-
the voltmeter +/- 1% correct to output
-
the resistor 5.6 ohm +/- 1% correct to output, 0.25 watt or more
-
the electrical cables.
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R Functional Test MLG Safety Valve Solenoid Figure 509/TASK 32-31-00-991-016
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(3)
Connect the 1.5 VDC power supply to the solenoid electrical connector as follows:
-
connect the positive (+) electrical cable to the connector pin B
-
connect the negative (-) electrical cable to the connector pin A.
(4)
Measure the voltage drop across the resistor, and use the multimeter to measure the resistance of the solenoid.
(5)
Make sure the measured values are between the limits given in Table
001.
---------------------------------------------------------------------
| CABLE | SUPPLY | VOLTAGE DROP | SOLENOID |
| POLARITY | VOLTAGE | ACROSS RESISTOR | RESISTANCE |
|--------------|--------------|-------------------|-------------------|
| A (-) B (+) | 1.5 V +/- 1% | 150 - 215 mV | 35 - 47 ohms |
|--------------|--------------|-------------------|-------------------|
| A (+) B (-) | 1.5 V +/- 1% | 600 mV - 1.0 V | 4 - 11 ohms |
---------------------------------------------------------------------Limits for the Measured Values Table 001
(6)
Disconnect the electrical cables from the electrical connector on the solenoid.
(7)
Connect the 1.5 VDC power supply to the solenoid electrical connector as follows:
-
connect the positive (+) electrical cable to the connector pin A
-
connect the negative (-) electrical cable to the connector pin B.
(8)
Measure the voltage drop across the resistor, and use the multimeter to measure the resistance of the solenoid.
(9)
Make sure the measured values are between the limits given in Table
001.
5. Close-up________
Subtask 32-31-00-860-088
A. Aircraft Maintenance Configuration
(1)
Disconnect and remove the electrical cables from the MLG safety valve solenoid.
(2)
Connect the electrical connector to the MLG safety valve solenoid.
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Subtask 32-31-00-869-105
B. Ground Configuration
(1) If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
Subtask 32-31-00-865-095
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 52GA, 2GA
Subtask 32-31-00-410-068
D. Close Access
(1) Close the MLG doors (Ref. TASK 32-12-00-410-001). Subtask 32-31-00-942-085
E. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 32-31-00-820-003
Adjustment of the MLG Uplock
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.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
1. Reason for the Job
__________________
If applicable, this task is completed during task 323100 820 004.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
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本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架4(90)
