charging DATSUN PICK-UP 1977 Service Manual

The
non
California

type
operates
as

follows

secondary
air
is
sucked

through
the
air

pump
air

cleaner
into

the
air

pump
driven

by
the
crank

pulley
It
is

then

discharged
through

the

check

valve
to

the
air

gallety
where

it
is

distributed
to
each

exhaust

porL

The

secondary
air
is
then

injected

from
the

injection
nozzle

into
the

exhaust

port
near
the
exhaust
valve

The
air
relief
valve

opens
only
when

the

discharge
pressure
of
the
air

pump

surpasses
the

spring
force
of
the
air

relief
valve

during
high
speed
opera

tion

When
the
air

relief
valve

opens

the

secondary
air
is

discharged
in
to

the

carburetor
air
c1eaner

The
anti

backfire
valve

opens
when

the
intake
manifold
vacuum

reaches
a

predetermined
value

during
decelera

tion

and

permits
fresh
air
to
now
into

the
intake

manifold
from
the
air

cleaner

f

I

Jl

rn
l

I
Air

pump

2
Air

pump
air

cleaner

3

Emergency
air

relief
valve

4

Air

relief
valve
riu

Qj

j

I

@
Emission
Control

System

To
intake

manifold

The
California

type
includes
in

addition
to
the

components
of
the

non
California

type
an

air

control

valve

and
an

emergency
air
relief
valve

The
air

control
valve

opens
when

the
sum
of
the
air

pump

discharge

pressure
and

the
intake

manifold
vacu

um

applied
to
the

diaphmgm
reaches
a

predetermined
level
and

discharges

the

secondary
air
into
the

air
cleaner

When
the

pressure
becomes
low
the

valve
doses

with
the

spring
force
of

3

5
Air

cleaner

6

Check
valve

7

Air

gallery

pipe

8

Carburetor

EC

13
To

intake

manifold

Air

diSlcharge
to

intake
manifold

Secondary

air

EC297

Fig
EC

23

Operation

of
A

B
lve

the
air
control
valve

and

stops
dis

charging
the

secondary
air

F
igure

EC

25

When
the

intake
manifold

vacuum

applied
to
the

diaphragm
reaches

a

predetermined
level
E
A

R
valve

operates
to

discharge
the

secondary
air

into
the

atmosphere
When
the

pres

sure

becomes

high
the
valve

closes

by

spring
tension
of
E
A
R
valve

and

stops

discharging
the

secondary
air

fl

t

9
Air
control
valve

10

Injection
nozzle

II
Exha
l
t

manifold

12
Anti
backfire
valve

EC780

Fig
EC
24

California

type
A
I

S

DATSUN
PICK

UP

MODEL
620

SERIES

I
NISSAN

I

NISSAN
MOTOR

CO
LTD

TOKYO
JAPAN
SECTION

EE

ENGINE

ELECTRICAL

SYSTEM

BATTERY

EE
2

STARTING

MOTOR
EE

4

CHARGING

CIRCUIT
EE

12

ALTERNATOR
EE
15

REGULATOR

EE
20

IGNITION

CIRCUIT
EE

26

DISTRIBUTOR

EE

30

Non

California

models

DISTRIBUTOR
California
models
EE

33

TRANSISTOR
IGNITION
UNIT

California
models

IGNITION
COIL

SPARK
PLUG
EE
36

EE

46

EE
47

REMOVAL

CHECKING
ELECTROLYTE
LEVEL

CHECKING
SPECIFIC
GRAVITY

REMOVAL

I
Disconnect

negative
and

positive

cables

2
Remove

nuts
from

battery

clamps
take
off

clamps

3
Remove

battery

CHECKING

ELECTROLYTE
LEVEL

Remove
six

vent

plugs
and
check

for

electrolyte
level
in
each
cell

If

nccessaJ

pour
distilled
water

CHECKING

SPECIFIC

GRAVITY

Specific
gravity
of

battery
electro

lyte
is
tested

by
a

hydrometer
If
the

srate

of

charge
of

battery
is

