TCH.1C-27J-2-27JG
2-51.1
(refer to figure
3.Disconnect from the position transducer emergency
trim (3CT) (5) the electrical connector (3CTA) (6).
4.Disconnect from the position transducer emergency
trim (3CTA) (5) the connection rod (3) by removing
bolt (4), washer (2) and nut, self-locking (1). Discard
removed nut, self-locking.
5.Disconnect and remove from the aircraft structure the
position transducer emergency trim (3CT) (5) by
removing bolts (9), washers (8) and nuts, self-locking
(7). Discard removed nuts, self-locking.
2-51.2
INSTALLATION (refer to figure
)
and (refer to figure
1.Position and install to the aircraft structure the position
transducer emergency trim (3CT) (5) by using bolts
(9), washers (8) and new nuts, self-locking (LCM NO.
00069) (7).
2.Connect to the position transducer emergency trim
(3CTA) (5) the connection rod (3) by using bolt (4),
washer (2) and new nut, self-locking (LCM NO.
00009) (1).
3.Connect to the position transducer emergency trim
(3CT) (5) the electrical connector (3CTA) (6).
4.Ensure that the LH emergency trim tab is to zero
position.
5.Adjust and connect the linkage rod between the
position LH emergency trim transducer lever and LH
emergency trim attachment point.
6.Check that, on the Combined Trim Indicator (15CB)
(10), the EMERGENCY indication (11) shows about
0
°
.
7.It is necessary to re-adjust the linkage rod and /or the
transducer lever to get 0
°
.
(Cont'd)
27-30-30
2-428