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时间:2011-03-25 12:16来源:蓝天飞行翻译 作者:admin
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R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-34Page 415 1 1 Config-1 Aug 01/05 1 1 1CES 1 Subtask 31-36-34-865-060


 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5TV
 Subtask 31-36-34-710-057
 C. Do the Loading of the FDIMU software
 (1) Load the DFDR software of the FDIMU (Ref. TASK 31-33-00-710-013)
 (2)
 Load the AIDS software of the FDIMU (Ref. TASK 31-36-00-710-013) Subtask 31-36-34-554-060

 D.
 Do the updating of APU hours and cycles data (Ref. TASK 31-36-00-740-013) and of Engine hours and cycles data (Ref. TASK 31-36-00-740-014) in the FDIMU


 Subtask 31-36-34-740-061
 E. Do the operational test of the FDIMU (Ref. TASK 31-36-00-740-012)
 5. Close-up
________ Subtask 31-36-34-410-053
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access door 824. (Ref. TASK 52-41-00-410-002)

 (3)
 Remove the access platform(s).


R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-34Page 416 1 1 Config-1 Aug 01/05 1 1 1CES 1


 RECORDER - DIGITAL AIDS (DAR) (2TV) - SERVICING
_______________________________________________ TASK 31-36-52-600-008 Replacement of the Disk with the DAR (2TV) Energized
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
 B. 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 52-41-00-410-002 Close the Avionics Compartment Doors after Access 31-36-52-991-005 Fig. 301
 3. Job Set-up
__________ Subtask 31-36-52-861-056
 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

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 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU RCDR/ACCLRM 9TU K18
 **ON A/C 151-199, 201-210,
 121VU AIDS/DMU 4TV K15 R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 31-36-52-010-059
 C. Get Access
 (1)
 Put the access platform in position at the access door 824.

 (2)
 Open the access door 824.


 4. Procedure
_________
 Subtask 31-36-52-020-058

 A. Removal of the Disk
 (Ref. Fig. 301/TASK 31-36-52-991-005)

 (1)
 On the DAR, make sure that:

 -
the POWER FAIL indication is not shown in the display (4).

 -
the FAULT WARNING light (1) is off.

 

 (2)
 Open the door (3) of the DAR.

 (3)
 Push the EJECT key (2).
 The EJECTING indication comes into view.


 (4)
 When the disk (5) is ejected, remove it from the disk drive.

 (5)
 Close the door (3) of the DAR.


R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-36-52Page 302 1401-499, 1Aug 01/05 1 1 1CES 1


 DAR Disk
 Figure 301/TASK 31-36-52-991-005

R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 31-36-52Page 303 1401-499, 1Aug 01/05 1 1 1CES 1 Subtask 31-36-52-420-058


 B. Installation of the Disk NOTE : If there is no disk in the disk drive, the INSERT DISK indication
____
 is shown in the display (4).

 (1)
 Open the door (3) of the DAR.

 (2)
 Put the disk (5) in the disk drive.

 (3)
 Push the disk fully in until it engages correctly in its chamber.

 (4)
 The DISK DETECTED indication comes into view in the display (4).

 (5)
 
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