TCH.1C-27J-2-27JG
2-44.4
ADJUSTMENT OF ELEVATOR CONTROL
OVERRIDE MECHANISM UNCOUPLING FORCE
(refer to figure
7.Adjust until uncoupling value is obtained.
8.Safety nut (14) with lock wire (15).
9.Reset the elevator control override mechanism using
jam override resetting tool (AGE NO. 00006).
10.Connect link (17) at the lever (16) by using bolt (12) ,
washer (13), nut (18) and new cotter pin (19) (LCM
NO. 00017).
11.Connect link (17) at the stop link (9) by using bolt (11)
, washers (8 and 10), roller (22) , nut (7) and new
cotter pin (6) (LCM NO. 00017).
12.Remove tool jam override adapter (AGE NO. 00006)
on control stick and dynamometer (AGE NO. 00034).
2-44.5
ADJUSTMENT OF BALANCE TAB NEUTRAL
POSITION (refer to figure
(refer to figure
1.Fit balance tab travel templates (AGE NO. 00038) on
LH and RH elevators.
2.Bring LH (RH) tab to neutral position, adjusting rod
connecting intermediate lever to tab. The LH (RH)
balance tab must be at 0
°
±
15
°
as read on the
template (AGE NO. 00038).
3.Remove the templates (AGE NO. 00038) from LH and
RH elevators.
2-44.6
)
1.Connect external AC power supply to aircraft (refer to
).
2.Connect the hydraulic test cart (AGE NO. 00263), via
the adaptor, to the aircraft and supply both hydraulic
systems at 3000 psi (210 Kg/cm
²
).
(Cont'd)
27-30-10
2-368