TASK 24-20-00-810-836
Failure of the APU Availability Relay
1. Possible Causes_______________
- GCU-APU (1XS)
- ECB (59KD)
- RELAY-APU AVAIL (6KD)
- wiring
2. Job Set-up Information______________________
A. Referenced Information
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REFERENCE DESIGNATION
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AMM 24-23-34-000-001 Removal of the GCU-APU (1XS)
AMM 24-23-34-400-001 Installation of the GCU-APU (1XS)
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the APU
AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the APU
AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)
AMM 49-61-34-000-002 Removal of the Electronic Control Box (ECB) (59KD) (APS 3200)
AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)
AMM 49-61-34-400-002 Installation of the Electronic Control Box (ECB) (59KD) (APS 3200)
ASM 24-23/02
ASM 49-61/01
3. Fault Confirmation__________________
A. Test
Not applicable.
NOTE : As the APU GEN was set to OFF because of a true failure, the fault
____
confirmation is not necessary.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page 289
201-299, 301-399, Aug 01/05 CES
4. Fault Isolation
_______________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
A. If the fault symptom is identified by the CFDS message CHECK GCU APU PIN A6A APU CTL RLY 6KD CKT and the upper ECAM DU warning APU GEN FAULT:
- replace the RELAY-APU AVAIL (6KD).
(1) If the fault continues:
- do a check of the wiring for open circuit: . between the APU generator pin B/2B and the APU availability relay pin A/2, . then between the APU GCU pin A/6A and the APU availability relay pin A/1, . then between the APU relay pin A/X1 and the ECB pin B/J6 (Ref. ASM 24-23/02) and (Ref. ASM 49-61/01).
(a) If the wiring is not correct:
- repair the above defective wiring.
(b) If the wiring is correct:
- replace the GCU-APU (1XS) (Ref. AMM TASK 24-23-34-000-001) and (Ref. AMM TASK 24-23-34-400-001).
(c) If the fault continues:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).
**ON A/C 106-149, 211-299, 301-399,
A. If the fault symptom is identified by the CFDS message CHECK GCU APU PIN A6A APU CTL RLY 6KD CKT and the upper ECAM DU warning APU GEN FAULT:
- replace the RELAY-APU AVAIL (6KD).
(1) If the fault continues:
- do a check of the wiring for open circuit: . between the APU generator pin B/2B and the APU availability relay pin A/2, . then between the APU GCU pin A/6A and the APU availability relay pin A/1, . then between the APU relay pin A/X1 and the ECB pin B/J6 (Ref. ASM 24-23/02) and (Ref. ASM 49-61/01).
(a) If the wiring is not correct:
- repair the above defective wiring.
(b) If the wiring is correct:
- replace the GCU-APU (1XS) (Ref. AMM TASK 24-23-34-000-001) and (Ref. AMM TASK 24-23-34-400-001).
「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 : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page 290
201-299, 301-399, Aug 01/05 CES (c) 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).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. Make sure that the aircraft electrical circuits operate correctly in APU configuration:
(1) Energize the aircraft electrical circuits from the APU (Ref. AMM TASK 24-41-00-861-002).
(2) De-energize the aircraft electrical circuits from the APU (Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page 291
201-299, 301-399, Aug 01/05 CES
TASK 24-20-00-810-837 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 1(129)
