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NOTE : If the upper ECAM DU shows a
____ warning, push the CLR key on the ECAM control panel until the MEMO page comes into view on the upper ECAM DU.
On the MEMO page of the upper ECAM DU,the N. WHEEL STEERING DISC indicationgoes out of view.
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2EN1, 2EN2. ________
5. Close-up
 Subtask 32-51-00-860-057
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

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 TASK 32-51-00-720-006 Functional Test of the Rudder Bar. WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  circuit breaker(s) safety clip(s)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 Material No. 04-022  USA MIL-PRF-81322 GRADE 2 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
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 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-586-001 Lowering of the Aircraft at Forward Jacking Point,
 MLG Wheels on the Ground 07-12-00-582-001 Jacking for Nose Gear Wheel Change 09-10-00-584-002 Towing with the Nose Gear from the Front 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 29-10-00-863-001 Pressurize the Green Hydraulic System R 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System
R  29-10-00-864-002 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 32-51-00-720-004 Functional Test of the Nose Wheel Steering with the
 Pedals.
 3. Job Set-up
__________
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 32-51-00-860-058
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Pressurize the Green hydraulic system (Ref. TASK 29-10-00-863-001).

 (3)
 If the test is to be done with the nose wheels on the ground, do these steps:

 NOTE : You will need two 1.2 m (3.93 ft.) square steel plates.
____
 (a)
 Position a steel plate in front of the nose wheels.

 (b)
 Apply a thick layer of COMMON GREASE (Material No. 04-004) or COMMON GREASE (Material No. 04-022) to the upper surface of the steel plate.

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 NOTE : Do not mix Material No. 04-004 with Material No. 04-022.____ You can use Material No. 04-022 as an alternative to Material No. 04-004. Clean and degrease the parts before you use Material No. 04-022.
 (c) Put the other steel plate on the top of the greased steel plate.
 (d) Move the aircraft and position the nosewheels on the greased steel plates (Ref. TASK 09-10-00-584-002).
 (4) If the test is to be done with the nose wheels clear of the ground do this:
 (a) Lift the nose gear (Ref. TASK 07-12-00-582-001).
　
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