-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the overhead panel 23VU (24VU), push the FLT CTL/ELAC1 (FLT CTL/ELAC2) pushbutton switch 6CE1 (6CE2).

2.
 Push the left or right pedal fully and keep it in this position

3.
 Push the pedal disconnection pushbutton switch on the CAPT or F/O handwheel

4.
 Release the pedal disconnection pushbutton switch on the CAPT or F/O handwheel

 5.
 Release the pedals

- on the pushbutton switch 6CE1 (6CE2),the OFF legend goes off, the FAULTlegend comes on and goes off aftersome seconds.
-do a check of the steering of thenose wheels (Ref. TASK 32-51-00-720-004).
-make sure that the nose wheels go tothe zero position: the pointer on thenose gear is aligned with the index.
-
the wheels move to their angle ofturn.

-
the wheels move to the zero position: the pointer on the nose gear is aligned with the fixed index.

 1EFF : ALL 1 32-51-00Page 536 1 1 Aug 01/05R 1 1 1CES 1

 Subtask 32-51-00-865-069
 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 32-51-00-860-059
 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) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 (5) If the front of the aircraft is lifted off the ground, lower the aircraft to the ground (Ref. TASK 07-11-00-586-001).
 (6) If the nosewheels are on grease plates, move the aircraft to remove the grease plates (Ref. TASK 09-10-00-584-002).
 (7) Make sure that the work area is clean and clear of tool(s) and other items. 
R  **ON A/C 401-499, 
R  Subtask 32-51-00-860-059-A 
R  A. Put the aircraft back to its initial configuration. 
R R  (1) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002). 
R  (2) Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-001).

 1EFF : ALL 1 32-51-00Page 537 1 1 Aug 01/05 1 1 1CES 1

R  (3) Do the EIS stop procedure 
R  (Ref. TASK 31-60-00-860-002). 
R  (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R  002). 
R  (5) 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  (6) If the nosewheels are on grease plates, move the aircraft to remove 
R  the grease plates (Ref. TASK 09-10-00-584-002). 
R  (7) 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 538 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL

 TASK 32-51-00-710-002 Integrity Test of the Nose Wheel Steering System 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

__________________
 To ensure aircraft safety after maintenance work on the wiring

 2.
 Job Set-up Information

______________________
 A. 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)

 1EFF : ALL 1 32-51-00Page 539 1 1 Aug 01/05 1 1 1CES 1 B. Referenced Information
　
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