TCH.1C-27J-2-27JG
Safety Conditions:
Be aware of information contained in Paragraph (refer to
para
maintenance.
PROCEDURE:
2-69.1 ADJUSTMENT OF FLAP CONTROL LEVER (refer
to figure
) and (refer to figure
1.Set the flap control lever (1), in the flight deck, to UP
position.
2.Lock the quadrant (5) at the frame No. 3 by inserting a
rigging pin (4) ∅ 8 mm (AGE NO. 00181) in the
proper hole of the quadrant support.
3.Insert a rigging pin (6) ∅ 4.915 mm (00181) in the last
quadrant (7) at the center wing.
4.Lock the tension regulator by means of a proper tool.
5.Increase the tension of the flap control cables and
stretch them (AGE NO. 00113), by means of two
turnbuckles (2 and 3) at frame No. 11, at a load of
36.71 kg (80.93 lb) (twice the nominal preload).
6.Remove both rigging pins (4 and 6) (AGE NO. 00181)
and perform 25 cycles at least (from UP to DOWN
and vice versa) of the flap control lever (1).
7.Set the pre-load to 18.35 kg (40.45 lb) after that the
rigging pin (4) (AGE NO. 00181) on frame No. 3 has
been inserted and verifying that the rigging pin (4)
enters freely in the last quadrant (5). Do not leave it
inserted.
8.Remove the locking tool from the tension regulator
and check the flap control cables are stretched in
accordance to the (refer to figure
(Cont'd)
27-50-00
2-515