(2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 Energize the CFDS (Ref. TASK 31-32-00-860-008).

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 Subtask 31-33-00-865-061
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU COM/CVR/CTL 4RK E13
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
 121VU FDIU & QAR 8TU K17 **ON A/C ALL
 121VU RCDR/ACCLRM  9TU K18
 121VU RCDR/DFDR  7TU K16

R **ON A/C 106-149, 211-299, 301-399, 401-499,
 121VU AIDS & RCDR/QAR  14TU K17
 121VU AIDS & RCDR/FDIMU  5TV K15
 **ON A/C ALL
 4. Procedure
_________
 Subtask 31-33-00-710-063

 A. Operational test of the DFDR
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the control panel 21VU: On the control panel 21VU:
 -press the GND/CTL button.  - the GND/CTL button integral light comes on
 2. On the panel 121VU:  On the ECAM display:
 1EFF : ALL 1 31-33-00Page 526 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------- open the circuit breaker DFDR - the message 'RECORDER DFDR FAULT' is 7TU (K16). shown.
 -close the circuit breaker DFDR  - the message 'RECORDER DFDR FAULT' 7TU (K16). goes off.
 3. On the control panel 21VU: On the control panel 21VU:
 -press the GND/CTL button.  - the GND/CTL button integral light goes off.
 5. Close-up
________ Subtask 31-33-00-862-055
 A. Put the aircraft back to its initial configuration.
 (1)
 De-energize the CFDS (Ref. TASK 31-32-00-860-008).

 (2)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 (3)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

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 INTENTIONALLY BLANK

R 1 1

31-33-00Page 528
1 1 Aug 01/05 1 1 1CES 1

 TASK 31-33-00-710-011 Functional Test of the Three-Axis-Accelerometer
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific digital multimeter
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
08-21-00-200-001 Quick Leveling Using the Attitude Monitor 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 31-55-34-000-001 Removal of the SDAC (1WV1,1WV2) 31-55-34-400-001 Installation of the SDAC (1WV1,1WV2)
 3. Job Set-up
__________ Subtask 31-33-00-861-060
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 Do the quick leveling procedure (Ref. TASK 08-21-00-200-001). NOTE : When the trim indicator shows the D4 position it is not

____ necessary to do the quick leveling procedure.
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 Subtask 31-33-00-020-051
 B. Remove the SDAC 1 (1WV1) (Ref. TASK 31-55-34-000-001). Subtask 31-33-00-865-070
 C. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ------------------------------------------------------- IDENT. LOCATION------------------
　
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