-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific warning notice(s)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-047 C Z-11.904
ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT)
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 19 braid 32-21-43 10 -160 19 braid 32-21-43 10A-160
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D. 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
32-22-00-410-001 Nose Gear Doors - Ground Doors Closing
R 32-49-00-710-001 Operational Test of the Tire Pressure Indicating
R System (TPIS) 32-51-00-710-001 Operational Test of the Nose Wheel Steering with the CFDS. 32-21-43-991-004 Fig. 405
3. Job Set-up
__________
Subtask 32-21-43-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(2)
Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
(3)
Make sure that the warning notice(s) is(are) in position: - on the panel 400VU, to tell persons not to operate the landing gear control lever,
- on the NWS handwheels and the rudder pedals to tell persons not to operate them.
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B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R **ON A/C 051-099,
R 121VU HYDRAULIC/TIRE/PRESS 1GV M31 R **ON A/C 001-004, 051-099,
4. Procedure
_________
Subtask 32-21-43-420-050
A. Installation of the Intermediate Harness:
(Ref. Fig. 405/TASK 32-21-43-991-004)
WARNING : FOR SAFETY STAND AFT OF THE GEAR LEG WHEN YOU OPERATE THE
_______ GROUND OPENING CONTROL OF THE DOOR. CAREFULLY READ THE PLACARD ON THE LEG DOOR BEFORE YOU OPEN THE NOSE GEAR DOORS.
NOTE : Remove the blanking caps from the electrical connectors
____
immediately before you connect them.
NOTE : Apply a layer of SPECIAL MATERIALS (Material No. 05-047) to the
____ threads of all the nuts and bolts before you install them.
(1)
Engage the intermediate harness (22) through the hole of the protector of the torque link assembly (24).
(2)
Hold the intermediate harness (22) in position and:
(a)
Connect the electrical connector (17) to the connector (16).
(b)
Safety the grommets (18) with the braid (19).
(c)
Install the clamp (4), the washer (3) and the screw (2).
(d)
Install the clamp (13), the washers (12) and the screws (11).
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(e) Install the cover (1), the washers (15) and the screws (14).
(f) Install the clamp (7), the washer (6) and the screw (5).
(g) Install the clamp (8), the washer (9) and the screw (10).
(h) Install the support (23), the clamp (21), the bolt (20), the washer (25) and the nut (26).
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