-
FOR 1000EM2
447AL, 448AR.
(3)
Remove the warning notice(s).
AC MAIN GENERATION - DESCRIPTION AND OPERATION______________________________________________
1. General_______ The two engine generators provide the AC main generation. The AC main generation supplies the whole aircraft in normal flight configuration. The transfer circuit supplies either one or the two distribution networks from any generation source: - main, - auxiliary, - or ground.
2. Component Location__________________
**ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
(Ref. Fig. 001)
**ON A/C 063-099, 106-149, 153-199, 206-299, 301-399,
(Ref. Fig. 001A)
R **ON A/C 401-499,
R (Ref. Fig. 001B)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
(Ref. Fig. 002)
R **ON A/C 401-499,
R (Ref. Fig. 002A)
AC Main Generation - Component Location
Figure 001 (SHEET 1)
R 1EFF : 001-049, 051-062, 101-105, 151-152, 1 24-22-00Page 2 1201-205, 1May 01/05 1 1 1CES 1
AC Main Generation - Component Location
Figure 001 (SHEET 2)
R 1EFF : 001-049, 051-062, 101-105, 151-152, 1 24-22-00Page 3 1201-205, 1May 01/05 1 1 1CES 1
AC Main Generation - Component Location
Figure 001A (SHEET 1)
R 1EFF : 063-099, 106-149, 153-199, 206-299, 1 24-22-00Page 4 1301-399, 1May 01/05 1 1 1CES 1
AC Main Generation - Component Location
Figure 001A (SHEET 2)
R 1EFF : 063-099, 106-149, 153-199, 206-299, 1 24-22-00Page 5 1301-399, 1May 01/05 1 1 1CES 1
R AC Main Generation - Component Location
R Figure 001B (SHEET 1)
R 1EFF : 401-499, 1 24-22-00 Page 6
1 1 Aug 01/05
1 1
1CES 1
R AC Main Generation - Component Location
R Figure 001B (SHEET 2)
R 1EFF : 401-499, 1 24-22-00 Page 7
1 1 Aug 01/05
1 1
1CES 1
R AC Main Generation - Component Location
R Figure 001B (SHEET 3)
R 1EFF : 401-499, 1 24-22-00 Page 8
1 1 Aug 01/05
1 1
1CES 1
INTENTIONALLY BLANK
R 1 1
24-22-00Page 9
1 1 Aug 01/05 1 1 1CES 1
AC Main Generation - Component Location
Figure 002 (SHEET 1)
1EFF : 001-049, 051-099, 101-149, 151-199, 1 24-22-00Page 10 1201-299, 301-399, 1Aug 01/05R 1 1 1CES 1
AC Main Generation - Component Location
Figure 002 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 24-22-00Page 11 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1
R AC Main Generation - Component Location
R Figure 002A (SHEET 1)
1EFF : 401-499, 1 24-22-00 Page 12
1 1 Aug 01/05
1 1
1CES 1
R AC Main Generation - Component Location
R Figure 002A (SHEET 2)
R 1EFF : 401-499, 1 24-22-00 Page 13
1 1 Aug 01/05
1 1
1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
-------------------------------------------------------------------------------
FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA
| | | | DOOR | REF.
-------------------------------------------------------------------------------
1XU1 GCU-1 91VU 121 811 24-22-34
1XU2 GCU-2 91VU 121 811 24-22-34
3XU1 P/BSW-ELEC/GEN 1 35VU 210 831 24-22-00
3XU2 P/BSW-ELEC/GEN 2 35VU 210 831 24-22-00
9XU1 GLC-1 120VU 212 831 24-22-55
9XU2 GLC-2 120VU 212 831 24-22-55
10XU P/BSW-ELEC/BUS TIE 35VU 210 831 24-22-00
11XU1 BTC-1 120VU 212 831 24-22-55
11XU2 BTC-2 120VU 212 831 24-22-55
13XU P/BSW-EMER ELEC PWR/SMOKE DRILL 21VU 211 831 24-22-00
22XU1 EGIU-1 95VU 123 811 24-22-33
22XU2 EGIU-2 96VU 123 811 24-22-33
41XU1 CT-AC, 1 131 831 24-22-00
41XU2 CT-AC, 2 133 831 24-22-00
42XU1 CT-AC, 1 120VU 212 831 24-22-00
42XU2 CT-AC, 2 120VU 212 831 24-22-00
42XU3 CT-AC, 1 120VU 212 831 24-22-00
42XU4 CT-AC, 2 120VU 212 831 24-22-00
50XU1 SENSOR-TDC AC, 1 103VU 126 822 24-22-18
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 ELECTRICAL POWER 电源1(95)