
TAILLIGHT
SYSTEM OUTLINE
WHEN THE LIGHT CONTROL SW IS TURNED TO TAIL OR HEAD POSITION. THE CURRENT FLOWS TO TERMINAL 3 OF THE LIGHT FAILURE SENSOR THROUGH THE TAIL FUSE.
WHEN THE IGNITION SW IS TURNED ON, THE CURRENT FLOWS FROM THE GAUGE FUSE TO TERMINAL 8 OF THE LIGHT FAILURE SENSOR, ANO ALSO FLOWS THROUGH THE REAR LIGHT WARNING LIGHT TO TERMINAL 4 OF THE LIGHT FAILURE SENSOR.
TAILLIGHT DISCONNECTION WARNING
WITH THE IGNITION SW ON AND THE LIGHT CONTROL SW TURNED TO TAIL OR HEAD POSITION, IF THE TAILLIGHT CIRCUIT IS OPEN, THE LIGHT FAILURE SENSOR DETECTS THE FAILURE BY THE CHANGE IN CURRENT FLOWING FROM TERMINAL 3 OF THE LIGHT FAILURE SENSOR TO TERMINAL 9, AND THE WARNING CIRCUIT OF THE LIGHT FAILURE SENSOR IS ACTIVATED.
AS A RESULT, THE CURRENT FLOWS FROM TERMINAL 4 OF THE LIGHT FAILURE SENSOR → TERMINAL 11 → GROUND AND TURNS THE REAR LIGHT WARNING LIGHT ON, WHICH REMAINS ON UNTIL THE LIGHT CONTROL SW IS TURNED OFF.
SERVICE HINTS
TAILLIGHT RELAY
5–3: CLOSED WITH LIGHT CONTROL SW AT TAIL OR HEAD POSITION
L 2 LIGHT FAILURE SENSOR
4, 8–GROUND: APPROX. 12 VOLTS WITH IGNITION SW AT ON POSITION
3–GROUND: APPROX. 12 VOLTS WITH LIGHT CONTROL SW AT TAIL OR HEAD POSITION
11–GROUND: ALWAYS CONTINUOUS
: PARTS LOCATION
CODE | SEE PAGE | CODE | SEE PAGE | CODE | SEE PAGE
C13 | 28 | F 5 | 26 (2JZ–GE) | R 9 | 30
F 3 | 24 (2JZ–GTE) | F 6 | 24 (2JZ–GTE) | R10 | 30
F 3 | 26 (2JZ–GE) | F 6 | 26 (2JZ–GE) | R11 | 30
F 4 | 24 (2JZ–GTE) | I20 | 29 | R12 | 30
F 4 | 26 (2JZ–GE) | L 1 | 30 | T 6 | 29
F 5 | 24 (2JZ–GTE) | L 2 | 30 |
: RELAY BLOCKS
CODE | SEE PAGE | RELAY BLOCKS (RELAY BLOCK LOCATION)
2 | 22 | R/B NO. 2 (ENGINE COMPARTMENT LEFT)
: JUNCTION BLOCK AND WIRE HARNESS CONNECTOR
CODE | SEE PAGE | JUNCTION BLOCK AND WIRE HARNESS (CONNECTOR LOCATION)
1A | 20 | ENGINE ROOM MAIN WIRE AND J/B NO. 1 (LEFT KICK PANEL)
1B | 20 |
1C | 20 | FLOOR NO. 2 WIRE AND J/B NO. 1 (LEFT KICK PANEL)
1E | 20 | INSTRUMENT PANEL WIRE AND J/B NO. 1 (LEFT KICK PANEL)
1J | 20 | COWL WIRE AND J/B NO. 1 (LEFT KICK PANEL)
1K | 20 |
2A | 22 | BATTERY AND J/B NO. 2 (ENGINE COMPARTMENT LEFT)
: CONNECTOR JOINING WIRE HARNESS AND WIRE HARNESS
CODE | SEE PAGE | JOINING WIRE HARNESS AND WIRE HARNESS (CONNECTOR LOCATION)
IE1 | 36 | INSTRUMENT PANEL WIRE AND FLOOR NO. 2 WIRE (LEFT KICK PANEL)
: GROUND POINTS
CODE | SEE PAGE | GROUND POINTS LOCATION
EA | 32 (2JZ–GTE) | FRONT SIDE OF RIGHT FENDER
EA | 34 (2JZ–GE) |
EB | 32 (2JZ–GTE) | FRONT SIDE OF LEFT FENDER
EB | 34 (2JZ–GE) |
IE | 36 | LEFT KICK PANEL
BI | 40 | LEFT QUARTER PILLAR
BJ | 40 | LOWER BACK PANEL CENTER
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