60
or

specific
gravity

reading
is
below
1
20

as
corrected
at
200e
680F
bat

tery
must
be

recharged
or

battery

electrolyte
concentration

adjusted

Add
or
subtract

gravity
points

according
to
whether
the

electrolyte

temperature
is
above

or
below
200e

680F

standard

The

gravity
of

electrolyte
chlll

ges

0

0007
for

every
Ioe
1
80F
tem

petature
A
correction

can
then
be

made

by
using
the

following
formula
Engine
Electrical

System

BATTERY

CONTENTS

EE
2

EE
2

EE
2
BATTERY
FREEZING

CHARGING

INST
ALLA
TION

S

20
St
0

0007
t
20

Where

St

Specific
gravity
of

electrolyte

at
tOe

520

Specific
gravity
of

electrolyte

corrected
at
200e
680F

t

Electrolyte

temperature

For

example
A

hydrometer

reading
of

1
260
at
300e

860F

would

be
1
267
corrected

to
200e

6goF

indicating
fully
charged

battery
On
the
other
hand
a

hydro

meter

reading
of
1
220
at
lOoe

140
F
would
be
1
199
corrected
to

200e
680F

indicating
a

partially

charged
battery

The
state
of

charge
of

battery
can

be
determined

by
the

following
table

if

the

specific
gravity
of

electrolyte
is

known
BefOIe

checking
be
sure
that

cells
are
filled
to
correct
level

G
U

o

N

b
t

E

u

ol

1
lilt

I
i
I

m
J

I
I

I
I

J
1
I

J
Sf
to
7
1
II

It
100

0wJIztI
COJJditioD

EE002

Fig
EE
2

ChaJ
ffing
condition

EE
2
1
28

@

126

S

Sow

E

l

l

u

o

o

l

e

u

0

U21

1

101
EE

3

EE

3

EE
3

Read

top
level

with
scale

1
Thermal

gauge

2

Hydrometer
feOOl

Fig
EE

l

Checking
pccme
gravity

Converted

specific
gavity

20

1
Je

I

dOldlOiJ
OSQ

Electrolyte
temperature
oC

EEOO3

Fig
EE
3

Specific
lNWity
at

eiectroly
te
temperature

BATTERY
FREEZING

Battery
electrolyte
freezing
point

varies
with
acid
concentration
or
its

specific
gravity
A

battery
with
an

insufficient

charge
will
freeze
at
lower

temperatures
If

specific
gravity
of
a

battery
falls
below
1
1
this
is

an

0

10

20

30

g

40
I
u

il

SO
I
0

e

60
0

E

70
Engine
Electrical

System

indication
that

battery
is

completely

discharged
and
will

freeze

readily

when

temperatures
fall
below

freezing

Note
Use
extreme
caution
to
avoid

freezing
battery
since

freezing
will

generally
ruin
the

battery

1

80

1
00
1
04
1
08
t
l2
1
16
t
20
1
24
1
28

Specific
gravity
of

electrolyte

CHARGING

I

f
electrolyte
level
is

satisfactory

battery
must
be

charged
when
electro

lyte
gravity
reading
falls
below
1
20
If

battery
on

car
is

quick
charged
to
1
32

EEOQ4

Fig
EE

4
Froezing
point
of
electrolyte

bring
it

up
to
full

charge
the

opera

tion
should
be
carried
out

with
nega

tive
cable
removed

Prior

to
charging
corroded
termi

EE
3
nals
should
be

cleaned
with
a

brush

and
common

baking
soda
solution
In

addition
the

following
items

should

be
observed
while

battery
is

being

charged

I
Be

sure
that
electrolyte
level
is

above

top
of

each
plate

2

Keep
removed

plugs
in

a
safe

place

3
Do

not
allow

electrolyte
tempera

ture
to

go
over
450C
I130F

4

After

charging
check
to
be
cer

tain
that

specific
gravity
does
not

exceed
1
260
at
200C
680P
Cor

rection
can
be
made

by
adding
dis

tilled
water
into

cells
as

