(3)
Pressurize the Blue hydraulic system with the Blue electric pump (Ref. TASK 29-10-00-863-003) or with a ground power supply (Ref. TASK 29-10-00-863-003).
(4)
On the FLAPS control panel 114VU:
-
Make sure that the flap/slat control lever is in the 0 position.
-
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is in position on the flap/slat control lever.
-Put a warning notice in position to tell persons not to operate the flap/slat control lever.
(5)
On the HYD section of the panel 50VU, release the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend comes on).
Subtask 24-24-00-010-053
B. Get access to the Avionics Compartment
(1)
Put an access platform at the access doors 812 and 822 of the avionics compartment.
(2)
Open the access doors 812 and 822.
1EFF : ALL 1 24-24-00Page 507 1 1 May 01/03R 1 1 1CES 1
Subtask 24-24-00-865-055
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 106VU CSM/G /EV/MAN/SPLY 6XE B04 106VU ESS TR/CNTOR/CTL 5PE C02
R 106VU ESS TR/SPLY 4PE C01
R 122VU ELEC/EMER GEN AUTO/2 9XE Z26 122VU ELEC/EMER GEN AUTO/1 11XE Z25
4. Procedure
_________
Subtask 24-24-00-710-058
A. Operational Test of the Emergency Generation System
NOTE : You must do this test with either the Blue electric pump or a
____
ground hydraulic cart.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the panel 21VU, on the EMER ELEC PWR section: - lift the safety guard, - push and hold the EMER GEN TEST pushbutton switch. On the lower ECAM display unit:- the ELEC page comes into viewautomatically,- the green lines between the AC1 andthe AC 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 related
parameters are shown in green, - the green lines between the EMER GEN and the AC ESS busbar, the EMER GEN
and the ESS TR, the ESS TR and the DC
ESS busbar come into view,
- the SHED indication comes into view
below the AC ESS and DC ESS busbar
indications.
2. On the panel 21VU: - release the EMER GEN TEST pushbutton switch. On the panel 21VU:- check that the safety guard is backin its place.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------NOTE : (1) The Blue electric pump stops
____ automatically (if you do the test with the Blue electric pump).
(2) If not, on the HYD section of the panel 50VU, push and release the BLUE PUMP/OVRD pushbutton switch. Make sure that the ON legend goes off. The Blue electric pump must stop. Do the trouble shooting of the emergency generation system (Ref. TSM TASK 24-24-00-810-806).
On the HYD section of the panel 50VU:
-the ON legend of the BLUE PUMP OVRD pushbutton switch goes off. The pushbutton switch is released.
3. On the ECAM control panel: On the lower ECAM display unit:
-get the ELEC page. - the normal configuration comes into view (the emergency AC generator stops).
5. Close-up
________
Subtask 24-24-00-860-057
A. Put the aircraft back to its initial configuration.
(1)
If the test continues for more than 30 seconds, on the panel 22VU, the FAULT legend of the EXTRACT pushbutton switch comes on. In this case, release then push the EXTRACT pushbutton switch (the FAULT legend goes off).
(2)
On the HYD section of the panel 50VU, push the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend goes off).
R (3) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) of R the flap/slat control lever.
R (4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
R (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 24-24-00-410-053
B. Close Access
(1) Close the access doors 812 and 822.
(2) Remove the warning notice(s).
(3) Remove the access platform(s).
TASK 24-24-00-710-002
Operational Test of the Emergency Generator Control Unit (GCU) from Centralized Fault Display System (CFDS)
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