3.
obey the intructions such as INITIAL CONDITIONS and press the line key adjacent to START TEST
5. Close-up
________
Subtask 31-60-00-860-084
-the DMC 1 (2), (3) main menu pagecomes into view
-MAINTENANCE MODE message comes into view on the CAPT PFD,CAPT ND, SD and EWD
-
the DMC 1 (2), (3) SWITCHING/DATA BUSAND DU BRIGHTNESS TESTS page comes into view
-
the DMC1 (2), (3) DATA BUS TEST pagecomes into view
-
the DMC 1 (2), (3) DATA BUS TEST pagecomes into view with the message:TEST IN PROGRESS 55s
-after 55s teh DMC 1(2), (3) DATA BUS TEST page comes into view with the result of the test: TEST OK.
-press the line key adjacent to RETURN indication.
A. Put the aircraft back to its initial configuration.
(1)
On the MCDU, push the line key adjacent to the RETURN indication until the MAINTENANCE MENU 1/2 page comes into view
(2)
On the MCDU, set the BRT knob to OFF.
(3)
Do the EIS Stop Procedure (Ref. TASK 31-60-00-860-002)
R 1EFF : 401-499, 1 31-60-00Page 564 1 1 Aug 01/05 1 1 1CES 1
(4)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : 401-499, 1 31-60-00Page 565 1 1 Aug 01/05 1 1 1CES 1 EIS - CONTROL - DESCRIPTION AND OPERATION
_________________________________________
1.
General
_______ This document defines EIS power supply in normal and emergency configurations and also EIS controls which are at the crew's disposal.
2.
EIS Component Location
______________________
(Ref. Fig. 001)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 002)
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 003)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 004)
**ON A/C ALL
(Ref. Fig. 005)
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL |ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------1WT1 DMC-1 85VU 127 824 31-63-34 1WT2 DMC-2 86VU 128 824 31-63-34 1WT3 DMC-3 85VU 127 824 31-63-34 2WT1 PFD-CAPT 3VU 211 831 31-63-22 2WT2 PFD-F/O 5VU 212 831 31-63-22 3WT1 ND-CAPT 3VU 211 831 31-63-22 3WT2 ND-F/O 5VU 212 831 31-63-22 4WT1 DU-ECAM, UPPER 4VU 211 831 31-63-22 4WT2 DU-ECAM, LOWER 4VU 211 831 31-63-22 6WT CTL PNL-ECAM 11VU 211 831 31-61-12 7WT1 POT-PFD, CAPT 301VU 211 7WT2 POT-PFD, F/O 500VU 212 8WT1 POT-ND, CAPT 301VU 211 8WT2 POT-ND, F/O 500VU 212
1EFF : ALL 1 31-61-00Page 1 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL |ZONE|ACCESS | ATA | | | | DOOR | REF. -------------------------------------------------------------------------------
9WT1 P/BSW-PFD/ND XFR, CAPT 301VU 211
9WT2 P/BSW-PFD/ND XFR, F/O 500VU 212
18WT SEL SW-EIS DMC 8VU 211 831
19WT SEL SW-ECAM/ND XFR 8VU 211 831
20WT1 RELAY BOX-CAPT PFD-ND XFR 301VU 211 831
20WT2 RELAY BOX-F/O PFD-ND XFR 500VU 212 831
25WT1 P/BSW-CHRONO, CAPT 131VU 211
25WT2 P/BSW-CHRONO, F/O 130VU 212
26WT RELAY-BUS1 TO ESS BUS SWTG, DMC3 103VU 126
1WV1 SDAC-1 85VU 127 824 31-55-34
1WV2 SDAC-2 86VU 128 824 31-55-34
1WW1 FWC-1 85VU 127 824 31-53-34
1WW2 FWC-2 86VU 128 824 31-53-34
7WW LOUD SPEAKER-CAPT 2VU 211 831 31-53-21
8WW LOUD SPEAKER-F/O 6VU 212 831 31-53-21
9WW1 LT-MASTER WARN, CAPT 131VU 211
9WW2 LT-MASTER WARN, F/O 130VU 212
11WW1 LT-MASTER CAUT, CAPT 131VU 211
11WW2 LT-MASTER CAUT, F/O 130VU 212
13WW1 WARN LT-AUTO LAND, CAPT 131VU 211
13WW2 WARN LT-AUTO LAND, F/O 130VU 212
15RN1 POT LOUD SPEAKER, CAPT 301VU 211
15RN2 POT LOUD SPEAKER, F/O 500VU 212
1EFF : ALL 1 31-61-00Page 2 1 1 Feb 01/05R 1 1 1CES 1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 7(96)
