(2)
Make sure that the replaced component is correctly installed.
(3)
Make sure that the hydraulic reservoir of the Blue hydraulic system is pressurized. If necessary pressurize it (Ref. TASK 29-14-00-614-002).
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4. Procedure
_________
Subtask 29-00-00-870-065
A. Bleeding Procedure of the Blue Hydraulic System Downstream of the Blue E-Pump
NOTE : Do the bleeding procedure in the sequence that follows, to make
____
sure that no air stays in the hydraulic system.
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(3)
Operate the flight controls. NOTE : Make sure that when you operate the flight controls, you
____ monitor the ECAM display and read the level of the reservoir. If the fluid level becomes low, add fluid as necessary (Ref. TASK 12-12-29-611-002) or (Ref. TASK 12-12-29-611-001).
(a)
Make sure that the slat flap control lever on the center pedestal is in the 0 position.
(b)
Make sure that the speed-brake control lever on the center pedestal is in the RET position.
(c)
Make sure that the two side stick controllers are in the neutral position and that there is no priority on them.
(d)
Extend and retract the spoilers (Ref. TASK 27-64-00-710-001). Do this procedure two times.
NOTE : Operate only the spoilers and ignore the specific test
____ procedure of the system which is described in the referenced task.
(e)
Move one of the two side stick controllers to the left and then to the right, and back to the neutral position to operate the ailerons. Do this procedure two times.
(f)
Extend and retract the slats (Ref. TASK 27-80-00-866-004) and (Ref. TASK 27-80-00-866-005). Do this procedure two times.
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(g) Operate the flap wing tip brake (Ref. TASK 27-51-00-710-001). Do this procedure two times.
NOTE : Operate only the flap wing tip brake and ignore the
____ specific test procedure of the system which is described in the referenced task.
(h) Operate the slat wing tip brake (Ref. TASK 27-81-00-710-001). Do this procedure two times.
NOTE : Operate only the slat wing tip brake and ignore the
____ specific test procedure of the system which is described in the referenced task.
(4) Operate the CSM/G.
NOTE : When you operate the Constant Speed Motor/Generator (CSM/G),
____ obey the fluid level in the Blue reservoir. Add fluid as necessary (Ref. TASK 12-12-29-611-002) or (Ref. TASK 12-12-29-611-001).
(a) Pressurize the Blue hydraulic system with the Blue E-pump (Ref. TASK 29-10-00-863-003).
NOTE : Do this procedure three times. If you hear unusual noise
____ or vibrations during this time, do the procedure again.
NOTE : You can ignore the warning indications during the
____
operation of the CSM/G.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 21VU: On the lower ECAM display unit:
- open the guard, press and hold - the ELEC page comes into view pushbutton switch EMER GEN TEST automatically. 23XE. - the green lines between the AC1 and
the DC ESS busbar and the DC1 and the DC ESS busbar go out of view,
-the EMER GEN and ESS TR indications are shown in white. The parameters are shown in green.
-green lines come on between: EMER GEN and AC ESS, EMER GEN and ESS TR, ESS TR and DC ESS indications.
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-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
2. On the overhead panel 21VU:
-release the pushbutton switch EMER GEN TEST.
(5) Operate the flight controls:
-the SHED indication comes into view below the AC ESS and DC ESS busbar indications.
NOTE : If the essential TR is not in
____ line:
-its related parameters are shown in amber,
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