(Ref. Fig. 403/TASK 27-84-67-991-003)
Slat Attachment at the No. 11 Slat Track
Figure 402/TASK 27-84-67-991-002
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Slat Attachment at the No. 11 Slat Track
Figure 402A/TASK 27-84-67-991-002-A
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slat Attachment at the No. 12 Slat Track Figure 403/TASK 27-84-67-991-003
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Subtask 27-84-67-020-051-A
A. Removal of the No. 5 Slat
(1)
Lift the SLING-SLATS, until it has the weight of the slat.
(2)
Disconnect the slat-to-track bonding strap at No. 11 slat track:
(a)
Remove and discard the lockwire from the bolt (24).
(b)
Remove the nut (19) the washer (20) and the bonding strap (21) from the bolt (24) but do not remove the bolt (24).
(c)
Install the washer (20) and the nut (19) on the bolt (24).
(3)
Disconnect the slat-to-slat interface:
(a)
Remove the nut (6), the bolt (9) and the washer (8) then move the bonding strap (7) away from the bonding tag.
(b)
Remove the screws (1) and the stops (3).
(c)
Remove the weather seal (2).
(d)
Loosen the clamps (5) and then remove the flexible tube (4) and the clamps (5).
(e)
Install blanking-covers on the open ends of the anti-icing ducts.
(4)
At the Nos. 11 and 12 slat tracks:
(a)
Remove and discard the cotter pins (27) from the nuts (35), (47),
(46)
and (45).
(b)
Loosen the nuts (35), (47), (46) and (45), but do not remove them.
(c)
Remove and discard the cotter pins (27) from the nuts (26), (31),
(43)
and (44).
(d)
Remove the items that follow:
-
the nuts (26), (31), (43) and (44)
-
the washers (25), (30), (51) and (52)
-
the bolts (18), (32), (48) and (56)
-
the bush (29).
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NOTE : The bush (29) is a part of the slat track and the slat
____
track linkage assembly.
(5) Lift the slat (30 kg (66.1386 lb)) from the slat tracks.
(6) Move the slat with the hoist and lower it onto the support structure. Subtask 27-84-67-860-053
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
CAUTION : MAKE SURE THAT THE SLAT TRACK LINKS DO NOT TOUCH THE WING, IF
_______ YOU RETRACT THE SLAT SYSTEM AFTER A SLAT HAS BEEN REMOVED.
(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 27-84-67-400-002
Installation of the No. 5 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 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) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27804009001 1 SLING-SLATS
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. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (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)
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