TCH.1C-27J-2-27JG
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00011 NUT, SELF-LOCKING H14-3
8,00
00052 PIN, COTTER
MS24665-153
6,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
NOTE
This procedure is applicable to the LH and
RH aileron outer wing cables, LH and Aft
pulleys in center wing section.
2-11.1 REMOVAL (refer to figure
figure
) and (refer to figure
1.Insert a rigging pin (1) (AGE NO. 00181) in the LH
pulley (2) in center wing section.
2.Insert a rigging pin (14) (AGE NO. 00181) in the pulley
(15) in center wing section.
3.Insert a rigging pin (33) (AGE NO. 00181) in LH and
RH pulleys (34) in outer wing section between ribs 23
and 24.
4.Remove from LH pulley in the center wing section (2)
cable-lock clevis (7) by removing bolts (8), washers
(6), castellated nuts (5) and cotter pins (4). Discard
removed cotter pins.
5.Remove from aft pulley (15) cable-lock clevis (17) by
removing bolts (16), washers (18), castellated nuts
(19) and cotter pins (20). Discard removed cotter pins.
(Cont'd)
27-10-05
2-73