NISSAN ALMERA N15 1995 Service Manual

Page 821 of 1701

TROUBLEDIAGNOSIS FORDTC12
Mass AirFlow Sensor (MAFS) (Coni'd)

GA14DE, 16DEengine forEurope andIsrael, andGA15DE engine

W/R

rrh

;1

I I

! !t

I I
I I

~
.
EC-MAFS-01

MASS AIR
FLOW SENSOR

<lli)

W
JOINTCONNECTOR

-6

r~ B BB

ECM I..J
1

(ECCS •

Sg~GE~f
-!-
=

(IT)
ffi
ill)

G

~
QA+

lbj:n

G

<I>:

LHDmode 1s

@:
RHOmodels
@: ForEurope andIsrae 1

@:
Except@
_. Detectable line
for DTC
-: Non-detectable
line forDTC
~ B
~~ B B

~ &#34;:91

GND GND

-A -A

t

7.5A
RefertoEL-POWER.

[ill

W
i
L
<tl@(][)

0-<:0-
W!L~ W!L

<!>
W!L

d=
(EI0l)

I~I
CHID

/ JUNCTIONBOXNO.2
~RL (JOINTCONNECTORS)

&#39;T&#39; ~

0-<:0-
W/L
q---~
W!L

I
@)@

O-<li>-
W/L~ W/L~

4D-
W/L~ W/L
-<W-O

~cm .-
I

r-&#39;

W/L
W/L

It
~I
ECCS
~ RELAY

@

~~
WIG
W/R

I
i-t-O~

WIG
W/R W/R W/R

m~rr17n
riN9n

SSOFF VBVB CRTN

~1111~cm
3456 W

T.
@
2 1L

5
~1111~cm

4567B W
J&Lm

<IJg]])
GY
-~-@

ITIITITIITIII GY
Refer
tolast page
(Foldout page).

HEC030
EC-102

Page 822 of 1701

TROUBLEDIAGNOSIS FORDTC12
Mass AirFlow Sensor (MAFS) (Cont&#39;d)
GA 16DE engine models exceptforEurope andIsrael

EC-MAFS-02

Refer toEL-POWER.

(
&#34;

I&#39;
....
1

1 1
1 1
1 1
1 1
1

t
~!

1
1

I
I
I
I

JOINT

I
1

I
1
CONNECTOR

I I

em

I
I

~
....

.....--u1

~

,

1----


II

8 8 8

t...J
1

ffi
ill

-:
Detectable line
for DTC
-: Non-detectable
line forDTC
ECM (ECCS
CONTROL
MODULE)

em

MASS
AIR
FLOW SENSOR

rn>

I

W!R

rn
lbiJ~
OR W

OR W

1rf6il~
QA+ QA-

t

W!L

I

W!L

1$1
(~~1;

W!L

IEtJI
QHD

=r
CfID

W!L

I

T-,

W!L W!L

IT~I
ECCS

n
RELAY

U
(IT)

~~
WIG W!R

I

.
--_.

I

&#34;

WIG
W!RW!R

IFh~Wfl

SSOFF V8V8

~I
I
l!jj
CEID

45678 W
+

(IT)

2 1L

5
~rn>

ill]]]D
8R~em

UI.ill.I.ITIIII
GY
Refer
tolast page
(Foldout page).

HEC031
EC-103

Page 823 of 1701

TROUBLEDIAGNOSIS FOROTC12
Mass AirFlow Sensor (MAFS) (Conl&#39;d)
GA16DE forAustralia

EC-MAFS-01

t
-:
Detectable line
for DTC
-: Non-detectable
line forDTC

11

B 8 B

t...l
1

~ ~

ECM
(ECCSCONTROL
MODULE)

em

,

I.

JOINT

CONNECTOR-6

@

--.~=-
-=~I--&#34;&#34;

OR W

II}; 1
14-81

QA+ QA-

(

I&#39;

I
I

I

I

I
I

I

I

I

1

I
I
I

I

I ...

r
,
W/R

W
3 MASS

AIR

FLOW

SENSOR

4=!Ilbj:Jlrn>
OR W

Refer
toEL-POWER.
W/L
I

W
/L
tETt&#39;i7\
r=b~

I~I@)

W/L

11iJ,@
=r@
W/L

I

T.

W/L W/L

I~~I
ECCS
~ RELAY

~U:jJJ@
WIG W/R

I

.--_
...

I

&#34;

WIG
W/R W/R

mlf5&#39;sil~

SSOFF VBVB

~I
11[iJ
@

3456 W~~
~BR
~@

IIIIlII.IIIITJ
GY
Refer
tolast page

(Foldout page).

