clutch LAND ROVER DISCOVERY 1999 Owner's Manual

ENGINE - V8
12-2-32 REPAIRS
9.Fit alignment tool LRT-12-001 to spigot
bearing in crankshaft.
10.Fit drive plate onto tool LRT-12-001 ensure
side marked 'flywheel side' is towards flywheel.
11.Fit clutch cover and locate on dowels.
12.Fit clutch cover bolts and tighten in diagonal
sequence to 40 Nm (30 lbf.ft).
13.Fit gearbox assembly.

+ MANUAL GEARBOX - R380,
REPAIRS, Gearbox - V8.
Plate - drive - automatic
$% 12.53.13
Remove
Note: Later engines are fitted with a modified
starter ring gear which incorporates the reluctor
plate, spacer and hub. The modified ring gear
may be fitted as a replacement to early
engines.
1.Remove automatic gearbox.

+ AUTOMATIC GEARBOX - ZF4HP22
- 24, REPAIRS, Gearbox - convertor and
transfer gearbox - V8.
2.Remove 2 bolts securing CKP sensor cover.
3.Remove CKP sensor cover.
4.Remove 2 nuts securing CKP sensor.
5.Remove CKP sensor.

ENGINE - V8
12-2-50 OVERHAUL
Reassembly
1.Ensure both seal location and running surface
on crankshaft are clean. Ensure that bolt holes
in crankshaft are clean and dry.
2.Lubricate replacement oil seal with engine oil.
3.Lubricate seal guide LRT-12-095 with engine
oil and position guide to crankshaft.
4.Fit new seal squarely onto crankshaft and
remove guide LRT-12-095.
5.Fit seal into location using tools LRT-12-091
and LRT-99-003.
6. All engines: Ensure bolt holes in crankshaft
are clean and dry.
7. All engines: Clean all components.
8. All engines: Check that drive plate is free from
cracks and distortion.
9. Early engines: Fit hub, starter ring gear and
spacer to crankshaft, tighten Allen bolts to 78
Nm (58 lbf.ft).
10. Early engines: Fit drive plate and clamp ring,
tighten bolts to 45 Nm (35 lbf.ft).
11. Later engines: Fit starter ring gear, fit Allen
bolts and tighten to 85 Nm (63 lbf.ft).
12. Later engines: Fit drive plate and clamp ring,
fit bolts and tighten to 45 Nm (33 lbf.ft).
13.Fit CKP sensor.

+ ENGINE MANAGEMENT SYSTEM -
V8, REPAIRS, Sensor - crankshaft position
(CKP).
Seal - crankshaft - rear - manual models
$% 12.21.20.01
Disassembly
1.Restrain flywheel.
2.Working in sequence, loosen and remove 6
bolts securing clutch cover to flywheel.
3.Remove clutch cover.
4.Remove clutch plate.
5.Remove CKP sensor.

+ ENGINE MANAGEMENT SYSTEM -
V8, REPAIRS, Sensor - crankshaft position
(CKP).
6.Remove 6 bolts securing flywheel.
7.Remove flywheel.

ENGINE - V8
OVERHAUL 12-2-51
8.Carefully remove oil seal from cylinder block to
avoid damage to seal location or running
surface on crankshaft.
Reassembly
1.Ensure both seal location and running surface
on crankshaft are clean. Ensure that bolt holes
are clean and dry.
2.Lubricate replacement oil seal with engine oil.
3.Lubricate seal guide LRT-12-095 with engine
oil and position to crankshaft.
4.Fit new seal squarely onto crankshaft and
remove guide LRT-12-095.
5.Fit seal into location using tools LRT-12-091
and LRT-99-003.
6.Clean mating faces of flywheel and crankshaft,
dowel and dowel hole.
7.Fit flywheel to crankshaft and, working in a
diagonal sequence, tighten bolts to 78 Nm (58
lbf.ft). 8.Fit CKP sensor.

+ ENGINE MANAGEMENT SYSTEM -
V8, REPAIRS, Sensor - crankshaft position
(CKP).
9.Clean clutch cover, drive plate and spigot bush
in end of crankshaft.
10.Renew worn components as necessary.
11.If refitting existing drive plate, apply Molycote
FB 108 to splines.
12.Fit LRT-12-001 alignment tool to spigot bearing
in crankshaft.
13.Fit drive plate onto alignment tool, ensure side
marked 'flywheel side' is against flywheel.
14.Fit clutch cover and locate on dowels.
15.Fit clutch cover bolts and tighten in diagonal
sequence to 40 Nm (30 lbf.ft).

ENGINE - V8
12-2-52 OVERHAUL
Bearing - spigot - crankshaft
$% 12.21.45.01
Disassembly
1.Remove 6 bolts securing clutch cover.
2.Remove clutch cover.
3.Tap a thread in spigot bush to accommodate a
suitable impulse extractor.
4.Fit extractor to bush.
5.Remove bush from crankshaft. Reassembly
1.Clean bush register in rear of crankshaft.
2.Using a suitable drift, fit new bush to crankshaft
so that it is flush with or up to a maximum of 1.6
mm (0.06 in) below the end of the crankshaft.
3.Ream spigot bush to 19.117 + 0.025 − 0.00 mm
(0.75 + 0.001 − 0.00 in) .
4.Remove all traces of swarf on completion.
5.Clean mating faces of flywheel and crankshaft,
dowel and dowel hole.
6.Fit clutch cover to flywheel and tighten bolts by
diagonal slection to 40 Nm (30 lbf.ft).

