-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the MCDU, push the line key adjacent to the BSCU 1(2) indication.
2.
Push the line key adjacent to the LAST LEG REPORT indication.
The BSCU CHAN 1(2) page comes intoview.
The BSCU CHAN 1(2)/LAST LEG REPORT pagecomes into view.
-
If you have a fault messages related to an alternate pressure transducer, make sure that none of these messages is shown: ABCU (95GG) BRK ALTN SELECTOR VALVE (99GG) ABCU/BRK NORM SEL VALVE PRESS XDCR (96GG) ABCU/BRK ALTN SERVOVALVE (97GG) OR (98GG).
-
If you have neither a transducer fault message nor a servovalve fault message, make sure that none of these messages is shown: ABCU (95GG) BRK ALTN SELECTOR VALVE (99GG) ABCU/BRK NORM SEL VALVE PRESS XDCR (96GG) ABCU/BRK ALTN SERVOVALVE (97GG) OR (98GG) BRK ALTN PRESS TRANSDUCER (101GG) or (100GG)
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5. Close-up
________ Subtask 32-46-00-860-068
A. Put the aircraft back to its initial configuration.
(1)
On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002)
(3)
Remove the warning notice(s).
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BRAKES AND STEERING - BITE - ADJUSTMENT/TEST
____________________________________________
TASK 32-46-00-740-001
BITE Test of the BSCU
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
B. 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 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G
Page
R 31-60-00-860-001 EIS Start Procedure
R 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-004 IR Alignment Procedure 34-10-00-860-005 ADIRS Stop Procedure
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3. Job Set-up
__________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 301-399,
Subtask 32-46-00-860-052
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
On the panel 400VU, make sure that the Landing Gear control-lever is set to DOWN.
(3)
On the panel 402VU, make sure that the A/SKID & N/W STRG switch is at ON.
(4)
Do the IR alignment procedure. (Ref. TASK 34-10-00-860-004)
(5)
On one MCDU, get the SYSTEM REPORT/TEST/L/G Page (Ref. TASK 31-32-00-860-009).
R **ON A/C 106-149, 221-299, 401-499,
Subtask 32-46-00-860-052-A
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
On the panel 400VU, make sure that the Landing Gear control-lever is set to DOWN.
(3)
On the panel 402VU, make sure that the A/SKID & N/W STRG switch is at ON.
(4)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(5)
Do the IR alignment procedure. (Ref. TASK 34-10-00-860-004)
(6)
On one MCDU, get the SYSTEM REPORT/TEST/L/G Page (Ref. TASK 31-32-00-860-009).
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Subtask 32-46-00-941-054
B. Safety Precautions
(1) On the panel 400VU, put a warning notice on the Landing Gear control-lever to tell persons not to move it.
Subtask 32-46-00-865-050
C. Make sure that this(these) circuit breaker(s) is(are) closed:
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本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架8(17)