101 102 103
107 108109
113 114 115 104
105 106
110
111
112
116
117
118

HEC064
EC-104

Page 824 of 1701




Repair
harness orcon-
nectors.
Repair harness orcon-
nectors.
Replace massairflow
sensor. Repair
harness orcon-
nectors.
NG
NG
NG
NG
INSPECTION
START
CHECK POWER SUPPLY.
1. Turn ignition switch&#34;OFF&#34;.
2. Disconnect massairflow sensor har-
ness connector.
3. Turn ignition switch&#34;ON&#34;.
4. Check voltage between terminal
@

and ground withCONSULT ortester.
Voltage: Batterypositive voltage
CHECK INPUTSIGNAL CIRCUIT.
Check harness continuity betweenter-
minal
CD
and ECM terminal
@
or@.
Continuity shouldexist.
If OK, check harness forshort.
INSPECTION END
OK
Trouble isnot fixed.
CHECK
GROUND CIRCUIT.
1. Turn ignition switch&#34;OFF&#34;.
2. Disconnect ECMharness connector.
3. Loosen andretighten engineground
screws.
4. Check harness continuity between
terminal
@
and ECM terminal
@
or

@
orengine ground.
Continuity shouldexist.
If OK, check harness forshort.
CHECK COMPONENT
(Mass airflow sensor).
Refer to&#34;COMPONENT INSPECTION&#34;
on page EC-107.
Disconnect andreconnect harnesscon-
nectors inthe circuits. Thenretest.
Check ECMpinterminals fordamage
or the connection ofECM harness con-
nector. Reconnect ECMharness con-
nector andretest.
SEF138R
TROUBLE
DIAGNOSIS FORDTC12
Mass AirFlow Sensor (MAFS) (Conl&#39;d)
DIAGNOSTIC PROCEDURE
For Europe ~GA 15DE engine
and Israel
I~
&#34;,,~~)rl

\~\&#34; /JJ~

11&#39;
Mass airflow sensor
_ harness connector

==---,

I-

I
I

d.-
I

;~

*1 ForEurope andIsrael, andGA15DE engine
*2 :GA 16DE engine models exceptfor
Europe andIsrael SEF139R
~
Mass airflow sensor
~(~lr~~

,~\ C/

Power steering \&#39;
tluic! reservxr ..--\ /,&#39;&#34;

W~
Meo,&#34;&#34;&#34;
EC-105

Page 825 of 1701

TROUBLEDIAGNOSIS FORDTC12
Mass AirFlow Sensor (MAFS) (Cont&#39;d)

Ii)
For Europe andIsrael, and
GA 15DE engine

~i5
cill1D

GA 16DE engine models exceptfor
Europe andIsrael

~15

1=&#39;
=E=CM==:!iH CONNECTOR
II

17 48

@ :Except forAustralia

@ :
For Australia SEF140R
[!J
For Europe andIsrael, and
GA 15DE engine models

~i5 ~i5

II
ECM
Ef
CONNECTOR
II
c:illli:>

16

@a

GA 16DE engine models exceptfor
Europe andIsrael

~io
~i5

II
ECM El&#39;CONNECTORII
ULffhD

16 47

@:
Except forAustralia
47 :For Australia SEF141R
EC-106

Page 826 of 1701




Voltage
V
Less than1.0
Conditions
Ignition switch&#34;ON&#34;(Engine stopped.)

Mass
airflow sensor

1. Turn ignition switch&#34;ON&#34;.
2. Start engine andwarm itup sufficiently.
3. Check voltage between terminal
CD
and ground.
Idle (Engine iswarmed-up sufficiently.) 1.2-1.8
4. IfNG, remove massairflow sensor fromairduct. Check hot
wire fordamage ordust.

TROUBLE
DIAGNOSIS FORDTC12
Mass AirFlow Sensor (MAFS) (Cont&#39;d)
COMPONENT INSPECTION

- -

* 1:For Europe andIsrae( andGA15DE engine
models
*2 :GA 16DE engine models exceptfor
Euro eand Irael SEF142R
SEF154N
EC-107

Page 827 of 1701

TROUBLEDIAGNOSIS FORDTC13
SEF594K Engine
Coolant Temperature Sensor(ECTS)

The engine coolant temperature sensorisused todetect the
engine coolant temperature. Thesensor modifies avoltage sig-
nal from theECM. Themodified signalreturns tothe ECM as
the engine coolant temperature input.Thesensor usesather-
mistor whichissensitive tothe change intemperature. The
electrical resistance ofthe thermistor decreases astempera-
ture increases.

