(3)
Check of the hydraulic lines
(a)
Make sure that there is no distortion, that there are no cracks that start. Make sure that there are no signs of shock, specially on the elbows and the bends of the lines and on the connection point with other units.
(b)
Make sure that the conduit rails or the metal parts cannot damage the lines in their housings.
(c)
Make sure that there are no leaks of hydraulic fluid on the connectors. Make sure that they are safetied correctly.
(d)
Make sure that the mountings, the clamp blocks of the lines and the attachment collars are installed correctly.
(4)
Check of the hydraulic units
(a)
Make sure that the units are installed correctly. Make sure that there are no leaks on the hydraulic connectors.
(b)
Make sure that the electrical connections are in the correct condition.
(5)
Check of the electrical wiring
(a)
Make sure that the electrical connectors are installed correctly and that they are safetied correctly.
(b)
Make sure that the electrical connectors do not have any contamination from the hydraulic fluids. If it is necessary, clean them.
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R (c) Make sure that the wiring is fully protected and that it is in
R the correct condition.
R (6) Check of the nose landing gear
R Make sure that these components are installed correctly and that they
R are in the correct condition:
R - the electrical harnesses,
R - the connectors and plugs,
R (7) Check of the main landing gear
R Make sure that these components are installed correctly and that they
R are in the correct condition:
R - the hydraulic lines (clamps),
R - the electrical harnesses,
R - do a visual inspection to make sure that there are no signs of
R ageing, overheating, flaking and deformation,
R - the connectors and plugs (tachometers).
R (8) Make sure that there is no hydraulic fluid:
R - on the unions and the points where the lines connect with the
R units,
R - on the supply lines,
R - on the connecting blocks,
R - on the servo valve,
R - on the brakes (the bleed screws, the points where the lines connect
R with the units and the pistons).
R (9) Examine the connections of the wiring of the temperature sensor on
R the aft face of each brake assembly.
R **ON A/C ALL
5. Close-up________
Subtask 32-40-00-860-055
A. Aircraft Maintenance Configuration
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
B. Close Access
(1)
CLose the access doors, the access panels and the doors of the landing gears (Ref. TASK 32-12-00-410-001) (Ref. TASK 32-22-00-410-001).
(2)
If removed, install the brakes (Ref. TASK 32-42-27-400-001).
(3)
If removed, install the wheels (Ref. TASK 32-41-11-400-006).
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TASK 32-40-00-200-002
Inspection/Check of the Brakes
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
29-10-00-863-001 Pressurize the Green Hydraulic System
29-10-00-863-002 Pressurize the Yellow Hydraulic System
R 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-41-11-400-006 Installation of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-42-27-000-001 Removal of the Brake (2641GM,2642GM,2643GM,2644GM) 32-42-27-400-001 Installation of the Brake (2641GM,2642GM,2643GM,2644GM) 32-40-00-991-001 Fig. 601
3. Job Set-up
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本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架6(41)
