3.
On the MCDU:
-
push the line key adjacent to the EIS3 indication.
-
push the line key adjacent to the TEST indication
-
push the line key adjacent to the I/P TEST indication.
-Push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view.
4. On the panel 8VU, set the EIS DMC selector switch to NORM.
-
the I/P TEST IN PROGRESS indicationcomes into view; then the I/P TEST RESULTS and the NO BUS FAULT (or TCAS warning message if TCAS is not installed) indications come into view.
-
the CAPT (F/O) PFD and ND and theupper (lower) ECAM DU go back to thenormal mode.
-make sure that:
* the CAPT PFD and ND and the upperECAM DU operate in the maintenance mode (MAINTENANCE MODE comes into view on these 3 display units) * on the MCDU, the EIS DMC3 page comes into view.
- on the MCDU, the EIS DMC3 TEST pagecomes into view.
-
the I/P TEST IN PROGRESS indicationcomes into view; then the I/P TEST RESULTS and the NO BUS FAULT (or TCAS warning message if TCAS is not installed) indications come into view.
-
the CAPT PFD and ND and the upperECAM DU go back to the normal mode.
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5. Close-up
________ Subtask 31-60-00-860-060
A. Put the aircraft back to its initial configuration.
(1)
Do the EIS Stop Procedure (Ref. TASK 31-60-00-860-002)
(2)
On the maintenance panel 50VU, press the ENG/FADEC GND PWR 1 & 2 pushbutton switches (the ON legend goes off).
(3)
Do the ADIRS Stop Procedure (Ref. TASK 34-10-00-860-005).
(4)
On the radar control unit, set the control switches back to their initial position.
(5)
On the ATC control unit, set the control switches back to their initial position.
(6)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002)
(7)
Make sure that the work area is clean and clear of tool(s) and other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 31-60-00Page 533 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
TASK 31-60-00-740-004 EIS System Test WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
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
31-32-00-860-008 Procedure to Get Access to the SYSTEM
REPORT/TEST/INST Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
3. Job Set-up
__________ Subtask 31-60-00-860-062
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
(2)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001)
(3)
On one MCDU, get the SYSTEM REPORT/TEST INST menu page (Ref. TASK 31-32-00-860-008)
1EFF : ALL 1 31-60-00Page 534 1 1 Aug 01/05R 1 1 1CES 1
4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 31-60-00-740-051
A. DMC1 or DMC2 Test
NOTE : This test is for the DMC1. For the DMC2 use the indications
____
between parentheses.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU: On the MCDU:
2. Push the line key adjacent to the EIS1 (2) indication. - the EIS DMC1 (2) page comes intoview. On the EFIS/ECAM display units: - make sure that the CAPT (F/O) PFD and ND and the upper (lower) ECAM DU operate in the maintenance mode (MAINTENANCE MODE comes into view on these three display units).
3. Push the line key adjacent to the TEST indication. On the MCDU:- the EIS DMC1 (2) TEST page comes into view.
4. Push the line key adjacent to the SYSTEM TEST indication. - the EIS DMC1 (2) SYSTEM TEST pagecomes into view.
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