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TCH.1C-27J-2-27JG
2-47.1 ADJUSTMENT OF ELEVATOR NEUTRAL
POSITION (refer to figure 
1-52, sheet 1/6
) , (refer
to figure 
1-52, sheet 2/6
) , (refer to figure 
1-52,
sheet 3/6
) and (refer to figure 
1-52, sheet 4/6
)
(Cont'd)
3.Adjust the LH (RH) linkage rod (23) as per its nominal
dimension and connect it between the LH (RH)
bellcranck (25) on the LH (RH) rear quadrant and the
LH (RH) elevator control lever (24), taking care to
maintain aligned the reference mark on the lever and
on the rear quadrant.
4.Check that the LH (RH) elevator is to 0 ° ± 0.25° read
on the template (neutral position).
5.If necessary, adjust properly the LH (RH) linkage rod
(5) to set the LH (RH) elevator to neutral position.
6.Verify the correct engagement of the threads end.
Check that no more than 3 threads are visible on each
terminal lug.
7.Verify that the difference of neutral position between
left and right elevator does not exceed 0.1°.
8.Remove rigging pin (AGE NO. 00181) (1 and 3) from
LH (RH) rear quadrant (2 and 4).
9.Remove the template (AGE NO. 00065) from the LH
(RH) elevator trailing edge.
2-47.2 MEASUREMENT OF ELEVATOR
CONVENTIONAL PLAY - LEFT ELEVATOR
LOADING (refer to figure 
1-52, sheet 4/6
)
1.Install the template (AGE NO. 00065) on LH (RH)
elevator trailing edge.
2.Stiffen by proper tools (AGE NO. 00016) the LH
Stabilizer in order to avoid loss of reading accuracy on
elevator.
3.Connect external AC power supply to aircraft (refer to
manual 
TCH.1C-27J-2-00GV
).
(Cont'd)
27-30-10
2-365