NISSAN ALMERA N15 1995 Service Manual

SERVICEDATAANDSPECIFICATIONS (50S)
General Specifications

Suspension type
Strut type
Stabilizer Independent
macpherson struts
Double-acting hydraulic
For 14-and 15-inch wheelmodels

Inspection andAdjustment
WHEEL ALIGNMENT (Unladen*1)

GAengine andSR CDengine andSR
Applied model engine
models with enginemodels with
14-inch wheels 15-inchwheels
Camber Minimum

-no'

(-1.33')

.

Degree minute Nominal
-0'35'
(-0.58')
(Decimal degree)Maximum 0'10'
(0.1
r)

Caster Minimum

0'40'(0.6r)

Degree minute Nominal
1
'25' (1.42')
(Decimal degree)Maximum 2'10'
(217")
Kingpin inclination Minimum14'00'
(14.00')
Degree minute Nominal
14'45'
(14.75')
(Decimal degree)Maximum 15'30'
(15.50')
Total toe-in Minimum0(0)
Distance (A-B) Nominal
2(008)
mm (in) Maximum 4(0.16)
Minimum 0'
(0.00')
Angle (leftplus right)
Nominal 11'
(0.18')
Degree minute
(Decimal degree)Maximum 22'
(0.37")
Wheel turning angle Minimum
38'00'
(38.00') 34'00'(34.00')
Inside Nominal4nO'
(41.00')
3rOO'(37.00')

Degree minute
(Decimal degree)Maximum
42'00'
(42.00')
38'00'(38.00')
Full (urn'2
Outside
Degreeminute Nominal 34'00'
(34.00') 31'00'(3100')
(Decimal degree)
'1' Fuel, radiator coolantandengine oilfull. Spare tire,jack, hand tools andmats indesignated positions.
'2: On power steering models,wheelturning force(atcircumference ofsteering wheel)of98 to147 N(10 to15 kg, 22to33 Ib)with engine
idle

FA-29
•

SERVICEDATAANDSPECIFICATIONS (SDS)
Inspection andAdjustment (Cont'd)

Nissan genuine greaseorequivalent

g
(oz)
Grease
Capacity

DRIVE
SHAFT

GA14DE,GA16DE, SA
20DE
Applied model
GA15DECD20
AHLH

Bootlength

Joint type
Wheel
side

Transaxle side TS70C TS79C
DS83TS83
Wheel side ZF80ZF90 BF83
Boot length mm(in)
Transaxle sideL
2
95.5
-97.5 101.5-103.5 97
-99 98-100
(376 -3.84) (4.00-4.07) (3.82-3.90) (3.86-3.94)

Transaxle side

Wheel sideL, 90.5
-92.5 96-98
94-96 (3.70 -3.78)
(3.563 -3.642) (3.78
-3.86)
85-105 (3.00 -3.70)
Transaxle
side
Wheel side 110
-120
(388 -4.23)
95 (3.35) 155
-165
(5.47 -5.82)
115 -125
(4.06 -4.41) 115
-135
(4.06 -4.76) 130
-150
(4.59 -5.29)

SFA3968
WHEEL BEARING WHEEL
RUNOUT

Unit:mm(in)
Wheel bearing axialendplay
limit mm(in)
Wheel bearing locknut
tightening torque
N'm (kg-m, ft-Ib)
Preload 0.05
(0.0020) orless
196 -275 (20-28, 145 -203) Wheel
type Aluminum
wheel Steelwheel
Maximum radial
0.3(0.012) 0.5(0.020)
runout limit
Maximum lateral
03(0.012) 0.8(0.031)
runout limit
N'm (kg-em, in-Ib)
At hub bolt
N
(kg, Ib)
0.90
(9.2, 8.0)
6.08 (0.62, 1.37)

LOWER BALLJOINT

Swinging force"A"
(Measured atcotter pinhole)

N (kg, Ib)
8.24
-5737
(0.84 -5.85, 1.85-12.90)
Turning torque"B"
Nm (kg-em, in-Ib)
Vertical endplay limit "C"

mm (in)
0.49
-3.43 (5.0-35, 4.3 -30.4)
0(0)

FA-30

ACCELERATORCONTROL,FUEL
&

EXHAUST SYSTEMS
SECTION
FE
CONTENTS
ACCELERATOR CONTROLSySTEM 2FUELSYSTEM 3

Adjusting Accelerator Wire 2FuelPump andGauge 4

EXHAUST SySTEM
5
•

ACCELERATORCONTROLSYSTEM

CAUTION:
• When removing accelerator wire,make amark toindicate locknut's initial position.
• Check thatthrottle valveopens fullywhen accelerator pedalisfUlly depressed. Checkthatthrottle
valve returns toidle position whenaccelerator pedalisreleased.
• Check accelerator controlpartsforimproper contactwithanyadjacent parts.
• When connecting accelerator wire,becareful nottotwist orscratch wire.
• For adjustment ofAfT throttle wire,refertoinAT section ("Throttle WireAdjustment", "ON-VEHI-
CLE SERVICE").
SEC. 180

