TCH.1C-27J-2-27JG
2-20.1
REMOVAL (refer to figure
), (refer
to figure
7.Disconnect the bungee (20) from sector assembly
(19).
8.On the center wing section remove the locking
clips(60 and 62), turnbuckles (61 and 63) and
slowlyrelease the tension of cables (34) connecting
the aftquadrant to left pulley (68). Disconnect the
cables(34) from turnbuckles (61 and 63).
9.On center wing section, remove thelocking clips (58
and 64), turnbuckles (59 and 65), and slowly
releasethe tension of cables (35) connecting the
aileronautopilot actuator (66) to aft quadrant
(42).Disconnect the cables (35) from turnbuckles (59
and65).
10.Disconnect the retaining rings (21 and 23), the locking
nuts (22 and 24), and remove the fair lead sector (25)
from the support (44).
11.Disconnect cable (26) from the sector assembly (56).
12.Remove the sector assembly (56) with two bearings
(28 and 57) and spacer (27) from support (44).
13.Disconnect locking ring (30), locking nut (29) and
fairlead flange (31) from the support (44). Discard
removed the locking ring.
14.Disconnect from the aft quadrant (42) the bolts (40, 46
and 55), flat washers (38, 48 and 53), the castellated
nuts (36, 49 and 51), the cotter pins (37, 50 and 52)
and cable lock clevises (39, 47 and 54). Discard
removed cotter pins.
15.From the grooves of the aft quadrant (44) remove the
cables (34, 35 and 41), to the copilot control wheel, to
LH pulley, to right aileron and to autopilot actuator.
(Cont'd)
27-10-15
2-161