TCH.1C-27J-2-27JG
2-10.2 INSTALLATION (refer to figure
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figure
) (Cont'd)
8.Insert the retaining clips (15, 17, 18 and 20) then
acting on the turnbuckles (16 and 19) and perform
tension of cables (3 and 4) (refer to para
9.Connect at the LH pulley (27) the cable-lock clevis
(32) by using bolts (33), washers (31), castellated nuts
(29) and new cotter pins (30) (LMC NO. 00052)
10.Connect at the aft pulley (42) the cable-lock clevis
(47) by using bolts (48), washers (46), castellated nuts
(44) and new cotter pins (45) (LMC NO. 00052).
11.Connect at the support (43) of the aft pulley (42) the
fairlead (41) by using rings retaining (35 and 40), nuts
locking (34 and 39), fairlead (36), sector (37) and
spacer (38).
12.Connect at the support (28) of the LH pulley (27) the
fairlead (26) by using nut locking (24) and ring locking
(25).
13.Remove a rigging pin (49) (AGE NO. 00181) from aft
pulley (42) in center wing section.
14.Remove a rigging pin (23) (AGE NO. 00181) from LH
pulley (27) in center wing section.
15.Remove a rigging pin (8) (AGE NO. 00181) from LH
Quadrant (7).
16.Remove a rigging pins (5) (AGE NO. 00181) from
Pilot (Copilot) (6) control wheels.
FOLLOW ON MAINTENANCE:
1.Restore hydraulic power system (refer to manual
2.Connect electrical power to aircraft (refer to manual
27-10-05
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