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TCH.1C-27J-2-27JG
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054 Kit, torque wrenches
G0001200001-001**
00074 Kit, aircraft assy platform
G0005100001
00181 Kit, flight controls rigging
pins
11G001-C052200-801
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00041 PIN, COTTER
MS24665-302
1,00
00052 PIN, COTTER
MS24665-153
1,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para 
1-9
) before performing
maintenance.
PROCEDURE:
2-73.1 REMOVAL (refer to figure 
1-88, sheet 1/4
) , (refer
to figure 
1-88, sheet 2/4
) and (refer to figure 
1-88,
sheet 3/4
)
1.Gain access through the opened access panels and
insert the rigging pin (1) (AGE NO. 00181) in the
forward flap quadrant (2).
2.Lock the flap quadrant (32) placed in the centre wing
by means a rigging pin (33) (AGE NO. 00181).
3.Lock the flap tension regulator (14) by means a proper
tools.
4.Remove the clips (28 and 29) from the turnbuckles
(30 and 31) and slack the flap cables (3 and 4).
5.Disconnect the first pulley (6) by removing bolt (20),
washers (19 and 9), castellated nut (8) and cotter pin
(7). Discard removed cotter pin.
(Cont'd)
27-50-15
2-563