- wiring
- DEU mount 2010VU16
- DEU mount 2010VU12
- DEU mount 2010VU8
- DEU mount 2010VU4
- DEU mount 2014VU4
- DEU mount 2010VU22
- DEU mount 2010VU18
- DEU CONNECTION BOX (208RH10)
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CES
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 23-73-00-740-005 BITE Test of the Cabin Intercommunication Data System (CIDS) through the CFDS AMM 23-73-00-740-010 Interface and Power-Up Test of the Cabin
Intercommunication Data System (CIDS) via the CFDS AMM 23-73-34-000-001 Removal of the CIDS Director (101RH,102RH) AMM 23-73-34-400-001 Installation of the CIDS Director (101RH,102RH) AMM 23-73-42-000-001 Removal of the Connection Box AMM 23-73-42-400-001 Installation of the Connection Box AMM 23-73-43-000-001 Removal of the Termination Box AMM 23-73-43-400-001 Installation of the Termination Box AMM 23-73-46-000-001 Removal of the Decoder/Encoder Unit (DEU) A 200RH AMM 23-73-46-400-001 Installation of the Decoder/Encoder Unit (DEU) A
200RH
AMM 23-73-48-000-001 Removal of the DEU A / DEU B - Mount
AMM 23-73-48-400-001 Installation of the DEU A / DEU B - Mount
ASM 23-73/06
ASM 23-73/06
3. Fault Confirmation
__________________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
A. Test
(1) Do the CIDS1/CIDS BUS test through the MCDU/CFDS.
(2) Do the CIDS1/DEU-A test through the MCDU/CFDS.
R **ON A/C 106-149, 301-399, 401-499,
A. Test
(1) Do the CIDS Interface and Power-Up Test via the CFDS (Ref. AMM TASK 23-73-00-740-010).
**ON A/C ALL
4. Fault Isolation
_______________
A. If the test gives a different maintenance message, do the trouble shooting procedure related to the maintenance message.
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**ON A/C 001-049, 051-099, 101-105, 201-299,
B. If the CIDS1/CIDS BUS test gives the maintenance message TOP LINE 1R:
- remove the DIR-CIDS (101RH) (Ref. AMM TASK 23-73-34-000-001),
- make sure that at least one cabin door is open,
- close these CBs:
49VU: 150RH (G02) CIDS/DIR 1 & 2/ESS,
121VU:151RH (M05) CIDS/DIR 1 & 2/NORM,
- wait for approx. 120 s,
- do the CIDS2/CIDS BUS test through the MCDU/CFDS.
(1) If the CIDS2/CIDS BUS test is OK:
- install a new DIR-CIDS, 1 (101RH) (Ref. AMM TASK 23-73-34-400-001).
(2) If the fault continues:
- remove the DIR-CIDS, 2 (102RH) (Ref. AMM TASK 23-73-34-000-001).
- install the DIR-CIDS, 1 (101RH) (Ref. AMM TASK 23-73-34-400-001).
- do the CIDS1/CIDS BUS test through the MCDU/CFDS.
(3) If the CIDS1/CIDS BUS test is OK:
- install a new DIR-CIDS, 2 (102RH) (Ref. AMM TASK 23-73-34-400-001).
(4) If the fault continues:
- remove the DIR-CIDS, 1 (101RH) (Ref. AMM TASK 23-73-34-000-001)
- open these CBs: 49VU: 154RH COM/CIDS/DEU A ESS/LINE 1 49VU: 155RH COM/CIDS/DEU A ESS/LINE 2 121VU: 164RH COM NAV/CIDS/DEU A NORM/R FWD 121VU: 166RH COM NAV/CIDS/DEU A NORM/R MID 121VU: 168RH COM NAV/CIDS/DEU A NORM/R AFT
- make sure that the resistance (line to line) at DIR-CIDS (101RH) and (102RH) connector AA/A15 and connector AA/B15 is between approx. 80 and 200 ohms (Ref. ASM 23-73/06).
(5) If the resistance (line to line) is between approx. 80 and 200 ohms:
- make sure that the resistance (line to GND) is not less than 50 ohms (short circuit) between: DIR-CIDS (101RH) and (102RH) connector AA/A15 and GND, DIR-CIDS (101RH) and (102RH) connector AA/B15 and GND. (Ref. ASM 23-73/06)
(a) If there is no short circuit:
- remove the DEU-A (200RH24) (Ref. AMM TASK 23-73-46-000-001)
- install the DIR-CIDS (101RH) and DIR-CIDS (102RH) (Ref. AMM TASK 23-73-34-400-001).
- close these CBs: 49VU: 154RH COM/CIDS/DEU A ESS/LINE 1 49VU: 155RH COM/CIDS/DEU A ESS/LINE 2 121VU: 164RH COM NAV/CIDS/DEU A NORM/R FWD 121VU: 166RH COM NAV/CIDS/DEU A NORM/R MID 121VU: 168RH COM NAV/CIDS/DEU A NORM/R AFT 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 COMMUNICATIONS 通訊2(83)
