R 1EFF : 061-099, 103-149, 151-199, 202-299, 1 24-50-00Page 20
1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
| | | | DOOR | REF. -------------------------------------------------------------------------------2000VU C/B PNL 2000VU 220 93-00-00 2001VU C/B PNL 2001VU 260 93-00-00
**ON A/C ALL
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS| ATA | | | | DOOR | REF. -------------------------------------------------------------------------------8XH CNTOR-AC SHED ESS BUS 106VU 125 812 24-52-55
The panel 123VU mainly contains:
-
the channel 1 line and transfer contactor and 115 VAC bus 1 (1XP),
-
the channel 2 line and transfer contactor and 115 VAC bus 2 (2XP),
-
the APU generator line contactor (APU GLC) and the external power
contactor. The panel 106VU mainly contains contactors related to the electrical emergency power.
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
The panel 105VU comprises the static inverter contactor.
B. Spare Fuses (Ref. Fig. 002) Panel 120VU also contains a set of 3 spare fuses of different amperage for replacement of the fuses given below if defective:
-350A spare fuse to replace fuses 4PB11 and 4PB21 (Ref. 24-30-00, P. Block 1),
-400A spare fuse to replace fuse 6KA (Ref. 49-42-00, P. Block 1),
-80A spare fuse to replace fuse 20PC1 (Ref. 24-30-00, P. Block 1).
R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
The panel 105VU comprises the static inverter contactor. (Ref. Fig. 002A) **ON A/C ALL
3. System Description
__________________ The distribution busbars are supplied according to various configurations depending on:
-
the procedures applied by the crew members in the different failure configurations,
-
the availability of the various power sources.
The possible configurations are:
-normal flight configuration:
**ON A/C 001-049, 051-060, 101-102, 201-201,
(Ref. Fig. 003)
**ON A/C 061-099, 103-105, 151-158, 202-209,
(Ref. Fig. 003A)
**ON A/C 106-149, 159-199, 210-299, 301-399,
(Ref. Fig. 003B) R **ON A/C 401-499,
R (Ref. Fig. 003C) **ON A/C ALL
-emergency configuration corresponding to the loss of the two main
generators with the auxiliary generator not available:
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(Ref. Fig. 004)
**ON A/C 106-149, 159-199, 210-299, 301-399,
(Ref. Fig. 004A)
Normal Flight Configuration for the Whole Network (AC/DC)
Figure 003
R 1EFF : 001-049, 051-060, 101-102, 201-201, 1 24-50-00Page 23/24 1 1 May 01/05 1 1 1CES
1
Normal Flight Configuration for the Whole Network (AC/DC)
Figure 003A
R 1EFF : 061-099, 103-105, 151-158, 202-209, 1 24-50-00Page 25/26 1 1 May 01/05 1 1 1CES
1
Normal Flight Configuration for the Whole Network (AC/DC)
Figure 003B
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1R Normal Flight Configuration for the Whole Network (AC/DC) R Figure 003C
R 1EFF : 401-499, 1 24-50-00Page 29/30 1 1 Aug 01/05 1 1 1CES
Emergency Configuration for the Whole Network (AC/DC)
Figure 004
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 24-50-00Page 31/32 1201-209, 1Aug 01/05 1 1 1CES
Emergency Configuration for the Whole Network (AC/DC)
Figure 004A
R 1EFF : 106-149, 159-199, 210-299, 301-399, 1 24-50-00Page 33/34 1 1 Aug 01/05 1 1 1CES
1
R **ON A/C 401-499,
R (Ref. Fig. 004B) **ON A/C ALL
- smoke configuration: **ON A/C 001-049, 051-099, 101-105, 151-158, 201-209,
(Ref. Fig. 005) **ON A/C 106-149, 159-199, 210-299, 301-399,
R (Ref. Fig. 005A) **ON A/C 401-499,
R (Ref. Fig. 005B) **ON A/C ALL
NOTE : These configurations are dealt with in their respective ATA chapter.____
R 1EFF : ALL 1 24-50-00Page 35 1 1 Aug 01/05 1 1 1CES 1
INTENTIONALLY BLANK
1 1
24-50-00Page 36
1 1 Aug 01/05R 1 1
1CES 1R Emergency Configuration for the Whole Network (AC/DC) R Figure 004B
R 1EFF : 401-499, 1 24-50-00Page 37/38 1 1 Aug 01/05 1 1 1CES
Smoke Configuration for the Whole Network (AC/DC)
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