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MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 493
ALL
VOR INDICATIONS ON ND
FAILURES
CONDITIONS OF DISPLAY
Depending on the mode selected on the EFIS control
panel, red flags are displayed.
TMUVORB01-T04 LEVEL 2
EFFECTIVITY 34-55-00 Page 8
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 494
ALL
VOR INDICATIONS ON ND
TMUVORB01-P04 LEVEL 2
EFFECTIVITY 34-55-00 Page 9
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 495
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SELF EXAMINATION
In which ND mode is the VOR course deviation
information displayed ?
A - In ROSE-VOR mode.
B - In ROSE-NAV mode.
C - In any mode.
When is the "M" symbol displayed in the VOR
characteristics ?
A - When the VOR is tuned from the MCDU.
B - When the VOR is tuned from the RMP.
C - When a failure occurs.
TMUVORB01 LEVEL 2
EFFECTIVITY 34-55-00 Page 10
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 496
ALL
34 - NAVIGATION
34-55-00 VOR/MKR COMPONENTS
CONTENTS:
VOR/MKR Receiver (Collins)
VOR/MKR Receiver (Allied)
VOR Antenna
MKR Antenna
TMUVORE03 LEVEL 3
EFFECTIVITY 34-55-00 Page 1
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 497
ALL
VOR/MKR COMPONENTS
VOR/MKR RECEIVER (COLLINS)
IDENTIFICATION
FIN: 3RS1,3RS2
LOCATION
ZONE:127,128
COMPONENT DESCRIPTION
The face of the VOR/MKR Receiver is fitted with two
LEDs and a TEST pushbutton switch. When it is pressed
in, the functional test starts.
If no fault is detected during the test the green LRU
STATUS LED comes on.
The back is fitted with an ARINC 600 connector.
VOR/MKR RECEIVER (ALLIED)
IDENTIFICATION
FIN: 3RS1,3RS2
LOCATION
ZONE:127,128
COMPONENT DESCRIPTION
The face of the VOR/MKR Receiver is fitted with two
momentary pushbutton switches and a Liquid Cristal
Display (LCD).
The LCD provides user intefaces for test, fault display
and troubleshooting.
The front face is also fitted with an RS-232 connector
for interfacing with personal computers.
The back is fitted with an ARINC 600 connector.
TMUVORE03-T01 LEVEL 3
EFFECTIVITY 34-55-00 Page 2
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 498
ALL
VOR/MKR COMPONENTS - RECEIVERS
TMUVORE03-P01 LEVEL 3
EFFECTIVITY 34-55-00 Page 3
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 499
ALL
VOR/MKR COMPONENTS
VOR ANTENNA
IDENTIFICATION
FIN: 4RS
LOCATION
ZONE: 324
COMPONENT DESCRIPTION
The dual VOR antenna is located on the top of the tail.
It is a small-sized half-wave folded dipole type.
The antenna is horizontally polarized and has an
impedance of 50 ohms.
MKR ANTENNA
IDENTIFICATION
FIN: 1RS
LOCATION
ZONE: 133
COMPONENT DESCRIPTION
The dielectric, foam-filled, polyester fiberglass
housing, fitted with a metal leading edge, protects
against moisture and erosion.
The antenna is horizontally polarized and has an
impedance of 50 ohms.
TMUVORE03-T02 LEVEL 3
EFFECTIVITY 34-55-00 Page 4
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 500
ALL
TMUVORE03-P02 LEVEL 3
VOR/MKR COMPONENTS - ANTENNAE
EFFECTIVITY 34-55-00 Page 5
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
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EFFECTIVITY Page 501
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUVORE03 LEVEL 3
EFFECTIVITY 34-55-00 Page 6
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 34 NAVIGATION
UF94200
EFFECTIVITY Page 502
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34 - NAVIGATION
34-00-00 ECAM WARNINGS (EXCEPT ADIRS)
CONTENTS:
General
ILS Fault
PRED W/S Fault
RA Fault
　
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