TCH.1C-27J-2-27JG
2-44.3
) (Cont'd)
C.The backlash value C2 is the distance between the
intersection of the lines U2 and L1 read on the
surface displacement axis.
D.The total resulting backlash C is defined as the
mean value between C1 and C2.
10.Check, from the graph, that the backlash C is 1.5 mm
max (0.2
°
).
11.Remove from the right elevator trailing edge the
comparator.
12.Remove from the elevator the templates.
13.Remove both hydraulic and electric power to the
aircraft.
14.Remove the stiffening tools (AGE NO. 00016) from
the RH stabilizer.
2-44.4
ADJUSTMENT OF ELEVATOR CONTROL
OVERRIDE MECHANISM UNCOUPLING FORCE
(refer to figure
1.Install tool jam override adapter (AGE NO. 00006) on
control stick in order to apply a dynamometer (AGE
NO. 00034).
2.Measure uncoupling force: if override mechanism
uncouples at a load different from 132.276 lb
±
5.511
lb (60 kg
±
2.5 kg).
3.Disconnect link (17) from stop link (9) by removing
bolt (11) , washers (8 and 10) , roller (22) , nut (7) and
cotter pin (6). Discard removed cotter pin.
4.Disconnect link (17) from lever (16) by removing bolt
(12) , washer (13) , nut (18) and cotter pin (19) (LCM
NO. 00017). Discard removed cotter pin.
5.Remove lock wire (15).
6.Loosen nut (14) screw out bolt (21) and washer (20).
(Cont'd)
27-30-10
2-367