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TCAS COMPONENTS
TCAS ANTENNAE
IDENTIFICATION
FIN: 7SG1, 7SG2
LOCATION
ZONE: 230, 130
COMPONENT DESCRIPTION
The TCAS directional antennae are composed of four
passive and independent vertically-polarized
elements.
A teflon gasket is located between the fuselage and
the base of the antenna in order to facilitate the
removal of the antenna.
TMUTCAN05-T04 LEVEL 3
EFFECTIVITY 34-43-00 Page 8
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 324
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TCAS COMPONENTS - ANTENNAE
TMUTCAN05-P04 LEVEL 3
EFFECTIVITY 34-43-00 Page 9
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 325
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TCAS COMPONENTS
TCAS CONTROL PANEL (COLLINS)
IDENTIFICATION
FIN: 3SH
LOCATION
ZONE: 211
COMPONENT DESCRIPTION
The processor of the TCAS/ATC control panel controls
the ATC and TCAS function via an ARINC 429 bus.
TMUTCAN05-T05 LEVEL 3
EFFECTIVITY 34-43-00 Page 10
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 326
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TCAS COMPONENTS - CONTROL PANEL (COLLINS)
TMUTCAN05-P05 LEVEL 3
EFFECTIVITY 34-43-00 Page 11
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 327
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TCAS COMPONENTS
TCAS CONTROL PANEL (SEXTANT)
IDENTIFICATION
FIN: 3SH
LOCATION
ZONE: 211
COMPONENT DESCRIPTION
The processor of the TCAS/ATC control panel controls
the ATC and TCAS function via an ARINC 429 bus.
TMUTCAN05-T06 LEVEL 3
EFFECTIVITY 34-43-00 Page 12
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 328
ALL
TCAS COMPONENTS - CONTROL PANEL (SEXTANT)
TMUTCAN05-P06 LEVEL 3
EFFECTIVITY 34-43-00 Page 13
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 329
ALL
TCAS COMPONENTS
TCAS CONTROL PANEL (BENDIX)
IDENTIFICATION
FIN: 3SH
LOCATION
ZONE: 211
COMPONENT DESCRIPTION
The processor of the TCAS/ATC control panel controls
the ATC and TCAS function via an ARINC 429 bus.
TMUTCAN05-T07 LEVEL 3
EFFECTIVITY 34-43-00 Page 14
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 330
ALL
TCAS COMPONENTS - CONTROL PANEL (BENDIX)
TMUTCAN05-P07 LEVEL 3
EFFECTIVITY 34-43-00 Page 15
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 331
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THIS PAGE LEFT INTENTIONALLY BLANK.
TMUTCAN05 LEVEL 3
EFFECTIVITY 34-43-00 Page 16
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
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EFFECTIVITY Page 332
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34 - NAVIGATION
34-48-00 ENHANCED GROUND PROXIMITY
WARNING SYSTEM PRESENTATION
CONTENTS:
General
Principle
Components
Indicating
TMUEGPA01 LEVEL 1
EFFECTIVITY 34-48-00 Page 1
Feb 28/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 333
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ENHANCED GROUND PROXIMITY WARNING SYSTEM PRESENTATION
GENERAL
The Enhanced Ground Proximity Warning System (EGPWS)
is built over the current GPWS.
- EGPWS = GPWS + "ENHANCED" functions.
PRINCIPLE
The purpose of the Enhanced Ground Proximity Warning
System (EGPWS) is to help prevent accidents caused by
Controlled Flight Into Terrain (CFIT).
When boundaries of any alerting envelope are exceeded;
aural alert messages, visual annunciations and
displays are generated.
The basic GPWS modes generate aural and visual warnings
corresponding to an aircraft behaviour when the alert
envelope is penetrated.
The "ENHANCED" features complete the basic GPWS modes:
- Terrain Clearance Floor (TCF): Increase the
terrain clearance envelope around the airport
runway.
- Terrain Awareness alerting and Display (TAD):
　
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