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时间:2011-03-25 12:19来源:蓝天飞行翻译 作者:admin
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 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/GPWS/115VAC 3WZ P07
 4. Procedure
_________ Subtask 31-50-00-710-083
 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.
R 1EFF : 001-049, 101-101, 1 31-50-00Page 531 1 1 Aug 01/05 1 1 1CES 1 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).


 Subtask 31-50-00-710-079
 B. Automatic Test of the Announcements NOTE : This test is for RA1. For RA2, you must open the circuit breaker
____
 1SA1.

 NOTE : During the test, you can hear only the call-out in the ramp test
____
 range.

 NOTE : The 500ft call-out is not triggered, even if it is activated,
____
 because the ramp test begins at 500ft.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:  On the MCDU:
 - push the line key adjacent to the RA1 (RA2) indication. - The RA1 (RA2) page comes into view.
 On the MCDU:  On the MCDU:
 - push the line key adjacent to the RAMP TEST indication.  - the RA1 (RA2) RAMP TEST page comesinto view with these indications:
 TWO SUCCESSIVE RAMPS:
 RAMP1: 500-50FT (10FT/S) RAMP2: 50/0FT (3FT/S) MAKE SURE THAT AUTO CALL-OUT
 ALTITUDES ARE CORRECTLY ANNOUNCED.
 On the CAPT (F/O) PFD: - the ramp test starts. The speed scale moves down from 500 to 0 ft. and
 stops after approximately 1 minute. - during the descent, make sure that you can hear the programmed 

R 1EFF : 001-049, 101-101, 1 31-50-00Page 532 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------ACTION RESULT
 -------------------------------------------------------------------------------announcements in the CAPT and F/O loudspeakers.
 On the MCDU:
 -at the end of the test, the TEST OK indication comes into view.
 -push the line key adjacent to  - the MCDU shows the CFDS menu page. the RETURN indication until the CFDS menu page comes into view.
 NOTE : If all the call-outs in the ramp test range are heard, the
____
 call-out operational test is successful.

 5. Close-up
________ Subtask 31-50-00-865-076
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3WZ
 Subtask 31-50-00-860-092
 B. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002)

 (2)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005)

 (3)
 On the MCDU, set the BRT knob to off.

 (4)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002)


 (5)
 Make sure that the work area is clean and clear of tool(s) and other items.


R 1EFF : 001-049, 101-101, 1 31-50-00Page 533 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 TASK 31-50-00-740-002 Read SDAC and FWC Hardware Pin Programming WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 NOTE : IGNORE ALL THE ECAM WARNINGS AS LONG AS THE COMPUTER IS IN THE MENU
____ MODE.
 1.
 Reason for the Job

__________________
 Make sure that the pin programming and parity of SDAC and FWC 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 31-32-00-860-008 Procedure to Get Access to the SYSTEM REPORT/TEST/INST Page
 
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