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EMERGENCY POWER SUPPLY UNITS
IDENTIFICATION
FIN :10WL, 11WL, 12WL, 13WL
LOCATION
ZONE :221, 242, 241, 263
COMPONENT DESCRIPTION
There are 4 Emergency Power Supply Units which consist
of :
- Electronic logic and switching circuits,
- A 28VDC/6VDC converter which supplies
electrical power,
- A 6VDC battery which supplies the loads in
abnormal configuration,
- A test circuit which tests the condition of
the battery unit, the logic unit and the related
loads.
ISOLATED EPSU TEST
An individual test on each EPSU must be performed when
the test from the PTP shows a fault on the emergency
lighting network.
This isolated test starts when the test pushbutton is
pushed.
A defective EPSU will cause a red LED to come on and
indicate which part is defective. The green SYSTEM OK
LED indicates a serviceable EPSU.
TMULIGQ05-T01 LEVEL 3
EFFECTIVITY 33-50-00 Page 2
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 196
ALL
EMERGENCY LIGHTS COMPONENTS - EMERGENCY POWER SUPPLY UNITS
TMULIGQ05-P01 LEVEL 3
EFFECTIVITY 33-50-00 Page 3
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 197
ALL
EMERGENCY LIGHTS - COMPONENTS ALTERNATE FLOOR MOUNTED "L.S.I." & "BRUCE" EEPMS
CABIN EMERGENCY LIGHTS
20WL, 21WL, 32WL, 33WL
IDENTIFICATION
FIN :20WL, 21WL, 32WL , 33WL
LOCATION
ZONE :222, 221, 262, 261
COMPONENT DESCRIPTION
There are 4 cabin emergency lights located in the
forward and the aft entrance areas above the passenger
doors. Each light consists of a housing and a lens,
containing two 6VDC lamps in parallel.
200WL thru 207WL
IDENTIFICATION
FIN :200WL thru 207WL
LOCATION
ZONE :230, 240, 250, 260
COMPONENT DESCRIPTION
There are 8 cabin emergency lights located in the cabin
ceiling panels. Each light consists of a housing and
a lens, containing two 6VDC lamps in parallel.
TMULIGQ05-T02 LEVEL 3
EFFECTIVITY 33-50-00 Page 4
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 198
ALL
EMERGENCY LIGHTS COMPONENTS - CABIN EMERGENCY LIGHTS
TMULIGQ05-P02 LEVEL 3
EFFECTIVITY 33-50-00 Page 5
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 199
ALL
EMERGENCY LIGHTS - COMPONENTS ALTERNATE FLOOR MOUNTED "L.S.I." & "BRUCE" EEPMS
EXIT MARKING SIGNS
IDENTIFICATION
FIN :40WL, 41WL, 42WL, 43WL, 44WL, 45WL
LOCATION
ZONE :220, 230, 250, 260
COMPONENT DESCRIPTION
There are 6 single-side exit marking signs :
- 40WL, 41WL, 44WL, 45WL for each passenger/crew
door,
- 42WL, 43WL for each emergency exit door side.
The exit lights consist of a plastic case housing, a
lens and a number of 6VDC lights connected in parallel.
TMULIGQ05-T03 LEVEL 3
EFFECTIVITY 33-50-00 Page 6
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 200
ALL
EMERGENCY LIGHTS COMPONENTS - EXIT MARKING SIGNS
TMULIGQ05-P03 LEVEL 3
EFFECTIVITY 33-50-00 Page 7
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 201
ALL
EMERGENCY LIGHTS - COMPONENTS ALTERNATE FLOOR MOUNTED "L.S.I." & "BRUCE" EEPMS
EXIT LOCATION SIGNS
IDENTIFICATION
FIN :50WL, 51WL, 52WL, 53WL
LOCATION
ZONE :221, 241, 261
COMPONENT DESCRIPTION
There are 2 single-side exit location signs :
- 50WL, 52WL for each passenger/crew door,
and 2 double-side exit location signs :
- 51WL, 53WL for emergency exit doors.
The exit lights consist of a plastic case housing, a
lens and a number of 6VDC lights connected in parallel.
TMULIGQ05-T04 LEVEL 3
EFFECTIVITY 33-50-00 Page 8
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
UF94200
EFFECTIVITY Page 202
ALL
EMERGENCY LIGHTS COMPONENTS - EXIT LOCATION SIGNS
TMULIGQ05-P04 LEVEL 3
EFFECTIVITY 33-50-00 Page 9
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 33 LIGHTS
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