TM 55-1520-240-23-6
7-16
FILLING AND BLEEDING FLIGHT CONTROL HYDRAULIC SYSTEMS
(Continued)
7-16
9.
In cabin, remove lockwire from bleed plug (14)
on No. 1 extensible link assembly (15) of each
integrated lower controls actuator (ILCA) (16).
10.
Loosen bleed plug (14) on each ILCA (16). Use
container and cloths (E120). When fluid flow
from each bleed plug is air-free, tighten plug.
Install lockwire (E231). Use gloves (E186).
11.
At No. 1 reservoir/cooler (17) open bleed valve
(18) until all air is bled. Close bleed valve.
12.
Service No. 1 reservoir (17) (Task 1-61 or 1-63).
7-100
