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
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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) 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap 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
27-54-52-991-001 Fig. 401
27-54-52-991-002 Fig. 402
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-52-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are retracted to the 0 degree position (Ref. TASK 27-50-00-866-009).
(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 main gear main door opening.
(4)
Make sure that the Green and Yellow 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 Yellow hydraulic
systems are depressurized (Ref. TASK 29-14-00-614-001).
(6) Make sure that the warning notice is in position to tell persons not
to pressurize the hydraulic systems.
(7) Put a container in position below the Power Control Unit (PCU) (1).
(8) Make sure that the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) is in
position at the left and right flap track positions 1.
R **ON A/C 301-399,
R Subtask 27-54-52-860-054-A
R A. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are retracted to the 0 degree position
R (Ref. TASK 27-50-00-866-009).
R (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
R (98D27803000000) is installed (Ref. TASK 27-00-00-480-002) on the
R slat/flap control lever.
R (3) Make sure that the access platform is in position at the main gear
R main door opening.
R (4) Make sure that the Green and Yellow hydraulic systems are
R depressurized and put them in the maintenance configuration
R (Ref. TASK 29-00-00-864-001).
R (5) Make sure that the reservoirs of the Green and the Yellow hydraulic
R systems are depressurized (Ref. TASK 29-14-00-614-001).
R (6) Make sure that the warning notice is in position to tell persons not
R to pressurize the hydraulic systems.
R (7) Put a container in position below the Power Control Unit (PCU) (1).
R (8) Make sure that the PIN RIGGING FLAPS (98D27504006000) is in position
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