(d)
 Remove:

 -
the nuts (31) and (32)

 -
the washers (30) and (33)

 -
the bolts (39) and (41)

 -
the bush (34).

 (6)
 Lift the slat (41 kg (90.3895 lb)) from the slat tracks.

 (7) Move the slat with the hoist and lower it onto the support strut. **ON A/C ALL
 Subtask 27-84-63-860-053
 B. Removal of Support Equipment
 (1) If you are to install a new slat, remove the SLING-SLATS (Ref. TASK 27-80-00-000-001).
 1EFF : ALL 1 27-84-63Page 413 1 1 Nov 01/03R 1 1 1CES 1

 TASK 27-84-63-400-002
 Installation of the No. 1 Slat
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific pneumatic wrench No specific safety barriers No specific warning notice(s) No specific adjustable access platform 3.5 m (11 ft. 6 in.) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804009001 1 SLING-SLATS 98D27804011000 1 BAR-TURNING 98D27804020000 1 BLOCK-SLAT GAPPING
 1EFF : ALL 1 27-84-63Page 414 1 1 May 01/04R 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 09-001 Material No. 09-016 Material No. 11-026 Material No. 19-003 Material No. 19-010  USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 5 5 5 5 5  cotter pins cotter pins cotter pin cotter pins cotter pin cotter pins  27-84-61 01A-00527-84-61 01B-00527-84-61 02 -00527-84-61 02 -00527-84-61 02A-00527-84-61 02A-005
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
R R R R  20-28-00-912-004 24-42-00-861-001 24-42-00-862-001 27-50-00-000-003  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Energize the Ground Service Network from the External Power De-energize the Ground Service Network Supplied from the External PowerRemoval of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003  Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001) 27-80-00-000-001 Removal of the Hoisting Sling 27-80-00-200-002 Check of the Permitted Aerodynamic Tolerances between
 the Slats 1 thru 5 27-80-00-400-001 Installation of the Hoisting Sling 27-80-00-866-004 Extending the Slats on the Ground 27-84-00-710-001 Operational Test of the Slat System 27-84-45-000-004 Removal of the Torque Shaft 6010CM(6060CM) 27-84-45-400-005 Installation of the Torque Shaft 6010CM(6060CM) 27-84-69-000-001 Removal of the Closing Plates for the Slat Tracks 1
 thru 12
 27-84-69-400-001 Installation of the Closing Plates for the Slat
 Tracks 1 thru 12

 57-41-37-000-006  Removal of the Access Panels 522FB(622FB),
 522JB(622JB), 522KB(622KB), 522LB(622LB),
 522NB(622NB), 522QB(622QB), 522SB(622SB),
 522UB(622UB)

 57-41-37-400-006  Installation of the Access Panels 522FB(622FB),
 522JB(622JB), 522KB(622KB), 522LB(622LB),
 522NB(622NB), 522QB(622QB), 522SB(622SB),
　
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