TCH.1C-27J-2-27JG
2-68.2
(refer to figure
) (Cont'd)
6.Insert the flap cable (3) in the second pulley seat (24).
7.Connect the second pulley (24) to the flap tension
regulator (14) using bolt (12), washers (13 and 22),
castellated nut (23) and new cotter pin (21).
8.Remove the lock tension regulator proper tools with
related red flag.
9.Install the clips (28 and 29) to the turnbuckles (31 and
30) and stretch the flap cables (3 and 4).
10.Remove the rigging pin (33) (AGE NO. 00181) from
the flap quadrant (32) placed in the centre wing.
11.Remove the rigging pin (1) (AGE NO. 00181) from the
forward flap quadrant (2).
FOLLOW ON MAINTENANCE:
1.Close emergency exit door 885A.
2.Remove emergency stair.
3.Close the access panels 553A, 553B and 553C.
4.Remove maintenance platform (AGE NO. 00074).
5.Close the access panels 130AG, 130AE, 711A, 712A,
130B, 130C and 220FZ.
6.Restore hydraulic power system (refer to manual
7.Connect electrical power to aircraft (refer to manual
8.Perform the functional test:
) .
9.Perform a visual check on tension regulator scale and
record the value displayed.
10.Check if the recorded value is according to the
diagram (refer to figure
27-50-15
2-560