R  Subtask 32-31-00-010-082  
R  B. Get Access  
R  (1) Open the MLG doors (Ref. TASK 32-12-00-010-001).  
R  (2) Open the NLG doors (Ref. TASK 32-22-00-010-001).  
R  (3) Make sure that the ground safety locks are installed on the landing  
R  gear and the landing gear doors (Ref. TASK 32-00-00-481-001) and  
R  (Ref. TASK 32-00-00-481-002).  
R  Subtask 32-31-00-869-115  
R  C. Flight Configuration Precautions  
R  (1) Do the flight configuration precautions (Ref. TASK 32-00-00-860-001).  
R  Subtask 32-31-00-865-118  
R  D. Make sure that this(these) circuit breaker(s) is(are) closed:  
R  ------------------------------------------------------------------------------- 
R  PANEL DESIGNATION IDENT. LOCATION  
R  ------------------------------------------------------------------------------- 
R  49VU L/G/LGCIU/SYS1/NORM 1GA C09  
R  121VU HYDRAULIC/LGCIU/SYS2 2GA Q35  
R  121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34  
R  Subtask 32-31-00-860-109  
R  E. Aircraft Maintenance Configuration  
R  (1) Install the brace tool on the applicable MLG lockstay actuating  
R  cylinder (Ref. TASK 32-00-00-480-001).  
R  (2) Install a FALSE TARGET (98F32304000000) on:  
R  (a) The NLG extension proximity sensors 24GA and 25GA.  
R  (b) The MLG extension proximity sensors:  
R  - for the LH MLG 21GA and 23GA  
R  - for the RH MLG 20GA and 22GA.
R (3) Pressurize the Green hydraulic system using: 
R - a ground hydraulic supply (Ref. TASK 29-10-00-863-001) 
R or 
R - the Yellow hydraulic system (through the PTU) (Ref. TASK 29-24-00-R 863-001).
R (4) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-R 002).
R (5) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) 
R (Ref. TASK 31-60-00-860-001).
R Subtask 32-31-00-081-055
R F. Removal of the Safety Devices
R (1) Remove the GROUND LOCK SLEEVE or the GROUNDLOCK SLEEVE from the 
R applicable MLG lockstay actuator.
R 4. Procedure
_________ R Subtask 32-31-00-720-075 R A. Functional Test of the MLG Lockstay Actuating Cylinder with Brace Tool 
R Installed R (1) Do this test: R -------------------------------------------------------------------------------
R ACTION RESULT R -------------------------------------------------------------------------------
R 1. On the panel 400VU: 
R - move the landing-gear 
R control-lever 6GA to the UP 
R position.
R 2. On the panel 400VU: 
R - move the landing-gear 
R control-lever 6GA to the DOWN 
R position.
R 3. Do the test procedure three 
R times. This is to make sure that 
R the actuator movement is the same 
R each time.
On the aircraft: 
-
monitor the movement of the actuator as it retracts, the movement must be free and smooth.
On the aircraft:
-
monitor the movement of the actuator as it extends, the movement must be free and smooth.
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R  5. Close-up________  
R  Subtask 32-31-00-860-110  
R  A. Aircraft Maintenance Configuration  
R  (1) Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).  
 
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