necessary

5

Keep
battery
away
from

open

flame
while
it
is

being
charged

6
After
all
vent

plugs
have
been

tightened
clean
all

sprayed
electrolyte

off

upper
face

of

battery

INSTALLATION

1
Install
and

tighten
clamps
secure

Iy

2
After

clamps
have
been

tightened

clean

battery
cable
terminals
and

apply
grease
to
retard
formation
of

corrosion

Condition
Engine
Electrical

System

Probable
cause

Starting
motor

cranks

slowly
Dirty
or
worn
commutator

Armature
rubs

field
coil

Damaged
solenoid
switch

Starting
motor

operates
but
does

not
crank

engine
Worn

pinion

Locked

pinion
guide

Worn

ring

gear

Starting
motor
will

not

disengage
even
if

ignition
switch
is

turned
off
Damaged
solenoid
switch

Damaged

gear
teeth

The

charging
circuit
consists

of
the

battery
alternator

regulator
and

necessary

wiring
to
connect
these

parts
The

purpose
of
this

system
is
to

convert
mechanical

energy
from
the

engine
into

electrical

energy
which

is

used
to

operate
all

electrically

operat

ed
units

and
to

keep
the

battery
fully

charged

When
the

ignition
switch
is

set
to

ON
current
flows
from
the

battery

to

ground
through
the

ignition
switch

voltage
regulator
IG
terminal

primary

side
contact

point
PI

movable

contact

point
P2

voltage

regulator

IF

terminal
alternator
IF
terminal

rotor

field
coil
and
alternator

E

terminal

as
shown
in

Figure
EE

23

by

full
line

arrow
marks
Then
the

rotor

in

the

alternator
is
excited

On
the

other
hand

current
flows

from
the

battery
to

ground

through
the

ignition

switch

warning

lamp
voltage
regula

tor
L

terminal

lamp
side
contact

point
P4

movable

contact

point

P5
and

voltage
regulator
E
termi

nal
as
shown

by
dotted

line
arrow
CHARGING
CIRCUIT

marks
Then

the

warning
lamp
lights

When
the
alternator

begins
to

op

erate
three

phase

alternating
current
is

induced
in

the

stator
armature
coil

This

alternating
current
is
rectified

by

the

positive
and

negative
silicon

diodes
The
rectified

direct
current

output
reaches
the
alternator
A

and

E

terminals

On
the
other
hand
the
neutral

point
voltage
reaches
N
and
E

terminals

nearly
a
half
of

the

output

voltage
and
current
flows
from

voltage
regulator
N
terminal
to
E

terminal
or

ground
through
the
coil

VCI
as
shown
in

Figure
EE
24

by

the
dotted
line
arrow
marks
Then
the

coil
VCI
is
excited
and
the

movable
contact

point
IPS
comes

into
contact
with

voltage
winding
side

contact

point
P6
This
action
causes

to
turn
off

the

warning
lamp
and

complete
the

voltage
winding
circuit

as
shown

by
the
full

line
arrow
marks

When
the
alternator

speed
is
in

creased
or
the

voltage
starts
to
rise

excessively
the
movable
contact

point

EE
12
Corrective
action

Clean
and

repair

Replace
assembly

Repair
or

replace

Replace

Repair

Replace

Repair
or

replace

Replace
damaged

gear

P2
is

separated
from

the

primary

side
contact
PI

by
the

magnetic

force

of
coil
VC2
Therefore

registor
RI
is

applied
into
the
rotor

circuit

and

output
voltage
is
decreased

AJ

the

output
voltage
is
decreased

the

movable
contact

point
