TCH.1C-27J-2-27JG
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00052
PIN, COTTER
MS24665-153
3,00
00179
RING, LOCKING
68538-101
1,00
Safety Conditions:
performingmaintenance.
PROCEDURE:
2-20.1
REMOVAL (refer to figure
), (refer
to figure
1.Insert a rigging pin (2) (AGE NO. 00181) in the pilot
and copilot control column (1) in order to set them
inneutral position.
2.Insert a rigging pin (3) (AGE NO. 00181) in the left
quadrant (4).
3.Insert a rigging pin (6) (AGE NO. 00181) in the right
pulley (5) in outer wing between ribs 23 and 24.
4.Insert a rigging pin (67) (AGE NO. 00181) in the left
pulley (68) in center wing section.
5.On right outer wing trailing edge remove the locking
clips (8, 9,10 and 13), turnbuckles (11 and 14) and
slowly release the tension of cables (12) connecting
the aft quadrant (42) to the right pulley between ribs
23 and 24. Disconnect the cables (7 and 12) to aft
quadrant (42) from the turnbuckles (11 and 14).
6.On the right side of the cargo compartment
ceiling,frame 11, remove the locking clips (15 and 17),
turnbuckles (18), and slowly release the tension ofthe
flap control cables (16) to the aft quadrant (42).Do not
disconnect the cables (16).
(Cont'd)
27-10-15
2-160