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ZONE: 711
COMPONENT DESCRIPTION
The take-off light consists of a single filament lamp,
rated at 600 Watts, installed on the nose landing gear
in a fixed position.
TMULIGV06-T03 LEVEL 3
EFFECTIVITY 33-40-00 Page 6
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 106
ALL
EXTERIOR LIGHTS COMPONENTS - TAKE-OFF LIGHT
TMULIGV06-P03 LEVEL 3
EFFECTIVITY 33-40-00 Page 7
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 107
ALL
EXTERIOR LIGHTS - COMPONENTS
NAVIGATION LIGHTS
WING-TIP LIGHTS
IDENTIFICATION
FIN: 9LA, 10LA
LOCATION
ZONE: 534, 634
COMPONENT DESCRIPTION
Each wing-tip navigation light assembly contains two
light units which operate independently.
To get access to these lights, the respective glazing
panel must be removed.
TAIL LIGHT
IDENTIFICATION
FIN: 15LA
LOCATION
ZONE: 317
COMPONENT DESCRIPTION
The tail navigation light assembly contains two light
units which operate independently.
TAIL LIGHT TRANSFORMER
IDENTIFICATION
FIN: 13LA
LOCATION
ZONE: 317
COMPONENT DESCRIPTION
The tail navigation light transformer assembly
contains two step-down transformers, which operate
independently to supply their related light unit.
TMULIGV06-T04 LEVEL 3
EFFECTIVITY 33-40-00 Page 8
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 108
ALL
EXTERIOR LIGHTS COMPONENTS - NAVIGATION LIGHTS
TMULIGV06-P04 LEVEL 3
EFFECTIVITY 33-40-00 Page 9
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 109
ALL
EXTERIOR LIGHTS - COMPONENTS
WING AND ENGINE SCAN LIGHTS
IDENTIFICATION
FIN: 3LX, 4LX
LOCATION
ZONE: 231, 232
COMPONENT DESCRIPTION
The lights are installed one each side in the forward
fuselage of the aircraft.
An attached transformer gives the rated operation
voltage to each light unit.
TMULIGV06-T05 LEVEL 3
EFFECTIVITY 33-40-00 Page 10
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 110
ALL
EXTERIOR LIGHTS COMPONENTS - WING AND ENGINE SCAN LIGHTS
TMULIGV06-P05 LEVEL 3
EFFECTIVITY 33-40-00 Page 11
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 111
ALL
EXTERIOR LIGHTS - COMPONENTS
ANTI-COLLISION LIGHTS
LOWER BEACON LIGHT
IDENTIFICATION
FIN: 6LV
LOCATION
ZONE: 191
COMPONENT DESCRIPTION
The lower anti-collision light consists of a flash
tube mounted on a reflector. It is enclosed in a faraday
cage, and covered by a red glass.
UPPER BEACON LIGHT
IDENTIFICATION
FIN: 7LV
LOCATION
ZONE: 244
COMPONENT DESCRIPTION
The upper anti-collision light consists of a flash
tube mounted on a reflector. It is enclosed in a faraday
cage, and covered by a red glass.
BEACON POWER UNITS
IDENTIFICATION
FIN: 3LV, 4LV
LOCATION
ZONE: 244, 192
COMPONENT DESCRIPTION
The power unit supplies a high voltage frequency to
start and operate the anti-collision lights.
The upper power unit 3LV is the master synchronization
for alternating with the strober.
- WARNING: These units produce 400 to 500
Volts DC.
TMULIGV06-T06 LEVEL 3
EFFECTIVITY 33-40-00 Page 12
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 112
ALL
EXTERIOR LIGHTS COMPONENTS - ANTI-COLLISION LIGHTS
TMULIGV06-P06 LEVEL 3
EFFECTIVITY 33-40-00 Page 13
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 113
ALL
EXTERIOR LIGHTS - COMPONENTS
STROBE LIGHTS
WING-TIP STROBE LIGHTS
IDENTIFICATION
FIN: 16LV, 17LV
LOCATION
ZONE: 634, 534
COMPONENT DESCRIPTION
The wing-tip strobe lights consist of two tubes
enclosed in a metal case with a faraday cage in the
white lens.
TAIL STROBE LIGHT
IDENTIFICATION
FIN: 19LV
　
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