P2
and

primary
side
contact
Pin

comes
into

contact
once

again
and

the
alternator

voltage
increases

Thus
the

rapid

vibration
of
the
movable

contact

point

IPl

maintains
an
alternator

output

voltage
constant

When
the
alternator

speed
is

further

increased
or
the

voltage
starts
to
rise

excessively
the

movable
contact

point

P2
comes

into
contact
with

secondllJ
side
contact

point
P3

Then
the
rotor
current
is

shut
off
and

alternator

output
voltage
is

decreased

immediately
This

action
causes

movable
contact
n
to

separate

from

secondary
contact
P3
Thus

the

rapid
vibration
of

the
movable

contact

point
P2

or

breaking
and

completing
the

rotor
circuit
maintains

an
alternator

output
voltage
constant

Engine
Electrical

System

r
l

I

I

I

i

r
Ye
Ff
p

Stator
ma

ture
coiJ

FF
vw

I

I
RI

L

Rot
r

field
C
oil

e
R

I

I

I
I

I

J

1
J

Alternator

Voltage
regulator
11

t

c

I

Fusible
link

t
8

c

J
5

9

i
c
c

0

Battery

t
u
J

EE029

Fig
EE
23

Charging
circuit

II

p
ns

1

Slator
ar

ature
coil

teJ

U

2iI
I

r
R
l
I

I

A3

R2
0
Fusible
link

Roto
field
coil

e

I
I
t
I

I
PS

M
g

j

t

i

H
U

Battery

Lh

A

l
a
o
J

L

V

It

g
t

f

EE030

Fig
EE

24

Charging
circuit
II

EE

13

Engine
Electrical

System

B

v

W

WR

WL

L2
VOLTAGE
REGULATOR

co

LW

I
P
B

r

FUSIBLE
LINK

m
I
WLI

LW

cJ

I

B

t
EARTH
POINT
m
WR
WR

CHARGE

g
00
WARNING
lAMP

00000

Equipped
with

cooler
I
I
I
I

TjT
m

CLB

W

WB
B
YWR

I
I
I
I

1
W

B

rn

ALTERNATOR
I

l
LW
BW

j
J

M
IG
I

W

BwtIl

IGNITION
SWITCH

COLOR
CODE

B
Black

OW
Black
with

white

stripe

W
White

WB
White
with
black

stripe

WR
White
with
red

stripe

WL
White
with
blue

stripe

LO

Blue
with

black

stripe

LW
Blue
with
white

stripe

Y
Yellow
lOA

C
o
0
0
0

o
0
0
FUSE

BLOCK

M
0
0
0

lOA

Ii

California
models

E
E492

Fig
EE
25
Circuit

diagram
of
charging
lfY
t

m

EE
14

DESCRIPTION

REMOVAL

DISASSEMBLY

INSPECTION
AND
REPAIR

ROTOR
INSPECTION

INSPECTION
OF

STATOR

DESCRIPTION

In
the
alternator
a

magnetic
field
is

produced
by
the
rotor
which
consists

of
alternator
shaft
field
coil

pole

pieces
and

slip
rings
The

slip
rings

pressed
in
the
shaft
conduct

only
a

small
field
current

Output
current
is

generated
in
the
armature
coils
located

in

the
stator
The
stator
has
three

windings
and

generates
three

phase

alternating
current
Silicon
diodes
act

@God

A
tfff
Engine
Electrical

System

ALTERNATOR

CONTENTS

EE
15

EE
16

EE
16

EE
16

EE
17

EE
17
INSPECTION
OF
DIODE

INSPECTION
OF
BRUSH

SPRING
PRESSURE
TEST

ASSEMBL
Y

ALTERNATOR
TEST

SERVICE
DATA
AND
SPECIFICATIONS
EE
17

EE
1B

EE1B

EE

1B

EE19

EE
19

like
a
one

way
valve
for

electricity
so

that

charging
current

passes
easily
but

reverse
current
is
shut
out

In
this
alternator

pack
type
silicon

di
odes

are
used

Six

diodes
three

negative
and
three

positive
are
installed
in

positive
and

negative
plates
as
an

assembly

These
diodes
are
direct
soldered
at

their

tips
and
constructed
with

posi

3

2

I
4

e

o

e

9
tive
and

negative
conjunction

They
are
mounted
on
the
two

plates
which

combine
the
function
