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The BSU receives commands from the SDU and converts
them in order to control an electronic antenna to point
its beam at the satellite.
BITE
The SDU is interfaced with the CFDIU for BITE purposes
via an ARINC 429 bus.
The HPA and BSU can be tested through the SDU via ARINC
429 buses. They also provide HGA and D/LNA status.
TMU23SD02-T01 LEVEL 3
EFFECTIVITY 23-28-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 142
ALL
23 - COMMUNICATIONS
23-28-00 COLLINS MCS SATCOM COMPONENTS
CONTENTS:
Satellite Data Unit
High Power Amplifier
Diplexer/low Noise Amplifier
Beam Steering Unit
High Gain Antenna
TMU23SE01 LEVEL 3
EFFECTIVITY 23-28-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 143
ALL
COLLINS MCS SATCOM COMPONENTS
SATELLITE DATA UNIT
IDENTIFICATION
FIN: 5RV1
LOCATION
ZONE: 160
COMPONENT DESCRIPTION
A plug is provided on the front face of the SDU for
in situ data loading.
TMU23SE01-T01 LEVEL 3
EFFECTIVITY 23-28-00 Page 2
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UF94200
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TMU23SE01-P01 LEVEL 3
COLLINS MCS SATCOM COMPONENTS - SATELLITE DATA UNIT
EFFECTIVITY 23-28-00 Page 3
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 145
ALL
COLLINS MCS SATCOM COMPONENTS
HIGH POWER AMPLIFIER
IDENTIFICATION
FIN: 7RV1
LOCATION
ZONE: 160
TMU23SE01-T02 LEVEL 3
EFFECTIVITY 23-28-00 Page 4
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 146
ALL
COLLINS MCS SATCOM COMPONENTS - HIGH POWER AMPLIFIER
TMU23SE01-P02 LEVEL 3
EFFECTIVITY 23-28-00 Page 5
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 147
ALL
COLLINS MCS SATCOM COMPONENTS
DIPLEXER/LOW NOISE AMPLIFIER
IDENTIFICATION
FIN: 19RV1
LOCATION
ZONE: 250
COMPONENT DESCRIPTION
The D/LNA features:
on the front side:
- a J1 connector for connection with the SDU,
- a J2 connector for connection with the BSU,
- a J3 connector for connection with the High
Power Amplifier.
on the back side:
- a J4 connector for connection with the BSU.
TMU23SE01-T03 LEVEL 3
EFFECTIVITY 23-28-00 Page 6
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 148
ALL
COLLINS MCS SATCOM COMPONENTS - DIPLEXER/LOW NOISE AMPLIFIER
TMU23SE01-P03 LEVEL 3
EFFECTIVITY 23-28-00 Page 7
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 149
ALL
COLLINS MCS SATCOM COMPONENTS
BEAM STEERING UNIT
IDENTIFICATION
FIN: 8RV1
LOCATION
ZONE: 160
COMPONENT DESCRIPTION
This BSU can be provided for a top mounted antenna
management.
The BSU front face features four red LEDs and one green
LED to indicate, while in either operational or
diagnostic mode, a failure in the operational integrity
of the BSU power status.
LEDs will remain on until corrective action is
performed.
TMU23SE01-T04 LEVEL 3
EFFECTIVITY 23-28-00 Page 8
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 150
ALL
COLLINS MCS SATCOM COMPONENTS - BEAM STEERING UNIT
TMU23SE01-P04 LEVEL 3
EFFECTIVITY 23-28-00 Page 9
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 151
ALL
COLLINS MCS SATCOM COMPONENTS
HIGH GAIN ANTENNA
IDENTIFICATION
FIN: 16RV
LOCATION
ZONE: 250
COMPONENT DESCRIPTION
The top mounted High Gain Antenna is mounted with an
adapter plate on the fuselage. It is equipped with a
J1 connector for connection with the BSU and a J2
　
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