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TCH.1C-27J-2-27JG
2-95.1 REMOVAL (refer to figure 
1-113, sheet 1/2
) and
(refer to figure 
1-113, sheet 2/2
) (Cont'd)
8.Disconnect the rod (34) from spoiler actuator lever
(30) by removing bolt (28), washers (29 and 31), nut
(32) and cotter pin (33). Discard removed cotter pin.
9.Disconnect the rod (27) from spoiler actuator ram (23)
by removing bolt (21), washers (22 and 24), nut (25)
and cotter pin (26). Discard removed cotter pin.
10.Disconnect the spoiler actuator (3) from the aircraft
structure support (39) by removing bolts (35, 36, 37
and 38), washers (40, 43, 45 and 47) and self locking
nuts (41, 42, 44 and 46). Discard removed self locking
nuts.
11.Remove the LH (RH) spoiler actuator (3).
12.Position the item on workbench and do the following
operations:
A.Loosen the unions (5 and 13) and remove the
preformed packings (4, 11, 14 and 20). Discard
removed preformed packings.
B.Loosen the nut (9) and tee (8), remove the packing
retainer (10) and preformed packing (11). Discard
removed the packing retainer and preformed
packing.
C.Loosen the nut (18) and elbow (16), remove the
packing retainer (19) and preformed packing (20).
Discard removed the packing retainer and
preformed packings.
2-95.2 INSTALLATION (refer to figure 
1-113, sheet 1/2
)
and (refer to figure 
1-113, sheet 2/2
)
NOTE
Lubricate all packings and O-ring with
hydraulic fluid. If the packing is deteriorate
change it before the installation.
(Cont'd)
27-60-10
2-685