(2)
Disconnect the Adapter Cable from the DMU.
(3)
Disconnect the Adapter Cable from the PDL.
R 1EFF : 001-049, 051-099, 101-105, 201-202, 1 31-36-00Page 279 1 1 May 01/05 1 1 1CES 1 Subtask 31-36-00-410-059
B. 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 **ON A/C 001-049, 051-099, 101-105, 201-202,
Subtask 31-36-00-710-064
C. Do the test of the DMU (Ref. TASK 31-36-00-710-001).
R 1EFF : 001-049, 051-099, 101-105, 201-202, 1 31-36-00Page 280 1 1 May 01/05 1 1 1CES 1R **ON A/C 106-149, 211-299, 301-399, 401-499,
TASK 31-36-00-710-013
FDIMU (10TV) AIDS Software Load Procedure
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific software disks 10TV SW2 / 10TV MD2
No specific software disks 10TV2
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 31-36-00-740-012 Test of the FDIMU (10TV) 31-36-00-740-015 Printout of the Engine / APU Hours and Cycles Stored
in the FDIMU (10TV)
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 281 1 1 Aug 01/05 1 1 1CES 1
3. Job Set-up
__________ R **ON A/C 106-149, 229-299, 303-399, 401-499,
Subtask 31-36-00-860-082-B
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
(2)
Do a print out of the engine and APU hours and cycles (Ref. TASK 31-36-00-740-015).
NOTE : This prevents the loss of the engine and APU hours and cycles.
____
(3)
Make sure that the aircraft is in ground configuration (Landing Gear compressed and all Engines stopped).
(4)
Make sure that the software disks 10TV SW2 / 10TV MD2 are in non-writeprotected status (writeprotection OFF).
**ON A/C 211-228, 301-302,
Subtask 31-36-00-860-082-A
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
(2)
Do a print out of the engine and APU hours and cycles (Ref. TASK 31-36-00-740-015).
NOTE : This prevents the loss of the engine and APU hours and cycles.
____
(3)
Make sure that the aircraft is in ground configuration (Landing Gear compressed and all Engines stopped).
(4)
Make sure that all software disks 10TV2 are in non-writeprotected status (writeprotection OFF).
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-36-00Page 282 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 106-149, 211-299, 301-399, 401-499,
Subtask 31-36-00-865-087
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU CFDS/CFDIU/SPLY 2TW J18 121VU CFDS/CFDIU/BACK/UP 8TW J17 121VU DATA/LOADER/SPLY 3TD J16 121VU DLS&/DLRB/SPLY 5TD J15 121VU AIDS & RCDR/FDIMU 5TV K15 121VU ENGINE/ENG1 AND 2/EVMU 1EV R44
4. Procedure
_________
R **ON A/C 106-149, 229-299, 303-399, 401-499,
Subtask 31-36-00-710-078-B
A. System Software Load Procedure
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the overhead panel, on the Data On the Data Loading Selector display: Loading Selector:
-Put the data loading selector - The DB/N:XXXXXXXX and PUSH NEXT/PREV ON/OFF switch to the ON position. indications show.
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