20
18
6
9 4

B
2

Iii
10

1ii
0.8

&#39;0

£ 0.4
0.2
0.1 -20 020 40 60 80100
(-4) (32) (68)(104)(140)(176)(212)
Temperature &#39;C
(OF)

SEF012P
<

Reference data>

Engine coolant temper-
Voltage Resistance
ature
&#39;C (&#39;F) (V)

(kQ)
-10 (14) 4.47.0-11.4
20 (68)
3.52.1-2.9
50 (122)
2.20.6-1.0
90 (194) 0.9
0.23-0.26

Diagnostic
Trouble Code

No.
Malfunction
isdetected when... Check
Items
(Possible Cause)

13
•An excessively highorlow voltage fromthesensor •Harness orconnectors
is entered toECM. (Thesensor circuitisopen orshorted.)
• Engine coolant temperature sensor

DIAGNOSTIC TROUBLECODECONFIRMATION
PROCEDURE

(F.i\
1)Turn ignition switch&#34;ON&#34;.
~ 2)Select &#34;DATA MONITOR&#34; modewithCONSULT.
3) Wait foratleast 5seconds.

------------OR------------
fU\
1)Turn ignition switch&#34;ON&#34;andwait foratleast 5sec-
~ onds.
2) Turn ignition switch&#34;OFF&#34;, waitforatleast 5seconds
and then turn&#34;ON&#34;.
3) Perform &#34;Diagnostic TestMode II&#34;(Self-diagnostic
reSUlts) withECM.

EC-108

Page 828 of 1701

TROUBLEDIAGNOSIS FORDTC13 ~
Engine Coolant Temperature Sensor(ECTS)
(Cont&#39;d)

EC-ECTS-01

t
ENGINE
COOLANT
TEMPERATURE
SENSOR

m

@:ForEurope and
Israel

@:
Except@

*1&#34;,@ GY@BR!Y

,

-: Detectable line
for DTC
-: Non-detectable
line forDTC


lZlfll)

<I[g)
GY
B

~
GND
-A
B
~
GND -A ECM
(ECCSCONTROL
MODULE)

em

HEC032
EC-109

Page 829 of 1701

GA16DE forAustralia TROUBLE
DIAGNOSIS FORDTC13
[]K]

Engine Coolant Temperature Sensor(ECTS)
(Cont&#39;d)

EC-ECTS-01

~ENGINE COOLANT

TEMPERATURE

SENSOR

(ffl)

U:iJ
lbi=ll

BR/Y B

t
-:
-:
Detectable
line
for DTC
Non-detectable line forDTC

~<rrD

@
GY
BR/Y

IT5TI
TW
B

115&#34;0
I

GND -A
ECM
(ECCS
CONTROL
MODULE)

em

101 102103
107 108109
113 114115 104
105 106
110 HI H2
116 117118

EC-110 HEC065

Page 830 of 1701




Replace enginecoolant
temperature sensor.
Check
thefollowing.
• Harness foropen or
short between ECM
and engine coolant
temperature sensor
If NG, repair harness or
connectors.
Check thefollowing.
• Harness foropen or
short between ECM
and engine coolant
temperature sensor
If NG, repair harness or
connectors.

NG
NG
NG

CHECK COMPONENT
(Engine coolanttemperature sensor).
Refer to&#34;COMPONENT INSPECTION&#34;
on next page.INSPECTION
START

m
CHECK POWER SUPPLY.

1. Turn ignition switch&#34;OFF&#34;.
2. Disconnect enginecoolant tempera-
ture sensor harness connector.
3. Turn ignition switch&#34;ON&#34;
4. Check voltage between terminal @
and ground withCONSULT ortester.

~oltage:
Approximately SV
SEF519Q
Ii)

CHECK GROUND CIRCUIT.

1. Turn ignition switch&#34;OFF&#34;.
2. Check harness continuity between

SEF518Q
terminal
G)
and engine ground.

Continuity shouldexist.

If OK, check harness forshort.

TROUBLE
DIAGNOSIS FORDTC13 ~
Engine Coolant Temperature Sensor(ECTS)
(Cont&#39;d)
DIAGNOSTIC PROCEDURE

Engine
coolant temperature
sensor harness connector

~/

~Io
ten

~Io

~

Disconnectandreconnect harnesscon-
nectors inthe circuits. Thenretest.
Trouble isnot fixed.
Check ECMpinterminals fordamage
or the connection ofECM harness con-
nector. Reconnect ECMharness con-
nector andretest.
INSPECTION END

EC-111

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