TCH.1C-27J-2-27JG
2-47.1
ADJUSTMENT PILOT (COPILOT) CONTROL
STICK TO FORWARD QUADRANT (refer to figure
) and (refer to figure
) (Cont'd)
19.Connect the LH (RH) linkage rod (16) at the LH (RH)
control stick (12) by using bolt (4), washer (13),
special washer (6), spring (5), spacer (7), castellated
nut (14) and new cotter pin (15) (LMC NO. 00010).
20.Connect the LH (RH) linkage rod (16) at the LH (RH)
bellcrank (34) by using bolt (33), washer (31),
bushings (32), castellated nut (30) and new cotter pin
(29) (LMC NO. 00052).
21.Check that the LH (RH) rod axis (22) and the LH (RH)
lever axes (18) are positioned at 90
°
±
1
°
.
NOTE
If necessary, to obtained the above
requirement, adjust properly the RH linkage
rod (22). Would this not be enough, adjust
also the RH linkage rod (16).
22.Check for correct engagement of the sliding terminal
through the inspection hole. No more than 3 threads
must be visible.
23.Remove both rigpins (1 and 35) (AGE NO. 00181).
2-47.2
CENTERING SPRING ADJUSTMENT (refer to
figure
NOTE
The following procedure is valid for left side.
For right side is similar.
1.Insert a 0.193 in (4.915 mm) (AGE NO. 00181) (37
and 39) diameter rigging pin to the LH and RH rear
quadrants (38 and 40) to ensure neutral position.
(Cont'd)
27-30-15
2-399