**ON A/C 151-154, 201-207,
(Ref. Fig. 005B)
The FDIU is supplied from the busbar via the circuit breaker 8TU. The power interlock controls the power supply of the DFDR. The LA is connected to the 28 V DC bus, via the circuit breaker 9TU. The supply of the power interlock relays is achieved via the circuit breaker 4RK. The maximum power consumption and the busbar connection is as listed below.
----------------------------------------------------------------------------COMPONENT | PWR.CONS. | VOLTAGE | BUSBAR | C/B
----------------------------------------------------------------------------DFDR | 15 VA | 115 V AC | 202XP NORM | 7TU FDIU | 25 VA | 115 V AC | 202XP NORM | 8TU LA | 2 VA | 28 V DC | 204PP NORM | 9TU
----------------------------------------------------------------------------
**ON A/C 151-199, 201-210,
Post SB 31-1154 For A/C 151-154,201-207,
(Ref. Fig. 005B)
The FDIU is supplied from the busbar via the circuit breaker 8TU. The power interlock controls the power supply of the DFDR. The LA is connected to the 28 V DC bus, via the circuit breaker 9TU. The supply of the power interlock relays is achieved via the circuit breaker 4RK. The maximum power consumption and the busbar connection is as listed below.
----------------------------------------------------------------------------COMPONENT | PWR.CONS. | VOLTAGE | BUSBAR | C/B
----------------------------------------------------------------------------DFDR | 18 VA | 115 V AC | 202XP NORM | 7TU FDIU | 23 VA | 115 V AC | 202XP NORM | 8TU LA | 2 VA | 28 V DC | 204PP NORM | 9TU
----------------------------------------------------------------------------
**ON A/C ALL
5. Interface_________
R 1EFF : ALL 1 31-33-00Page 28 1 1 Aug 01/05 1 1 1CES 1
R Power Supply Figure 005B
R 1EFF : 1 1 1CES 151-199, 201-210, 1 111 31-33-00 Page 29 May 01/05
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
A. FDIU Input Sources
(Ref. Fig. 006)
The following systems are connected to the FDIU:
(1)
Electrical Flight Control System (Ref. 27-90-00)
-FCDC1, FCDC2 (3CE1, 3CE2)
(2)
Independent Instruments System (Ref. 31-20-00)
-GMT CLOCK (2FS).
(3)
Central Warning System (Ref. 31-50-00)
-FWC1, FWC2 (1WW1, 1WW2)
-SDAC1, SDAC2 (1WV1, 1WV2).
(4)
Electronic Instrument System (Ref.31-60-00)
-DMC1, DMC2 (1WT1, 1WT2).
(5)
Wheel and Brakes (Ref. 31-60-00)
-BSCU (10GG).
(6)
Power Supply of Input Sources All parameter source systems are supplied by their own system power supplies.
R **ON A/C 106-149, 211-299, 301-399, 401-499,
A. FDIMU (FDIU-Part) Input Sources (Ref. Fig. 006A) The following systems are connected to the FDIU-part of the FDIMU:
(1)
Electrical Flight Control System (Ref. 27-90-00)
-FCDC1, FCDC2 (3CE1, 3CE2).
(2)
Independent Instruments System (Ref. 31-20-00)
-GMT CLOCK (2FS).
(3)
Central Warning System (Ref. 31-50-00)
-FWC1, FWC2 (1WW1, 1WW2)
-SDAC1, SDAC2 (1WV1, 1WV2).
(4)
Electronic Instrument System (Ref. 31-60-00)
-DMC1, DMC2 (1WT1, 1WT2).
1EFF : ALL 1 31-33-00Page 30 1 1 Aug 01/05 1 1 1CES 1
Block Diagram of Parameter Sources
Figure 006
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-33-00Page 31 1201-210, 1May 01/05 1 1 1CES 1
Block Diagram of Parameter Sources
Figure 006A
R 1EFF : 106-149, 211-299, 301-399, 401-499, 1 31-33-00Page 32 1 1 Aug 01/05 1 1 1CES 1
(5)
Wheel and Brakes (Ref. 31-60-00)
-BSCU (10GG).
(6)
Power Supply of Input Sources All parameter source systems are supplied by their own system power supplies.
**ON A/C ALL
B. Parameters The information about the parameters are in the Flight-Data Recording Parameter-Library (FDRPL).
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
C. FDIU Input/Output Pin Assignment (Ref. Fig. 007) The connection between the related computers and the FDIU is shown in the DFDRS inputs schematic. The summary of the input and output pin assignment is shown in:
-
Table 1 for the discrete inputs
-
Table 2 for the discrete outputs
-
Table 3 for the bus inputs
-
Table 4 for the bus outputs
-
Table 5 for power supply and digital ground.
- 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 2(56)
