:
with the associated Fault Code Number(s):
011 - 014, 040, 044, 048, 050, 056, 174, 175, 231, 232, 234, 235, 237,
238
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-003, 051-099, 401-499, ∞∞49-61-00∞∞∞∞∞∞∞∞∞∞Page 201
Config-1 Aug 01/05 CESR **ON A/C 001-003, 051-099, 401-499,
B. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004). NOTE : Make an entry in the applicable logbook that you must read the APU
____ CLASS 3 FAULTS after the first flight on the subsequent day.
R **ON A/C 063-099, 401-499,
TASK 49-61-00-810-802
Incorrect PIN Coding (GTCP 36-300)
1. Possible Causes
_______________
- aircraft wiring
- ECB (59KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-710-001 Self-Test of the ECB (59KD) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) ASM 49-61/01
3. Fault Confirmation
__________________
A. Do the self test of the ECB (59KD) (Ref. AMM TASK 49-00-00-710-001).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
WRG: ACFT TYPE PIN PROG / ECB 59KD
with the LRU TROUBLE SHOOT DATA menu information:
A/C PIN CODING DISAGREE
Fault Code Number: 095
- do a check and make sure that the two A321 IDENTIFICATION signals at the ECB (59KD) AB/A12,A13 (Ref. ASM 49-61/01) are the same.
(1) If the two A321 IDENTIFICATION signals are not the same:
- do a check and repair of the aircraft wiring to the ECB (59KD) AB/A12,A13 to GND (Ref. ASM 49-61/01).
(a) If the fault continues after the first flight on the subsequent day:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 063-099, 401-499, ∞∞49-61-00∞∞∞∞∞∞∞∞∞∞Page 203
Config-1 Aug 01/05 CES (2) If the two A321 IDENTIFICATION are the same:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
B. Do the test given in para. 3.
CONTROL AND MONITORING ((131-9(A))) - FAULT ISOLATION PROCEDURES
________________________________________________________________
TASK 49-61-00-810-806
Incorrect Pin Coding (131-9(A))
1. Possible Causes
_______________
- A/C PIN CODING DISAGREES
- aircraft wiring
- ECB (59KD)
中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 机载辅助动力 2(151)
