(a)
 Loosen the clamps (5) and then remove the flexible tube (4) and the clamps (5).

 (b)
 Install blanking covers on the open ends of the anti-icing ducts.

 (4)
 At the Nos. 7 and 8 slat tracks:

 (a)
 Remove and discard the cotter pins (18) from the nuts (29), (46),

 (54)
 and (55).

 (b)
 Loosen the nuts (29), (46), (54) and (55) but do not remove them.

 (c)
 Remove and discard the cotter pins (18) from the nuts (22), (26),

 (48)
 and (50).

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 Slat Attachment at the No. 7 Slat Track Figure 402/TASK 27-84-65-991-002
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 Slat Attachment at the No. 8 Slat Track Figure 403/TASK 27-84-65-991-003
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 (d) Remove:
 -
the nuts (22), (26), (48) and (50)

 -
the washers (23), (27), (47) and (49)

 -
the bolts (19), (24), (40) and (41)

 -
the bush (17).
 NOTE : The bush (17) is a part of the slat track and the slat

____
 track linkage assembly.

 (5) Lift the slat from the slat tracks.
 (6) Move the slat with the hoist and lower it onto the support structure. Subtask 27-84-65-860-053
 B. Aircraft Maintenance Configuration
 (1) If you are to install a new slat, remove the SLING-SLATS (Ref. TASK 27-80-00-000-001).
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 TASK 27-84-65-400-002
 Installation of the No. 3 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 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804009001 1 SLING-SLATS 98D27804011000 1 BAR-TURNING 98D27804020000 1 BLOCK-SLAT GAPPING
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 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A
 FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
 Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  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)-
R 24-42-00-862-001 De-energize the Ground Service Network Supplied from R the External Power 27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 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)
 27-84-69-400-001 Installation of the Closing Plates for the Slat

 Tracks 1 thru 12
 30-11-41-000-001 Removal of the Telescopic Duct
　
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