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时间:2010-05-01 10:13来源:蓝天飞行翻译 作者:admin
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to the SDAC until the fault is corrected.
The CIDS caution message on the ECAM is displayed if
one director fails.
TMUCI2V02-T03 LEVEL 3
EFFECTIVITY 23-73-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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CIDS - WARNINGS / CIDS CAUTION ON ECAM
TMUCI2V02-P03 LEVEL 3
EFFECTIVITY 23-73-00 Page 7
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CIDS - WARNINGS
CIDS CAUTION LIGHT ON FAP
Some CIDS caution message or failure signals also
activate the CIDS CAUT light on the FAP.
NOTE : The CIDS CAUT light is resettable in flight,
but comes on again on the ground (landing gear
down and locked). The light cannot be reset on
the ground. When a CIDS CAUTION occurs, the
respective failure message is displayed on the
Programming and Test Panel.
The CIDS CAUT light comes on if :
- Both directors fail,
- 50% of all type A DEUs fail,
- 20% of adjacent type A DEUs fail zonewise,
- All type B DEUs with a connected handset fail,
- No data from SDCU channel 1 and 2,
- *) The lavatory smoke detector fails,
- *) Lav. fire extinguisher bottle pressure low,
- The heater of the drain mast fails,
- The control unit of the drain mast fails,
- The slides bottle pressure is low,
- The doors bottle pressure is low,
- CIDS Top Bus,
- CIDS Mid Bus,
- DEU-A,
- DEU-B,
- FAP, PTP, CAM,
- No data from CAM,
- No data from FAP,
- No data from PTP.
*) Not for all customers.
TMUCI2V02-T04 LEVEL 3
EFFECTIVITY 23-73-00 Page 8
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CIDS - WARNINGS / CIDS CAUTION LIGHT ON FAP
TMUCI2V02-P04 LEVEL 3
EFFECTIVITY 23-73-00 Page 9
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUCI2V02 LEVEL 3
EFFECTIVITY 23-73-00 Page 10
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23 - COMMUNICATIONS
23-73-00 CIDS - DIRECTOR INTERFACES
CONTENTS:
Director Interfaces
TMUCI2W03 LEVEL 3
EFFECTIVITY 23-73-00 Page 1
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CIDS - DIRECTOR INTERFACES
Here is the list of interfaces described in this
module.
DIRECTOR INTERFACES
- Centralized Fault Display Interface Unit
- System Data Acquisition Concentrator
- Audio Management Unit
- Cockpit Handset
- Service Interphone Boomsets
- Calls Panel
- Signs Panel
- Oil Low Pressure Relay (12KS1)
- Landing Gear Control And Interface Units
- Slat Flap Control Computers
- Flight Warning Computer
- Service Interphone Override Pushbutton
- Forward Attendant Panel
- Programming and Test Panel (PTP)
- Directors
- Cockpit Door Switch
- Evac Panel
- Evac Horn
- Cabin Pressure Relay (19WR)
- Excessive Altitude Pressure Switches
- Smoke Detection Control Unit
- Audio Reproducer (PES)
- Video System Control Unit
- Prerecorded Announcement Module (PRAM)
- Passenger Entertainment And Passenger Service
System
- DEU B
- DEU A
- Top Line Cut-Off Relay (106RH)
- Pin Programming
- PES ON/OFF Relay (800MK)
- Relay Board Ann Light Test and Interface
- Exit Signs Relay (8WL)
NOTE: The CIDS Directors 1 and 2 have the same
interfaces and the same computations. The
outputs of the Director in stand-by mode are
disabled, except the BITE test which can be
carried out by the CFDIU.
TMUCI2W03-T01 LEVEL 3
EFFECTIVITY 23-73-00 Page 2
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MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
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CIDS - DIRECTOR INTERFACES
TMUCI2W03-P01 LEVEL 3
EFFECTIVITY 23-73-00 Page 3
Apr 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
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