TCH.1C-27J-2-27JG
2-22.2 INSTALLATION (refer to figure
(refer to figure
) , (refer to figure
) (Cont'd)
10.Connect the retaining clips (51, 52, 54 and 56) and
acting on the turnbuckles (57, 58, 59 and 60) between
frames 10 and 12. (If has been removed, replace the
LH / RH AILERON FUSELAGE CABLE in accordance
with maintenance task remove/replace LH / RH
aileron fuselage cable (refer to para
11.Connect the retaining clips (27, 29, 30, 35, 37 and 38)
and acting on the turnbuckles (28, 31, 36 and 39). If
has been removed, replace the LH / RH AILERON
CABIN CABLE in accordance with maintenance task
remove/replace LH / RH aileron cabin cable (refer to
) .
12.Perform cable tension (refer to para
13.Remove a rigging pins (47 and 50) (AGE NO. 00181)
from LH sector group (48) and from RH sector group
(49) located in the center wing section.
14.Remove a rigging pin (1) (AGE NO. 00181) from LH /
RH control wheel (2).
FOLLOW ON MAINTENANCE:
1.Close the access panels 213DZ, 213CZ, 213BZ and
213AZ (214AZ, 214BZ and 214CZ).
2.Install Pilot and Copilot seat (refer to manual
).
3.Restore hydraulic power system (refer to manual
4.Connect electrical power to aircraft (refer to manual
27-10-15
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