R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-12Page 431 1201-299, 1Config-1 May 01/05 1 1 1CES 1

 (c) Carefully pull the locking-pin (4) at its end and remove it.
 (d) Carefully remove the switchguard (5).
 (e) Carefully pull the brackets (6) until they have the correct position for the new switchguard and hold them in this position.
 (f) Put the new switchguard (5) in position and carefully push the locking-pin (4) into the brackets (6).
 NOTE : Make sure that the locking-pin (4) has the correct____ position and is fully locked.
 Subtask 23-73-12-865-074
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R  **ON A/C 001-049, 051-061, 101-105, 201-203,
 121VU COM NAV/CIDS/FWD ATTND/PNL  170RH  M14 
R  **ON A/C 062-099, 204-299, 
R  121VU COM NAV/CIDS/FWD ATTND/PNL  170RH  Q14 
R  **ON A/C 151-199, 
R  121VU COM /CIDS/FLT ATTND/PNL  170RH  Q14 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
 Subtask 23-73-12-740-058
 C. Do the BITE Test of the Cabin Intercommunication Data System (CIDS) through the PTP (Ref. TASK 23-73-00-740-003). 

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-12Page 432 1201-299, 1Config-1 May 01/05 1 1 1CES 1 Subtask 23-73-12-710-051

 D. Do this (these) test(s) for the pushbuttons(s) where you have replaced the Switchguard(s).
 (1)
 For the Switchguard-replacement of the LIGHT EMER-pushbutton :

 -Do the Operational Test of the EMER LT SYS (Ref. TASK 33-51-00-710-007).

 (2)
 For the Switchguard-replacement of the EVAC CMD-pushbutton :

 -Do the Operational Test of the Emergency Evacuation Signalling System (Ref. TASK 23-73-00-710-004).
 5. Close-up
________
 Subtask 23-73-12-862-056
 A. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-12Page 433 1201-299, 1Config-1 May 01/05 1 1 1CES 1 ATTENDANT PANEL - FORWARD (120RH) - REMOVAL/INSTALLATION

________________________________________________________
 TASK 23-73-12-000-007
 Removal of the Flight Attendant Panel (FAP) 120RH
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-73-00-861-001 Energize the Cabin Intercommunication Data System
 (CIDS) 23-73-19-000-002 Removal of the Cabin Assignment Module (115RH) 23-73-21-000-001 Removal of the On Board Replaceable Module (OBRM)
 116RH 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 31-32-00-860-003 Procedure to Get Access to the SYSTEM REPORT/TEST/COM Page 23-73-12-991-008 Fig. 401
 3. Job Set-up
__________
 Subtask 23-73-12-861-063
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

R 1EFF : 106-149, 301-399, 401-499, 1 23-73-12Page 401 1 1 Config-2 Aug 01/05 1 1 1CES 1 Subtask 23-73-12-970-055

 B. Trouble Shooting Data
 (1)
 Make sure that the Cabin Intercommunication Data System (CIDS) is energized (Ref. TASK 23-73-00-861-001)

 (2)
 If available, you can print the Trouble Shooting Data (TSD) as follows:

 -get access to the SYSTEM REPORT/TEST COM page (Ref. TASK 31-32-00-860-003) - on this page, push the line select key adjacent to the CIDS1 (2) indication.
 - on the CIDS1 (2) page, push the line select key adjacent to the TROUBLE SHOOT DATA indication to get the CIDS 1 (2) TROUBLE SHOOTING DATA page.
 -print the Trouble Shooting Data page.
 Subtask 23-73-12-865-070
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR COND/CIDS/SDF/DIR2 ESS 18WH C06 49VU AIR COND/CIDS/SDF/DIR1 ESS 15WH C05
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM Communications 通訊4(97)