(5)
 Close the access door 822.

 (6)
 Remove the access platform.

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R **ON A/C 001-004, 051-099, 102-149, 151-199, 201-299, 301-399, 401-499,

 TASK 31-50-00-710-006 Operational Test of the Automatic Call-Out WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1. Reason for the Job__________________
 To make sure that the operation and the inhibition of the announcements are
 correct.
 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
 31-32-00-860-010  Procedure to Get Access to the SYSTEM REPORT/TEST NAV
 Page 31-50-00-740-002 Read SDAC and FWC Hardware Pin Programming 31-60-00-860-001 EIS Start Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure ASM 31-52/01
 3. Job Set-up
__________ Subtask 31-50-00-860-060
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)

 (2)
 Do the EIS start procedure (PFDs only) (Ref. TASK 31-60-00-860-001).

 (3)
 Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).

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 (4)
 On the panel 21VU, push the GPWS/SYS pushbutton switch (OFF legend on).

 (5)
 On one MCDU, get the SYSTEM REPORT/TEST NAV menu page (Ref. TASK 31-32-00-860-010).

 Subtask 31-50-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU COM NAV/RAD ALTM/2 1SA2 K12 121VU COM NAV/RAD ALTM/1 1SA1 K11
 4. Procedure
_________ Subtask 31-50-00-710-085
 A. Check of the Automatic Call-Out Announcements Pin-Programmed in the FWCs NOTE : The Aircraft Schematic Manual (ASM) gives the auto call-out
____ announcements pin-programmed in the FWCs (Ref. ASM 31-52/01). You can hear these announcements during A/C operation if their related pins are connected to the ground.
 NOTE : You can do this procedure with the FWC1 or the FWC2.
____ This procedure is for the FWC1. For the FWC2, use the indications between the parentheses.
 (1)
 Read the pin programming related to the FWC1 (2) (Ref. TASK 31-50-00-740-002).

 (2)
 Compare the pin programming related to the FWC1 (2) with the state of the aircraft pin programming given in the ASM (Ref. ASM 31-52/01).

R 1EFF : 001-004, 051-099, 102-149, 151-199, 1 31-50-00Page 526 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 31-50-00-710-075

 B. Operational Test
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal, on the
 MCDU, on the NAV menu page:
 - push the line key adjacent to  - on the MCDU:
 the RA1 indication. Then push
 the line key adjacent to the  *the LRRA1 RAMP TEST page comes into
 RAMP TEST indication.  view.
 - for each value, enter the  - on the MCDU, these values come into
 number in the scratchpad and  view:
 push the related line key:  * +3100ft.
 * +0ft.
 * START ALT : 3100ft.  * 10ft/s.
 * STOP ALT : 0ft.
 * SLOPE : 10ft/s.
 - push the line key adjacent to  - on the CAPT PFD, the ramp test
 the TRIGGER indication.  starts. The altitude scale moves down
 from 3100 ft. to 0 ft. and stops
 after approximately 5 minutes.
 - on the MCDU, the RAMP TEST PROCESSING
 indication comes into view.
 - during the descent, make sure that
 you can hear the programmed
 announcements in the CAPT and F/O
 loudspeakers.
 2. On the MCDU:
　
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