-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
3. On the ECAM control panel:
-get the ELEC page.
4. On the ECAM control panel:
-push the STS key to get the STATUS page.
5. On the panel 49VU: - open and close the circuit
breaker 3WW. On the panel 121VU: - open and close the circuit
breaker 2WW.
(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 lower ECAM display unit:
-the normal configuration comes into view (the emergency AC generator stops).
On the STATUS page of the lower ECAMdisplay unit:
-if the AIR BLEED indication comes into view below the INOP SYS item, it is necessary to reset the two FWCs. Thus the FWCs will not keep a record of the indication in the POST FLIGHT REPORT at the next flight. Do the step that follows.
On the STATUS page:
-the AIR BLEED indication goes out ofview.
5. Close-up________
Subtask 24-24-00-860-051
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 R (3) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) of 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 24-24-00-410-051
B. Close Access
(1) Close the access doors 812 and 822.
(2) Remove the warning notice(s).
(3) Remove the access platform(s).
TASK 24-24-00-710-001- 01
Operational Test of the Emergency Generation System with either the Blue Electric Pump or a Ground Hydraulic Cart
1. Reason for the Job
__________________
Refer to the MPD TASK: 242400-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice No specific access platform 1.8 m (5 ft. 11 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 29-10-00-863-003 Pressurize the Blue Hydraulic System with the Blue
Electric Pump 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure TSM 24-24-00-810-806 Result of the EMER GEN Test Incorrect (Failure of the
Switching)
1EFF : ALL 1 24-24-00Page 506 1 1 Nov 01/03R 1 1 1CES 1
3. Job Set-up
__________
Subtask 24-24-00-860-055
A. Aircraft Maintenance Configuration
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
CAUTION : DO NOT OPERATE THE FLAPS AND SLATS WHEN ONE OR MORE "LEAK
_______ MEASUREMENT VALVES" PUSHBUTTON SWITCHES ARE IN THE RELEASED POSITION ("OFF" LEGEND ON). OPERATION OF THE FLAPS AND SLATS IN THIS CONFIGURATION CAN CAUSE JAMMING OF THE MECHANICAL TRANSMISSION.
(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).
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