(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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