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 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)
3. Job Set-up
__________
Subtask 24-24-00-860-050
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.
1EFF : ALL 1 24-24-00Page 501 1 1 May 01/03R 1 1 1CES 1
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).
(3)
Pressurize the Blue hydraulic system with the Blue electric pump (Ref. TASK 29-10-00-863-003).
(4)
On the FLAPS control panel 114VU:
-
Make sure that the slat/flap control lever is on 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 24-24-00-010-051
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.
Subtask 24-24-00-865-050
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FWS/FWC1/SPLY 3WW F01 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 121VU EIS/FWC2/SPLY 2WW Q07 122VU ELEC/EMER GEN AUTO/2 9XE Z26 122VU ELEC/EMER GEN AUTO/1 11XE Z25
4. Procedure
_________ Subtask 24-24-00-710-050
A. Operational Test of the Emergency Generation System
-------------------------------------------------------------------------------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.
2. On the panel 21VU:
-release 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.
NOTE : - If the essential TR is not in
____ line: . its related parameters are shown in amber and . the green line between the essential TR and the DC essential busbar is not shown.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ELECTRICAL POWER 電源1(164)
