(2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 32-31-00Page A510 1 1 May 01/05R 1 1 1CES 1

 TASK 32-31-00-720-005
 Functional Test of the MLG Safety Valve Solenoid
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 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. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific multimeter No specific safety barriers No specific the electrical cables. No specific the resistor 5.6 ohm +/- 1% correct to output, 0.25
 watt or more No specific the voltmeter +/- 1% correct to output No specific the 1.5 VDC power supply +/- 1% correct to output No specific warning notice 460005835 1 GROUND LOCK SLEEVE
 1EFF : ALL 1 32-31-00Page A511 1 1 May 01/05R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical Power 32-00-00-860-002 Ground Configuration after Flight Configuration with
 Electrical Power
 32-12-00-010-001 Open the Main Gear Doors for Access
 32-12-00-410-001 Close the Main Gear Doors after Access

R 32-31-00-991-016 Fig. 509
 3. Job Set-up
__________
 Subtask 32-31-00-941-082
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 On panel 400VU:

 -make sure that the landing-gear control-lever 6GA is in the DOWN position.
 -put a warning notice in position to tell persons not to operate the landing gear system.

 (4)
 Put a warning notice on the flap/slat control lever to tell persons not to operate the flap/slat system.

 Subtask 32-31-00-010-074
 B. Get Access
 (1)
 Open the MLG doors (Ref. TASK 32-12-00-010-001).

 (2)
 Install the GROUND LOCK SLEEVE (460005835) on the MLG doors.

 1EFF : ALL 1 32-31-00Page A512 1 1 May 01/05 1 1 1CES 1 Subtask 32-31-00-860-087

 C. Aircraft Maintenance Configuration
 (1) Make sure that the green hydraulic system is depressurized.
 Subtask 32-31-00-869-106
 D. Flight Configuration Precautions
 (1)
 If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.

 (2)
 If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.

 Subtask 32-31-00-865-094
 E. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
 4. Procedure
_________
R (Ref. Fig. 509/TASK 32-31-00-991-016)
 Subtask 32-31-00-720-066
 A. Functional Test of the MLG Safety Valve Solenoid
 (1)
 Disconnect the electrical connector from the MLG safety valve solenoid.

 (2)
 Assemble the test equipment that follows, as shown in the circuit diagram:

 -
the 1.5 VDC power supply +/- 1% correct to output
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架4(89)