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时间:2011-03-25 12:26来源:蓝天飞行翻译 作者:admin
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R  **ON A/C 106-149, 303-399, 401-499,
 49VU EIS/PFD/CAPT/SPLY  11WT1  E03
 **ON A/C ALL
 121VU EIS/DMC3/SPLY 121VU EIS/DMC2/SPLY 121VU EIS/ECAM DU/LOWER/SPLY 121VU EIS/ECAM DU/LOWER/SWTG 121VU EIS/DMC2/SWTG 121VU EIS/ND/F/O/SWTG 121VU EIS/PFD/F/O/SWTG 121VU EIS/ND/F/O 121VU EIS/PFD/F/O  10WT3 10WT2 13WT2 24WT2 21WT2 23WT2 22WT2 12WT2 11WT2  Q09Q08R11R10R08R06R05R04R03

 1EFF : ALL 1 31-60-00Page 502 1 1 Aug 01/05 1 1 1CES 1


 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 31-60-00-710-050
 A. Test NOTE : This test is for the CAPT side. For the F/O side, use the
____
 indications between parentheses.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the center pedestal, on the  - make sure that there is no change on SWITCHING panel 8VU, set the EIS the PFD, the ND on the CAPT (F/O) DMC selector switch to CAPT/3 side and the upper (lower) ECAM DU. (F/O/3).

 2.
 Set the EIS DMC selector switch
 to NORM.

 


R  **ON A/C 401-499,
 Subtask 31-60-00-710-050-A
 A. Test NOTE : This test is for the CAPT side. For the F/O side, use the
____
 indications between parentheses.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 301VU (500VU):
-set the PFD potentiometer to the center position
2. On the panel 301VU (500VU):
-set the ND potentiometer to the center position
-
After some seconds the PFD comes intoview:SELF TEST IN PROGRESS (MAX 40 SECONDS)

-
After some seconds the ND comes into
view:
SELF TEST IN PROGRESS (MAX 40 SECONDS)

 

 1EFF : ALL 1 31-60-00Page 503 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
R R R R  ACTION RESULT -------------------------------------------------------------------------------3. On the ECAM control panel: - After some seconds the EWD comes into - set the UPPER display view: potentiometer to the center SELF TEST IN PROGRESS (MAX 40 SECONDS) position 
R R R R  4. On the ECAM control panel: - Set the LOWER display potentiometer to the center position  - After some seconds the SD comes into view. SELF TEST IN PROGRESS (MAX 40 SECONDS) 
R  **ON A/C ALL
 5. Close-up________
 Subtask 31-60-00-860-055
 A. 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) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 (4) Make sure that the work area is clean and clear of tool(s) and other items.

 1EFF : ALL 1 31-60-00Page 504 1 1 Feb 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,

 

 TASK 31-60-00-710-002
 Operational Test of EFIS/ECAM Switching Functions
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.

 1. Reason for the Job
__________________
 Refer to the MPD TASK: 316000-01
 To make sure that these functions are correct :
 -Automatic PFD/ND Transfer
 -
Manual PFD/ND Transfer

 -
Manual ECAM/ND Transfer

 -
Manual DMC1 and DMC2 to DMC3 switching


 -Automatic Upper DU/Lower DU Transfer.
 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
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 31-60-00Page 505 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1


 3. Job Set-up__________
 Subtask 31-60-00-860-056
 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
 
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