TCH.1C-27J-2-27JG
PROCEDURE:
2-92.1
GUST LOCK CABLE TENSION (refer to figure
) , (refer to figure
(refer to figure
)
1.Insert a rigging pin (8) (AGE NO. 00181) in the cabin
quadrant of gust-lock control (9).
2.By means of turnbuckles (5 and 10 ) positioned in
corrispondence of frame 11, 35, 36 and in the centre
wing, stretch the control cables at a load twice the
expected pre-load 128.14 lb (58.12 kg) (AGE NO.
00113).
3.Remove the rigging pin (8) (AGE NO. 00181) and
perform 25 cycles at least of the gust lock lever (6) on
the Throttle Quadrant (7).
4.Insert the rigging pin (8) (AGE NO. 00181) in the
cabin quadrant of gust-lock control (9) and set the
control cables pre-load to 64.07 lb (29.06 kg) (AGE
NO. 00113).
5.Check that the distance between the bellcrank and the
frame 44 is 1.949
±
0.079 in (49.5
±
2 mm).
6.On the elevator gust lock control, the distance
between the connecting bolt axis of the bellcrank (11)
to the push-pull cable (12) and the frame 42 axis is
1.417
±
0.079 in (36
±
2 mm).
7.On the aileron gust lock control, the distance between
the axis of the connecting bolt of the control cable (14)
to the bellcrank (15) and the rotation pin of the
bellcrank is 1.024
±
0.079 in (26
±
2 mm) towards
the wing tip.
2-92.2
ADJUSTMENT AND CHECK OF UNLOCKING
POSITION (refer to figure
(refer to figure
(Cont'd)
27-70-00
2-701