____ NO ACCELERATION - ACFT BAT NOT SELECTED / CONTACTOR (5KA) APU Auto Shut Down Fault Code Number: 051
although the A/C batteries are selected ON:
- do a check for continuity of the aircraft wiring from the ECB (59KD) AC/1 to the START CONTACTOR (5KA) B/3 (Ref. ASM 49-42/01).
(1) If there is no continuity:
- repair the aircraft wiring.
(2) If there is continuity:
- do a check for a ground signal (with APU MASTER SW pushed) at the MAIN START CONTACTOR (5KA) B/5 (Ref. ASM 49-42/01).
(a) If there is a ground signal:
- replace the CONTACTOR-MAIN START 5KA.
(b) If there is no ground signal:
1_ If the fault continues:
- replace the ECB 59KD (Ref. AMM TASK 49-61-34-000-002) and
(Ref. AMM TASK 49-61-34-400-002).
- replace the APU MASTER SW (14KD).
1 If the fault continues:
_
- do a check and repair of the aircraft wiring between the MAIN START CONTACTOR (5KA) B5 and the terminal block 2266VT/4 (Ref. AWM 49-42-01).
B. Do the test given in para. 3.
TASK 49-00-00-810-982
PMG Fault (PMG and Cooling Fan Assy) (APS 3200)
1. Possible Causes
_______________
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 49-00-00-710-008 Operational Test of the APU (APS 3200)
3. Fault Confirmation
__________________
A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).
4. Fault Isolation
_______________
A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008). NOTE : After the subsequent flight, make sure that the fault does not
____
continue.
TASK 49-00-00-810-985
Ignition Unit Fault (APS 3200)
1. Possible Causes
_______________
- ECB (59KD)
- IGNITION UNIT (8030KM)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-710-008 Operational Test of the APU (APS 3200)
AMM 49-41-38-000-002 Removal of the Ignition Unit (8030KM) (APS 3200)
AMM 49-41-38-400-002 Installation of the Ignition Unit (8030KM) (APS 3200)
AMM 49-61-34-000-002 Removal of the Electronic Control Box (ECB) (59KD)
(APS 3200) AMM 49-61-34-400-002 Installation of the Electronic Control Box (ECB) (59KD) (APS 3200) ASM 49-61/02
3. Fault Confirmation
__________________
A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).
4. Fault Isolation
_______________
A. If the APU Last Leg Report gives the maintenance message:
IGNITION UNIT (8030KM)
Fault Code Number: 023 or 091
- replace the IGNITION UNIT (8030KM) (Ref. AMM TASK 49-41-38-000-002) and (Ref. AMM TASK 49-41-38-400-002).
(1) If the fault continues:
- do a check and repair the wiring from the ECB (59KD) AB/F7, F6 to the IGNITION UNIT (8030KM) P10/1, 2 (Ref. ASM 49-61/02).
(a) If the fault continues:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-002) and (Ref. AMM TASK 49-61-34-400-002).
B. Do the test given in para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-106, 108-149, 211-299, 301-399, ∞∞49-00-00∞∞∞∞∞∞∞∞∞∞Page A259
Config-2 Aug 01/05 CES
TASK 49-00-00-810-986
Main Start Contactor output open (APS 3200)
1. Possible Causes
_______________
- aircraft wiring
- CONTACTOR-MAIN START (5KA)
- ECB 59KD
- APU MASTER SW (14KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-710-008 Operational Test of the APU (APS 3200) AMM 49-61-34-000-002 Removal of the Electronic Control Box (ECB) (59KD) (APS 3200) AMM 49-61-34-400-002 Installation of the Electronic Control Box (ECB)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 機(jī)載輔助動(dòng)力 1(135)