of

heat

dissipating
plate
and

positive

negative
terminals
and
are

light
in

weight
and

easy
to
service

The

pulley
mounted
on
the
air

conditioner
models
is

different
from

that
on
the

standard
models
without

air
conditioner

1

Pulley
usem

bly

2
Front
cover

3
Front

bearing

4

Rotor

5

Rear

bearing

6
Stator

7
Brush
assembly

8
Rear
cover

9

Diode
set

plate
assembly

10
Diode
cover

11

Through
botrs

EE
15
EE345

Fig
EE
26

Exploded
view

DESCRIPTION

MEASUREMENT
OF
REGULATOR

VOLTAGE

ADJUSTMENT

VOLTAGE
REGULATOR

DESCRIPTION

The

regulator
consists

basically
of

a

voltage
regulator
and
a

charge

relay

The
voltage

regulator
has
two
sets
of

contact

points
a
lower
set

and
an

upper
set
to
control
alternator
volt

age
An
armature

plate
placed
between

the
two
sets
of
contacts
moves

upward

or
downward
or
vibrates
The
lower

contacts
when
closed

complete
the

jCV
ID@
@

GJ
I

@

@

@
Engine
Electrical

System

REGULATOR

CONTENTS

EE
20
CHARGING
RELAY

SERVICE

DATA
AND

SPECIFICATIONS

TROUBLE
DIAGNOSES
AND

CORRECTIONS

Including
alternatorl

EE
25
EE
23

EE
24

EE

20

EE

23

EE
23

field
circuit
direct
to

ground
and
the

upper
contacts
when
closed

complete

the
field

circuit
to
ground

through
a

resistance
field
coil
and

produce

alternator

output

The

charge
relay
i
similar
in

construction

to
the

voltage
regulator

When
the

upper
contacts
are
closed

charge
warning
lamp
goes
on
v

1

Charge
relay

2

Voltage
regulator

EE285

Fig
EE
46
View

of
removing
cover

As

regards
the
construction
the

voltage
regulator
is

very
similar
to
the

charge
relay
as
shown
in

Figure
EE47

@

r

J
CD

@

@

@
Q
@
ID@

ID@

J
t

L

T

@
r

b
r
CD

L
@

j
1

g

f

@

@
EEJ97

J
I1Jlccting
spring

2
Y
kt

g
p

3
Armaturc

4
Core

go

5
Low

Sllccd
lnlacl

h
Point

ap

7

High
speed
conlat
t

8
Contact
c
9

3111111
0
118
ill

di

10

41l1I11W
157in
c1ia
few

II

Cuil

12

lock
nut

J3

Adjllslin
screw

14

Adjll
sting
sprin

15
Yoke
9

Adjusting
screw

10
Lock

nut

11
Coil

12
4mm

0
157
in

dia
screw

13
3mm
0
118
in

dla
crew

14
Contact

iet

15

Voltage

cgulatm
contact

a

Cnl1
Tlll
tion
f

lltagl
l

j
llIOltllT
I
Point

gilp

2

Charge
relay
contllct

3
Core

gap

4

ArlllatlJre

5

Connecting

sprin

6
Yoke

gap

7
Yoh

B

Adjusting
pring

b

Construction
of

charge
relay

Fig
EE
47
Structural
vi
w

EE
20

Engine
Electrical

System

RegulatoI

r
Yellow
terminal

A
W
L
WR

IG
WL

N

Y
E
B
F
WB
Voltmeter

Fig
EE

52
Tuting

charging
re
Qy
EE348

SERVICE
DATA
AND
SPECIFICATIONS

Voltage
legulator

Type

Regulating
voltage
with

fully

charged
battery

Voltage
coil

resistance

RotOI
coil

inserting
resistance

Voltage
coil

series
resistance

Smoothing
resistance

COle

gap

Point

gap

Ch
uge
lay

Release

voltage

Voltage
coil

resistance

Core

gap

Point

gap
v

fl

nun
in

nun
in

V

fl

nun
in

mID
in
TLl

Z
S5C

14
3
to
15
3
at

200C
680F

10
5
at
200C
680F

10

31

40

0
6
to
1
0
0
024
to
0
039

0
35
to
0
45

0
014
to
O

OIS

4
2
to
5

2
at
N
terminal

37
S
at
200C
680F

0
8

to
1
0
0
031
to
0
039

0
4
to
0
6
0
016
to
0
024

Standard

tempelatUIe
gIlIdient
O
OISV
oC

EE
24