• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-20 21:14来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
23-51-00-740-002 BITE Test of the Audio System
 23-51-12-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 23-51-12-865-051
 A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU COM/AUDIO/ACP/F/O 5RN G07 49VU COM/AUDIO/ACP/CAPT 4RN G06 49VU LIGHTING/XFMR/115V.5V/ESS BUS 29LP H03
R  121VU COM NAV/ACP/THIRD/OCCPNT 6RN M02 122VU LIGHTING/ANN LT SPLY/XFMR/BUS 2 27LP X05 122VU LIGHTING/ANN LT SPLY/XFMR/BUS 1 26LP X04 122VU LIGHTING/ANN LT SPLY/XFMR/STAT INV 28LP X03 122VU LIGHTING/INSTL LT/MAIN INST/PNL AND/PED 4LF Y04 122VU LIGHTING/INSTL LT/OVHD/PNL 3LF Y03
 1EFF : ALL 1 23-51-12Page 404 1 1 Feb 01/02 1 1 1CES 1 1EFF : ALL 1 23-51-12Page 405 1 1 Aug 01/05 1 1 1CES 1


 4. Procedure_________
 (Ref. Fig. 401/TASK 23-51-12-991-001)
 Subtask 23-51-12-420-050
 A. Installation of the Audio Control Panel
 NOTE : This installation procedure is applicable to each audio control____ panel.
 (1) Clean the component interface and/or the adjacent area.
 (2) Do an inspection of the component interface and/or the adjacent area.
 (3) Remove blanking caps from the electrical connector (4) and the receptacle (3).
 (4) Make sure that the electrical connector (4) and the receptacle (3) are in the correct condition.
 (5) Connect the electrical connector (4) to the receptacle (3).
 (6) Install the audio control panel (2) in its housing.
 (7) Tighten the Dzus fasteners (1) by a quarter turn.
 Subtask 23-51-12-865-052
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 4RN, 4LF, 28LP, 5RN, 29LP, 6RN, 3LF, 26LP, 27LP
 Subtask 23-51-12-740-050
 C. Do the BITE test of the AMU-ACP (Ref. TASK 23-51-00-740-002). 
R  5. Close-up________ 
R  Subtask 23-51-12-410-050 
R  A. Put the aircraft back to its initial configuration. 
R R  (1) Make sure that the work area is clean and clear of tool(s) and other items.

 

 CODE PANEL - SELCAL (3RN) - REMOVAL/INSTALLATION
________________________________________________ TASK 23-51-13-000-001 Removal of the SELCAL Code Panel (3RN)
 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 access platform 1.6 m (5 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-51-13-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 23-51-13-010-050
 A. Get Access
 (1)
 Put the access platform in position at the access door 824 in the zone 128.

 (2)
 Open the access door 824.


 1EFF : ALL 1 23-51-13Page 401 1 1 Feb 01/98 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 401/TASK 23-51-13-991-001) Subtask 23-51-13-020-050
 A. Removal of the SELCAL Code Panel
 (1)
 Write the code which is in view on the SELCAL code panel (3).

 (2)
 Loosen the fasteners (2) by one quarter turn.

 (3)
 Pull the SELCAL code panel (3) from its housing.

 (4)
 Disconnect the connector (4) from the receptacle (1).

 (5)
 Remove the SELCAL code panel (3).

 (6)
 Put blanking caps on the connector (4) and on the receptacle (1).


 1EFF : ALL 1 23-51-13Page 402 1 1 Feb 01/98 1 1 1CES 1


 SELCAL Code Panel
 Figure 401/TASK 23-51-13-991-001
 1EFF :  ALL  1  23-51-13 Page 403 
1  1  Feb 01/98
 1  1
 1CES  1

 

 TASK 23-51-13-400-001
 Installation of the SELCAL Code Panel (3RN)
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM Communications 通讯3(3)