1EFF : ALL 1 12-36-29Page A397 1 1 May 01/04R 1 1 1CES 1
(5)
Disconnect the HP1 and HP2 line between the aircraft and the TOOL -HYDRAULIC FLUID CHANGE (DH0501).
(6)
Disconnect all the lines between the TOOL - HYDRAULIC FLUID CHANGE (DH0501) and the hydraulic power cart.
(7)
Remove the dummy bowl of the HP hydraulic filter (2048GM) and replace the filter element (Ref. TASK 29-12-45-610-001).
(8)
Pressurize the Blue hydraulic reservoir (Ref. TASK 29-14-00-614-002).
(9)
Operate the flight controls and monitor the reservoir level. If necessary fill the Blue hydraulic reservoir (Ref. TASK 12-12-29-611-002).
(10) Each week, do a new sampling of the fluid (Ref. TASK 12-32-29-281-001).
(11) Remove the warning notice(s). Subtask 12-36-29-865-061
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1701GK, 1702GK, 3700GD, 3701GD, 3801GX, 3802GX, 3803GX
Subtask 12-36-29-410-089
D. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Close the access doors 197EB and 195BB.
(4)
Close the main landing gear door (Ref. TASK 32-12-00-410-001).
(5)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
