TCH.1C-27J-2-27JG
2-83.2 INSTALLATION (refer to figure
(refer to figure
) (Cont'd)
3.Gain access through opened access panels, manually
hold flap hydraulic actuator control lever (1) fully LH
and keep it in this position.
4.Insert a 0.195 in (4.915 mm) diameter rigging pin (18)
(AGE NO. 00181) into RH sector group (17).
5.Adjust the preselection rod (bungee) (5) and install it
in order to make the connecting bolts (7 and 13)
engage freely.
6.From this position disconnect again the spring rod and
crew 1 turn the adjustable retainer.
7.Connect again the preselection rod (bungee) (5) to
hydraulic actuator lever (1) and the flap cable sector
(12) using proper bolts (7 and 13), washers (6, 4 and
11), castellated nuts (2 and 10) and new cotter pins (3
and 9) (LCM NO. 00052). The spring must have a
0.039 in (1 mm) of traction precharge.
8.Remove the rigging pin (18) (AGE NO. 00181) from
RH sector group (17) and release the hydraulic
supply.
9.Remove the rigging pin (8) (AGE NO. 00181) from
flap cable sector (12).
FOLLOW ON MAINTENANCE:
1.Close the access panels 553A, 553B, 553C and
621N.
2.Remove maintenance platform (AGE NO. 00074).
3.Restore hydraulic power system (refer to manual
4.Connect electrical power to aircraft (refer to manual
27-50-55
2-614