TM 55-1520-240-23-6
7-16
FILLING AND BLEEDING FLIGHT CONTROL HYDRAULIC SYSTEMS
(Continued)
7-16
26.
In cockpit, cycle SYSTEM SEL switch (12) on
AFCS panel (13) from OFF to 2 to OFF five times.
27.
Set SYSTEM SEL switch (12) to 2.
28.
In cabin, remove lockwire from bleed plug (28)
on No. 2 extensible link (29) of each integrated
lower controls actuator (ILCA) (16).
29.
Loosen bleed plug (28) on each ILCA (16). Use
container and cloths (E120). When fluid flow
from each bleed plug is airfree tighten plug.
Install lockwire (E231).
7-103