2.
If there are warnings, on the MCDU push the line key adjacent to the BSCU 1 indication.
3.
Push the line key adjacent to the GND SCAN indication.
4.
Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST L/G page.
5.
Push the line key adjacent to the BSCU 2 indication.
6.
Do the same action as in Para. 4..
-
if the steering is correct (movementof the wheels = 6 deg) there is no warning
-
if the steering is not correct: .the WHEEL N/W STRG FAULT indication comes into view on the upper ECAM DU. .the NW STEER indication comes into view on the lower ECAM DU.
-the BSCU SYS 1 page comes into view.
-The BSCU SYS1 GROUND SCANNING pagecomes into view and shows the fault message that relates to the defective equipment (LRU).
-
the SYSTEM REPORT/TEST L/G page comesinto view.
-
the BSCU SYS 2 page comes into view.
-same results as for the BSCU SYS 1.
R 1EFF : 001-049, 062-099, 101-105, 151-156, 1 32-51-00Page 524 1201-220, 301-399, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 32-51-00-865-063
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2EN1, 2EN2.
5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 32-51-00-860-055
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
(2)
Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-001).
(3)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(4)
On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(6)
If the front of the aircraft is lifted off the ground, lower the aircraft to the ground (Ref. TASK 07-11-00-586-001).
(7)
If the nosewheels are on grease plates, move the aircraft to remove the grease plates (Ref. TASK 09-10-00-584-002).
(8)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 32-51-00Page 525 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 401-499,
R Subtask 32-51-00-860-055-A
R A. Put the aircraft back to its initial configuration.
R (1) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-
R 002).
R (2) Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-001).
R (3) Do the EIS stop procedure
R (Ref. TASK 31-60-00-860-002).
R (4) On the MCDU, push the line key adjacent to the RETURN indication
R until the CFDS menu page comes into view.
R (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R 002).
R (6) If the front of the aircraft is lifted off the ground, lower the
R aircraft to the ground (Ref. TASK 07-11-00-586-001).
R (7) If the nosewheels are on grease plates, move the aircraft to remove
R the grease plates (Ref. TASK 09-10-00-584-002).
R (8) Make sure that the work area is clean and clear of tool(s) and other
R items.
R 1EFF : 401-499, 1 32-51-00Page 526 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
TASK 32-51-00-720-005 Functional Test of the Nose Wheel Steering Deactivation Electrical-Box WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1.
Reason for the Job
__________________
Self Explanatory
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
3. Job Set-up
__________
Subtask 32-51-00-860-056
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
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