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LOCATION
ZONE: 317
COMPONENT DESCRIPTION
The tail strobe light consists of a tube enclosed in
a metal case with a faraday cage in the white lens.
STROBE LIGHT POWER UNITS
IDENTIFICATION
FIN: 14LV, 15LV, 18LV
LOCATION
ZONE: 634, 534, 311
COMPONENT DESCRIPTION
The power unit supplies a high voltage frequency to
start and operate the strobe lights.
- WARNING: These units may cause injury to
personnel due to residual voltage.
TMULIGV06-T07 LEVEL 3
EFFECTIVITY 33-40-00 Page 14
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 114
ALL
EXTERIOR LIGHTS COMPONENTS - STROBE LIGHTS
TMULIGV06-P07 LEVEL 3
EFFECTIVITY 33-40-00 Page 15
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 115
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EXTERIOR LIGHTS - COMPONENTS
LOGO LIGHTS
IDENTIFICATION
FIN: 3LY, 4LY
LOCATION
ZONE: 334, 344
COMPONENT DESCRIPTION
The logo lights are installed in the upper surface of
the trimmable horizontal-stabilizer.
The logo lights are optional.
TMULIGV06-T08 LEVEL 3
EFFECTIVITY 33-40-00 Page 16
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 116
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EXTERIOR LIGHTS COMPONENTS - LOGO LIGHTS
TMULIGV06-P08 LEVEL 3
EFFECTIVITY 33-40-00 Page 17
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 117
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EXTERIOR LIGHTS - COMPONENTS
LANDING LIGHTS
IDENTIFICATION
FIN: 7LB, 8LB
LOCATION
ZONE: 571, 671
COMPONENT DESCRIPTION
The landing lights are installed in the underside of
the wings.Each light has it own extension/retraction
and illumination circuit.
LANDING LIGHT ADJUSTMENT
To adjust landing light extension, act on both
adjustment screws by the same amount in the same
direction, using a vernier protractor.
Note : To avoid motor damage, never exceed 90.5 degrees
extension.
TMULIGV06-T09 LEVEL 3
EFFECTIVITY 33-40-00 Page 18
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 118
ALL
EXTERIOR LIGHTS COMPONENTS - LANDING LIGHTS
TMULIGV06-P09 LEVEL 3
EFFECTIVITY 33-40-00 Page 19
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UF94200
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TMULIGV06 LEVEL 3
EFFECTIVITY 33-40-00 Page 20
Apr 30/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 120
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33 - LIGHTS
33-50-00 EMERGENCY LIGHTING - SYSTEM
PRESENTATION
CONTENTS:
General
Cabin Emergency Lights
Exit Signs
Floor Proximity Emergency Escape Path Marking
System(FPEEPMS)
Lavatory Auxiliary Light
Door Escape Slide Lights
Emergency Power Supply Unit(EPSU)
Controls
Quiz
TMULIG502 LEVEL 1
EFFECTIVITY 33-50-00 Page 1
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 121
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EMERGENCY LIGHTING - SYSTEM PRESENTATION
GENERAL
In case of failure of the Main Lighting System or
during Emergency conditions, the purpose of the
Emergency Lighting System is to provide the
illumination of:
- the Cabin and Exit Areas,
- the EXIT location and EXIT Marking Signs at
each of the Passenger/Crew doors and at the
Emergency Exit doors,
- the Floor Proximity Emergency Escape Path
Marking System (FPEEPMS),
- the Lavatory Auxiliary Light,
- the emergency Escape Hatch-handles
(A319/A320),
- the escape route over the wing (A319/A320),
- and the Door Escape Slides.
The Emergency Lighting System is controlled from the
cockpit by the Flight Crew by a three position switch
"EMER EXIT LT" located on the Overhead panel or from
the cabin by the Cabin Attendants by the "EMER"
pushbutton located on the Forward Attendant Panel
(FAP).
EMERGENCY POWER SUPPLIED UNITS (EPSUs) located in the
Cabin, allow the associated Emergency Lights to be
electrically supplied by the 28 VDC ESSential BUS, via
　
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