Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 O-ring 27-84-51 01 -070 12 back-up rings 27-84-51 01 -150 13 O-rings 27-84-51 01 -160 15 back-up rings 27-84-51 01 -150 20 O-rings 27-84-51 01 -160 21 locking rings 27-84-51 01 -140 30 locking ring 27-84-51 01 -180 31 back-up rings 27-84-51 01 -190 32 O-rings 27-84-51 01 -200 34 back-up rings 27-84-51 01 -190 35 O-rings 27-84-51 01 -200
D. Referenced Information
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REFERENCE DESIGNATION
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12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart 27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000) 27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 27-80-00-866-005 Retracting the Slats on the Ground 27-84-00-710-001 Operational Test of the Slat System 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector
32-12-00-410-001 Close the Main Gear Doors after Access
27-84-52-991-001 Fig. 401
R 27-84-52-991-002 Fig. 402
3. Job Set-up
__________
Subtask 27-84-52-860-053
A. Aircraft Maintenance Configuration
(1)
Make sure that the slats are in the 0 degree position (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed (Ref. TASK 27-00-00-480-002) on the slat/flap control lever.
(3)
Make sure that the access platform is in position at the opening of the main door of the main gear.
(4)
Make sure that the Green and the Blue hydraulic systems are depressurized and put them in the maintenance configuration (Ref. TASK 29-00-00-864-001).
(5)
Make sure that the reservoirs of the Green and the Blue hydraulic systems are depressurized (Ref. TASK 29-14-00-614-001).
(6)
Make sure that the warning notice in position to tell persons not to pressurize the hydraulic systems.
(7)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is installed to lock the left slat transmission.
(8)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is installed to lock the right slat transmission.
(9)
Make sure that a container is in position below the Power Control Unit (PCU) (1).
Subtask 27-84-52-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
(Ref. Fig. 401/TASK 27-84-52-991-001)
Subtask 27-84-52-910-052
A. Preparation for Installation
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
R R R R R R (1) Use a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004) to fully remove the anti-corrosion compound from: - the mating faces of the POB - the mating face of the hydraulic motor - the mating face of the PCU.
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