A320飞机维护手册 AMM 指示/记录系统 5(138)

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

-DB/N:PUSH NEXT/PREV indication is shown
On the Data Loading Selector screen:
-FMGC1NOT SELECTEDindication is shown
On the Data Loading Selector screen:
-FMGCSELECTED indication is shown
On the Data Loading Selector screen:
-FMGC1NOT SELECTED indication is shown
 A. Make sure that the work area is clean and clear of tool(s) and other items.
 Subtask 31-38-21-862-051
 B. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-38-21Page 406 1401-499, 1Aug 01/05 1 1 1CES 1

 MDDU (MULTIPURPOSE DISK DRIVE UNIT) (1TD) - REMOVAL/INSTALLATION
________________________________________________________________ TASK 31-38-22-000-001 Removal of the MDDU (1TD)
 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 -------------------------------------------------------------------------------
24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-38-22-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 31-38-22-862-050
 A. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 Subtask 31-38-22-865-050
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU DATA/LOADER/SPLY 3TD J16 121VU DLS&/DLRB/SPLY 5TD J15
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-38-22Page 401 1401-499, 1Aug 01/05 1 1 1CES 1

 4. Procedure
_________
 (Ref. Fig. 401/TASK 31-38-22-991-001) Subtask 31-38-22-020-050
 A. Removal of the MDDU
 (1)
 Looseen the four quarter-turn fasterners (3).

 (2)
 Pull the MDDU (1) from its housing.

 (3)
 Disconnect the electrical connectors (2).

 (4)
 Remove the MDDU (1).

 (5)
 Put blanking caps on the disconnected electrical connectors.

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-38-22Page 402 1401-499, 1Aug 01/05 1 1 1CES 1

 Multipurpose Disk Drive Unit (1TD)
 Figure 401/TASK 31-38-22-991-001

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-38-22Page 403 1401-499, 1Aug 01/05 1 1 1CES 1

 TASK 31-38-22-400-001 Installation of the MDDU (1TD)
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-38-22-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 31-38-22-860-050
 A. Make sure that the aircraft electrical circuits from the external power is de-energized (Ref. TASK 24-41-00-862-002).
 Subtask 31-38-22-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU DATA/LOADER/SPLY 3TD J16 121VU DLS&/DLRB/SPLY 5TD J15
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-38-22Page 404 1401-499, 1Aug 01/05 1 1 1CES 1

 4. Procedure
_________ (Ref. Fig. 401/TASK 31-38-22-991-001) Subtask 31-38-22-420-050
 A. Installation of the data loading selector
 (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 the blanking caps from the electrical connectors.
　
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 指示/记录系统 5(138)