(4) For System 2 (25GA), if the dimension X1 was adjusted:
(a) Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the mating faces of:
-the sensor mounting bracket (38)
1EFF : ALL 1 32-31-73Page 598 1 1 May 01/04R 1 1 1CES 1
-the bracket (50).
NOTE : If the shim is to be installed, make sure that it is
____ installed in the correct position.
(b)
If applicable, apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-001) to both sides of the shim (35).
(c)
If applicable, put the shim (35) in position on the bracket (50).
(d)
Align the sensor mounting bracket (38) with the shim (35) if installed, and install with the bolts (49), the washers (36) and the nuts (37).
(e)
TORQUE the nuts (37) to between 0.25 and 0.35 m.daN (22.12 and
30.97 lbf.in).
(f)
Install the target (42) with the bolts (43), the washers (44) and the nuts (45).
(g)
TORQUE the nuts (45) to between 0.25 and 0.35 m.daN (22.12 and
30.97 lbf.in).
(h)
Remove the blanking caps from the applicable electrical connectors.
(i)
Connect the electrical connector (47) to the proximity sensor (40).
(j)
Apply a layer of SEALANTS (Material No. 09-001) to the bolts (43) and (49), the washers (36) and (44) and the nuts (37) and (45).
Subtask 32-31-73-865-080
F. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------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
1EFF : ALL 1 32-31-73Page 599 1 1 May 01/04R 1 1 1CES 1
Subtask 32-31-73-740-060
G. Test
(1)
Do a BITE test of the landing gear (Ref. TASK 32-69-00-740-001). Subtask 32-31-73-582-062
H. Lower the Aircraft
(1)
Lower the aircraft off jacks (Ref. TASK 07-11-00-586-001). Subtask 32-31-73-860-066
J. Aircraft Maintenance Configuration
(1)
If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
(2)
Connect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-002).
5. Close-up
________ Subtask 32-31-73-410-061
A. Close Access
(1) Remove the SAFETY PIN - NLG DOOR from each of the NLG doors.
(2) Close the NLG doors (Ref. TASK 32-22-00-410-001). Subtask 32-31-73-942-062
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-31-73Page A500 1 1 May 01/04R 1 1 1CES 1
TASK 32-31-73-820-008
Inductance Check of the Proximity Sensors/Switches
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
__________________
To check the condition of the proximity sensors and switches.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific non-metallic rod
No specific safety barriers
No specific warning notice
R No specific 1 KHz inductance meter accurate to +/- 0.25% No specific access platform 1.8 m (5 ft. 11 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
1EFF : ALL 1 32-31-73Page A501 1 1 May 01/05 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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