GEN 2 OFF _ Upper and Lower ECAM Display Unit
Figure 014 (SHEET 1)
1EFF : ALL 1 24-22-00 Page 84
1 1 Aug 01/05
1 1
1CES 1
GEN 2 OFF _ Upper and Lower ECAM Display Unit
Figure 014 (SHEET 2)
1EFF : ALL 1 24-22-00 Page 85
1 1 Aug 01/05
1 1
1CES 1
INTENTIONALLY BLANK
1 1
24-22-00Page 86
1 1 Aug 01/05 1 1 1CES 1
BTC-1 Supply - Schematic Diagram
Figure 015
1EFF : 001-049, 051-099, 101-149, 151-199, 1 24-22-00Page 87/88 1201-299, 301-399, 1Aug 01/05 1 1 1CES R BTC-1 Supply - Schematic Diagram R Figure 015A
1EFF : 401-499, 1 24-22-00Page 89/90 1 1 Aug 01/05 1 1 1CES
**ON A/C ALL
BTC2 control is symmetrical to BTC1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
(Ref. Fig. 016)
R **ON A/C 401-499,
R (Ref. Fig. 016A)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
GCU1 or GCU2 enables closure of BTC1 or BTC2 if: - no DP zone 2 condition, - no GLC welded failure occurred. Networks 1 and 2 are supplied in priority order: - by the corresponding generator, - by the electrical ground power unit, - by the auxiliary generator, - or by the other generator.
NOTE : BTC's 1 and 2 can be locked out by pressing BUS TIE pushbutton____ switch located on ELEC overhead panel (Ref. 24-00-00). This causes both channels to be isolated.
In case of transfer impossibility or inhibition, AC BUS 1 or AC BUS 2 are lost. The procedure to be applied in case of loss of these busbars is shown in figures.
(Ref. Fig. 017, 018)
R **ON A/C 401-499,
R R R R R R GCU1 or GCU2 enables closure of BTC1 or BTC2 if: - no DP overcurrent or Delta Current condition, - no GLC welded failure occurred. Networks 1 and 2 are supplied in priority order: - by the corresponding generator, - by the electrical ground power unit,
R R - by the auxiliary generator, - or by the other generator.
R R R NOTE : BTC's 1 and 2 can be locked out by pressing BUS TIE pushbutton____ switch located on ELEC overhead panel (Ref. 24-00-00). This causes both channels to be isolated.
R R R R R R R In case of transfer impossibility or inhibition, AC BUS 1 or AC BUS 2 are lost. The procedure to be applied in case of loss of these busbars is shown in figures. (Ref. Fig. 017, 018)
R **ON A/C ALL
C. Smoke Detection In case of smoke detection, amber SMOKE legend comes on on GEN 1 LINE pushbutton switch located on cockpit overhead panel (Ref. 24-00-00). It is accompanied by the single chime and the MASTER WARN. Then, the crew has to follow the procedure shown in figures
(Ref. Fig. 019)
NOTE : This smoke procedure is also described in Ref. 24-24-00 since the____ emergency generator is used in the smoke configuration.
R **ON A/C 001-049, 051-060, 101-101, 401-499,
6. BITE Test_________
R **ON A/C 001-049, 051-060, 101-101,
A. Conditions of Power-up Test Initialisation
(1) How long the computer must be de-energized: - 15 ms.
(2) A/C configuration: - A/C on ground and engines shutdown.
BTC-2 Supply - Schematic Diagram
Figure 016
1EFF : 001-049, 051-099, 101-149, 151-199, 1 24-22-00Page 93/94 1201-299, 301-399, 1Aug 01/05 1 1 1CES R BTC-2 Supply - Schematic Diagram R Figure 016A
1EFF : 401-499, 1 24-22-00Page 95/96 1 1 Aug 01/05 1 1 1CES
INTENTIONALLY BLANK
1 1
24-22-00Page 97
1 1 Aug 01/05 1 1 1CES 1
AC BUS 1 Fault - Upper and Lower ECAM Display Unit
Figure 017 (SHEET 1)
1EFF : ALL 1 24-22-00 Page 98
1 1 Aug 01/05
1 1
1CES 1
AC BUS 1 Fault - Upper and Lower ECAM Display Unit
Figure 017 (SHEET 2)
1EFF : ALL 1 24-22-00 Page 99
1 1 Aug 01/05
1 1
1CES 1
AC BUS 2 Fault - Upper and Lower ECAM Display Unit
Figure 018 (SHEET 1)
1EFF : ALL 1 24-22-00 Page A0
1 1 Aug 01/05
1 1
1CES 1
AC BUS 2 Fault - Upper and Lower ECAM Display Unit 中國航空網 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(109)
