-
The AIDS page comes into view.
-
The AIDS MAN REQST REPRT page comes into view.
On the center pedestal:
-
The printer makes a printout of the related report.
On the MCDU display:
-
The MCDU MENU page comes into view.
R 1EFF : 151-199, 201-210, 1 31-36-00Page 271 1 1 May 01/05 1 1 1CES 1
Example for Print Out of Manually Requested Reports R Figure 202B/TASK 31-36-00-991-005-A
R 1EFF : 151-199, 201-210, 1 31-36-00Page 272 1 1 May 01/05 1 1 1CES 1 **ON A/C ALL
5. Close-up
________ Subtask 31-36-00-860-081
A. Put the system back to the serviceable condition.
(1)
De-energize the CFDS.
(2)
De-energize the aircraft electrical circuits
R 1EFF : ALL 1 31-36-00Page 273 1 1 May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 201-202,
TASK 31-36-00-710-004
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 1TV1, 1TV2
No specific Adapter Cable
No specific PDL
No specific access platform 1.6 m (5 ft. 3 in.)
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 31-36-00-710-001 Test of the DMU (1TV) 31-36-00-740-006 Printout of the APU Hours and Cycles 31-36-00-740-007 Printout of the Engine Hours and Cycles 52-41-00-010-002 Open the Avionics Compartment Doors for Access 52-41-00-410-002 Close the Avionics Compartment Doors after Access
R 1EFF : 001-049, 051-099, 101-105, 201-202, 1 31-36-00Page 274 1 1 May 01/05 1 1 1CES 1
3. Job Set-up
__________ R **ON A/C 001-049, 051-099, 101-105,
Subtask 31-36-00-010-060
A. Get Access
(1) Put the access platform in position at the access door 824 in zone
128.
(2) Open the access door 824. (Ref. TASK 52-41-00-010-002) R **ON A/C 001-049, 101-105,
Subtask 31-36-00-860-050
B. 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 31-36-00-740-007) (Ref. TASK 31-36-00-740-006).
NOTE : This prevents the loss of engine and APU hours and cycles.
____
(3) Make sure that the OPERATING/STORAGE switch of the DMU is in OPERATING position.
NOTE : This enable the battery backup buffering of all internal DMU
____ data stored in the volatile memory in case of external power shut-down.
(4)
On the front panel of the DMU open the left flap to get access to the DMU front connector.
(5)
On the Portable Data Loader (PDL) make sure that the ON/OFF switch is in the OFF position.
(6)
Connect the Adapter Cable to the DMU front connector.
(7)
Connect the Adapter Cable to the PDL interface.
(8)
Make sure all software disks 1TV1, 1TV2 are not write-protected.
R 1EFF : 001-049, 051-099, 101-105, 201-202, 1 31-36-00Page 275 1 1 May 01/05 1 1 1CES 1
R **ON A/C 051-099,
R Subtask 31-36-00-860-050-A
R B. Aircraft Maintenance Configuration
R (1) Energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-861-002)
R (2) Do a print out of the engine and APU hours and cycles (Ref. TASK 31-
R 36-00-740-007) (Ref. TASK 31-36-00-740-006).
R NOTE : This prevents the loss of engine and APU hours and cycles.____
R (3) On the front panel of the DMU open the left flap to get access to the
R DMU front connector.
R (4) Make sure that the ON/OFF switch is in the ON position.
R NOTE : This enables the battery backup buffering of all internal DMU____
R data stored in the volatile memory in case of external power
R shut-down.
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