SFE413A

iii
:
N'm (kg-m, in-Ib)

5

~~
Iii]
3.4 (0.3 .0.4, 26.36)

~~~

5

CD20
engine models

r
1iI4.4 •5.9

~ (0.45-0.60, 39.1•52.1)

\i
v'

!il2.9-3.9

~ (0.30-0.40, 26.0-34.7)

7C
A~

~'
.

.
~

3l~

,

G)
Accelerator wire

@
Wire bracket
@

Pedal bracket

@
Return spring
CID

Accelerator pedal

@
Dynamic
damper

SFE249AD

GA
engine models

Locknut

~8 -11N.m

(0.8 -1.1 kg-m,

69 -95 in-Ib)
Adjusting
Accelerator Wire

1. Loosen locknut,andtighten adjusting nutuntil throttle drum
starts tomove.
2. From thatposition turnback adjusting nut1.5to2turns, and
secure locknut.

SR and CDengine models

Lock nut

• 8-11 N.m

(0.8 -1.1 kg-m,
69 -95 In-Ib)

SFE411AA FE-2

FUELSYSTEM

WARNING:
When replacing fuellineparts, besure toobserve thefollowing:
• Put a"CAUTION: INFLAMMABLE" signinworkshop.
• Donot smoke whileservicing fuelsystem. Keepopenflames andsparks awayfromwork area.
• Besure todisconnect batterygroundcablebefore conducting operations.
• Besure tofurnish workshop withaCO
2
fireextinguisher.
• Put drained fuelinan explosion-proof containerandputlidon securely.
CAUTION:
• For ECCS engine models, releasefuelpressure fromfuelline. Refer toEC section ("FuelPressure
Release", "BASICSERVICE PROCEDURE").
• Donot disconnect anyfuel lineunless absolutely necessary.
• Plug hose andpipe openings toprevent entryofdust ordirt.
• Always replace O-ringandclamps withnewones.
• Donot kink ortwist hose andtube when theyareinstalled.
• Donot tighten hoseclamps excessively toavoid damaging hoses. •
• When installing fuelcheck valve, becareful ofits designated direction.RefertoEC section ("FUEL
CHECK VALVE", "EVAPORATIVE EMISSIONSYSTEM").
• After installation, runengine andcheck forfuel leaks atconnections.

SFE414A

CD
engine models

.
I
i

~ tt'.J
28•35 (2.8 -3.6, 20•26)

,

.

~o-nngt:1

...,/ tt'.J
28-35

ge.
V
(2.'.3.6, 20•26)

, I

GA

&
SR engine models
SEC. 172 ~
2.0-2.5

r
(0.20•0.26,

~.4'22.6)

~ .---£l

~I

~j~
~.

tt'.J :
N. m (kg-m, It-Ib)

iii :
N'm (kg-m, in-Ib)

CD
Fuelgauge
@ Chamber @
Fuelpump
@

Fueltank

FE-3

Connector
/

SFE145A

t2Front
SFE366AFUEL
SYSTEM
Fuel Pump andGauge
REMOVAL
1. Release fuelpressure fromfuelline.
Refer toEC section ("FuelPressure Release", "BASICSER-
VICE PROCEDURE").
2. Remove inspection holecover located undertherear seat.
3. Disconnect fueloutlet, returntubeandconnectors.
4. Remove thesixscrews.
5. Remove fuelgauge assembly anddisconnect tubesand
connector.
6. Remove fuelpump withfueltank chamber asshown inthe
figure.
a. Pull upthe front offuel pump.
b. Slide itforward.

Fuel pump harness
Fuel pump

SFE366A
7.
Remove fueltank chamber fromfuelpump.

INSTALLATION

To install, reverse theremoval procedure.

CAUTION:
• Tighten tospecified torque.
• Install fuelpump harness onthe leftside ofthe feed hose
as shown inthe figure.
FE-4

SFE180A

SR engine models

SEC. 200-208

toJ
13-16 (1.3 -1.6, 9-12)
EXHAUST
SYSTEM
CAUTION:

• Always replace exhaust gasketswithnewones when reas-
sembling. If gasket isleft onflange surface, scrapeoffcompletely as
shown atleft.
• With engine running, checkalltube connections forexhaust
gas leaks, andentire system forunusual noises.
• After installation, checktoensure thatmounting brackets
and mounting insulators arefree from undue stress.
If
any
of the above partsarenotinstalled properly, excessive
