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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