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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.
TMU23SB02-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 126
ALL
23 - COMMUNICATIONS
23-28-00 HONEYWELL MCS SATCOM COMPONENTS
CONTENTS:
Satellite Data Unit
High Power Amplifier
Diplexer/low Noise Amplifier
Beam Steering Unit
High Gain Antenna
TMU23SC01 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 127
ALL
HONEYWELL MCS SATCOM COMPONENTS
SATELLITE DATA UNIT
IDENTIFICATION
FIN: 5RV1
LOCATION
ZONE: 160
COMPONENT DESCRIPTION
The face of the SDU features:
- two red SDU FAIL and SYSTEM LRU FAIL Light
Emitting Diodes (LEDs),
- a 20-character display capable of displaying
alpha-numeric characters,
- two momentary action pushbutton switches:
- SDU TEST for SDU testing; the result is
displayed on the LEDs,
- CM/SCROLL for alpha-numerical display
scrolling,
- a plug for in situ data loading.
TMU23SC01-T01 LEVEL 3
EFFECTIVITY 23-28-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 128
ALL
TMU23SC01-P01 LEVEL 3
HONEYWELL 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 129
ALL
HONEYWELL MCS SATCOM COMPONENTS
HIGH POWER AMPLIFIER
IDENTIFICATION
FIN: 7RV1
LOCATION
ZONE: 160
COMPONENT DESCRIPTION
The face of the HPA features:
- a PUSH TO TEST pushbutton switch,
- a red FAIL LED,
- a green PASS LED,
- a plug for in situ data loading.
TMU23SC01-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 130
ALL
HONEYWELL MCS SATCOM COMPONENTS - HIGH POWER AMPLIFIER
TMU23SC01-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 131
ALL
HONEYWELL 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.
TMU23SC01-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 132
ALL
HONEYWELL MCS SATCOM COMPONENTS - DIPLEXER/LOW NOISE AMPLIFIER
TMU23SC01-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 133
ALL
HONEYWELL 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.
TMU23SC01-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 134
ALL
HONEYWELL MCS SATCOM COMPONENTS - BEAM STEERING UNIT
TMU23SC01-P04 LEVEL 3
EFFECTIVITY 23-28-00 Page 9
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
　
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