noise orvibration maybetransmitted tothe vehicle body.

GaSket~
toJ:
N'm (kg-m, ft-Ib)
~ :N'm (kg-m, in-Ib)

SFE412A
FE-5
•

EXHAUSTSYSTEM

C1 tOJ
28•33 (2.9 -3.4, 21-25)
Ii]

4.9•6.9
(0.50 •0.70, 43.4•60.8)

L~tCJ
43-55

(4.4 •5.6,

32 •41)
~~
! ~

C1tOJ
28-33 ~~
(2.9 •3.4, 20.7 •24.3)
i

Gasket
C1
b ~

-~r~
5.1•6.5

V
(0.52•0.66,
45.1 •57.3)

Heat insulator
II]
5.1•6.5 (0.52 •0.66, 45.1•57.3)
GA
engine forEurope models
models

tOJ
13. 16(1.3 •1.6, 9.12)

Ii]
5.1•6.5
(0.52 -0.66, 45.1•57.3)

Ii]

5.1-6.5
(0.52 -0.66,
45.1 -57.3)
GA
engine forAustralia

SEC. 200-208

tCJ
43-55 Collar

(4.4 -5.6,

32 -41)
~ :N'm (kg-m, in-Ib)

tCJ :
N.m (kg-m, fl.lb) -
Among Europe model!l, onlyGA16DE engine model
has aheat insulator onthe exhaust fronttube,
MFE024A
FE-6

EXHAUSTSYSTEM

•

MFE023A

to.J

30-39 (3.1 -4.0, 22.1 -28.8)
~ 13-16 (1.33 -1.63, 9.6-11.8)

iii :
N'm (kg-m, in-Ib)
~ :N'm (kg-m, ft-Ib)
\ollar

8~
13-16
(1.33 -1.63,
~ 43_55 ~9.6-11.8)

(4.4.5.6,31.7' 40'6)'~~

o
to.J
28-33 \
{J)f:::@

(2.9 -3.4, 20.7 -124.3)

~~
Gasket
0
1 ".~

Gasket
0

v' •

. . . .v. ~
5.1-6.5 (0.52 -0.66,45.1 -57.3)

I~'''~ CD20engine models

. 0
to.J
60-70 (6.1 -7.1, 44.3 -51.6)

Heat Insulator ~~
• Gasket~ :

iii
5.1-6.5 (0.52 -0.66, 45.1-57.3)
7
r

o

GA
engine exceptforEurope andAustralia models
SEC. 200
FE-7

ENGINECONTROL SYSTEM
SECTION
EC
CONTENTS
•

PRECAUTIONS ANDPREPARATION
4

Special Service Tools 4
Supplemental RestraintSystem(SRS)"AIR
BAG" (DualAirBag System) 7
Supplemental RestraintSystem(SRS)"AIR
BAG" (Single AirBag System) 7
GA,SR
PRECAUTIONS ANDPREPARATION
8

Engine Fuel
&
Emission ControlSystem 8
Precautions forECCS Trouble Diagnosis of
Engine 9
Precautions 9
ENGINE ANDEMISSION CONTROLOVERALL
SYSTEM 11
Circuit Diagram -Except forAustralia 11
Circuit Diagram -For Australia 12
System Diagram -GA 14DE, GA16DE for
Europe andIsrael 13
System Diagram -GA15DE 14
System Diagram -GA 16DE except for
Europe, IsraelandAustralia 15
System Diagram -GA 16DE forAustralia 16
ECCS Component PartsLocation -GA 14DE,
GA 16DE forEurope andIsrael 17
ECCS Component PartsLocation -GA15DE 18
ECCS Component PartsLocation -GA 16DE
except forEurope, IsraelandAustralia 19
ECCS Component PartsLocation -GA 16DE
for Austral ia 20
ECCS Component PartsLocation 21
Vacuum HoseDrawing 22

c=
~

GA
ENGINE
ANDEMISSION BASICCONTROL
SYSTEM DESCRiPTION 23
System Chart.. 23
Multiport FuelInjection (MFI)System 24
Distributor Ignition(01)System 27
Air Conditioning CutControl 28
Fuel CutControl (atnoload &high engine
speed) 28
EVAPORATIVE EMISSIONSYSTEM
29

Inspection 29
POSITIVE CRANKCASE VENTILATION 31
Description 31
Inspection 32
BASIC SERVICE PROCEDURE 33
Fuel Pressure Release 33
Fuel Pressure Check 33
Fuel Pressure Regulator Check 33
Injector Removal andInstallation 34
Idle Speed/lgnition Timing/ldleMixtureRatio
Adjustment ,35
ON-BOARD DIAGNOSTIC SYSTEMDESCRIPTION .44
Malfunction IndicatorLamp(MIL) 44
CONSULT .48
TROUBLE DIAGNOSIS -General Description
58

Introduction 58
Work Flow 59
Description forWork Flow 60
Diagnostic Worksheet 61
Diagnostic TroubleCode(DTC) Chart 62
Fail-Safe Chart 64
Basic Inspection 65
Fast IdleCam (FIC) Inspection and
Adjustment -For Europe andIsrael 68
Fast IdleCam (FIC) Inspection and
Adjustment -Except forEurope andIsrael. 68
Symptom MatrixChart 71