ENGINE MANAGEMENT SYSTEM - V8
DESCRIPTION AND OPERATION 18-2-3
1Mass air flow/ inlet air temperature sensor
2Fuel injectors
3High tension leads/spark plugs
4Fuel pump relay
5ATC compressor clutch relay/ cooling fan relay
6Throttle position sensor
7Heated oxygen sensor
8Idle air control valve
9Ignition coils
10Engine coolant temperature sensor
11Crankshaft speed and position sensor
12Knock sensor
13Camshaft position sensor

ENGINE MANAGEMENT SYSTEM - V8
DESCRIPTION AND OPERATION 18-2-5
1Engine control module
2Crankshaft speed and position sensor
3Camshaft position sensor
4Engine coolant temperature sensor
5Mass air flow/ inlet air temperature sensor
6Throttle position sensor
7Heated oxygen sensors
8Fuel injectors
9Idle air control valve
10Fuel pump relay
11EVAP canister
12EVAP canister vent valve
13EVAP canister purge valve
14Fuel tank pressure sensor15Ignition coils
16Knock sensor
17Spark plugs
18High/ Low ratio switch
19Malfunction indication lamp
20Diagnostic connector
21Air temperature control clutch relay
22Air temperature control cooling fan relay
23ATC ECU
24CAN link to EAT
25SLABS ECU
26BCU
27Instrument cluster
28Thermostat monitoring sensor (where fitted)

ENGINE MANAGEMENT SYSTEM - V8
DESCRIPTION AND OPERATION 18-2-45
Malfunction Indicator Lamp (MIL)/ service engine soon warning lamp
The MIL/ service engine soon warning lamp is located in the instrument cluster. It illuminates to alert the driver to
system malfunctions. Service engine soon warning lamp is the name for this warning lamp in NAS only, it is called
MIL in all other markets.
During ignition a self-test function of the lamp is carried out. The lamp will illuminate for 3 seconds then it will
extinguish if no faults exist.

+ INSTRUMENTS, DESCRIPTION AND OPERATION, Description.
Input/Output
The MIL is supplied with battery voltage from the instrument cluster. When the ECM detects a fault, it provides an
earth path to illuminate the MIL. Output to the MIL is via pin 20 of connector C0637 of the ECM.
Air Temperature Control (ATC) request
The ATC request comes via the ATC switch located in the facia panel. When the driver operates the switch it acts as
a request from the ATC ECU to engage the ATC clutch to drive the system.
During periods of high driver demand such as hard acceleration or maximum rev/min the ATC clutch will be disabled
for a short time. This is to reduce the load on the engine.

+ AIR CONDITIONING, DESCRIPTION AND OPERATION, Description.

ENGINE MANAGEMENT SYSTEM - V8
18-2-46 DESCRIPTION AND OPERATION
Input/Output
The operation of the ATC request is via a switch being connected to earth. Voltage is supplied via pin 38 of connector
C0637 of the ECM, at the point at when the switch is pressed the connection is made and the ATC clutch is engaged.
The ATC request can fail as follows:
lOpen circuit.
lShort circuit to voltage supply.
lShort circuit to vehicle earth.
lWiring loom fault.
In the event of an ATC request failure, the ATC system does not work.
Should a malfunction of the component occur the following fault codes may be evident and can be retrieved by
TestBook.
P Code J2012 Description Land Rover Description
P1535 Air conditioning compressor request
malfunctionATC requested when not in standby mode

ENGINE MANAGEMENT SYSTEM - V8
DESCRIPTION AND OPERATION 18-2-47
ATC compressor clutch relay
The ATC compressor clutch relay is located in the engine compartment fuse box. It is a four pin normally open relay.
The relay must be energised to drive the ATC compressor clutch.
Input/Output
The ECM provides the earth for the relay coil to allow the relay contacts to close and the ATC clutch drive to receive
battery voltage. The ECM uses a transistor as a switch to generate an open circuit in the earth path of the relay coil.
When the ECM opens the earth path, the return spring in the relay will pull the contacts apart to shut down the ATC
clutch drive.
Input to the ATC clutch relay switching contacts is via fuse 6 located in the engine compartment fuse box. The relay
coils are supplied with battery voltage from the main relay, also located in the engine compartment fuse box. The earth
path for the relay coil is via pin 29 of the ECM C0657 connector. When the relay is energised the output from the
switching contacts goes directly to the ATC compressor clutch.
The ATC clutch relay can fail in the following ways:
lRelay open circuit.
lShort circuit to vehicle supply.
lShort circuit to vehicle earth.
lBroken return spring.
In the event of an ATC clutch relay failure, the ATC does not work.
Should a malfunction of the component occur, the following fault codes may be evident and can be retrieved by
TestBook.
P Code J2012 Description Land Rover Description
P1536 Air conditioning compressor request range/
performanceATC compressor clutch relay open circuit
P1537 Air conditioning compressor request low input ATC compressor clutch relay short to earth
P1538 Air conditioning compressor request high input ATC compressor clutch relay short to battery supply

ENGINE MANAGEMENT SYSTEM - V8
DESCRIPTION AND OPERATION 18-2-61
DESCRIPTION AND OPERAT ION
Cruise control component layout
1Cruise control ECU
2Cruise control master switch
3SET+ switch
4RES switch
5Brake pedal switch
6Clutch pedal switch7BCU
8Vacuum pump assembly
9Pneumatic actuator
10SLABS ECU
11Automatic gear selector lever