Tdi200 Turbina
Tdi200 Turbina
ENGINE
Firing order ........................................................ 1-3-4-2
. . .
Injection timing ................................................... 13"
Timing marks:
Valve timing ....................................................... Slot for peg in flywheel and TDC mark on front pulley
Injection timing ................................................... Special tool inserted in D.P.S. pump
Tappet clearances inlet and exhaust .......................... (0.010 in)
Valve timing
Inlet opens ..........................................................
Inlet closes .......................................................... 42" A.B.D.C.
Inlet peak ........................................................... 103" A.T.D.C.
Exhaust opens ..................................................... 51" B.B.D.C.
Exhaust closes ..................................................... 13"A.T.D.C.
Exhaust peak ...................................................... 109" R.T.D.C.
lift
Inlet .................................................................. (0,388 ins)
Exhaust ............................................................. (0.404 ins)
PUMP
.......................................................... CAV DPS type with boost control and two speed
mechanical governor with auto advance and solenoid
electrical shut-off. Tamper proof sealing on flight speed
and fuel adjustment screws.
Direction of rotation ............................................. Clockwise, viewed from drive
Advance box (two stage) ........................................ 7" advance with 3" start retard
Back leakage rate 150-100Atm:
New nozzle ................................................... 7 seconds
Original nozzle .............................................. 5 seconds
Despatch nozzle .............................................
INJECTORS
.......................................................... CAV Pintaux DES5385001
Nozzle size .......................................................... 6209
Opening pressure (working pressure) ........................ to 140
Injector pipe type ................................................. High pressure multi-bundy
size .................................................. to
length .............................................. (18 ins)
HEATER PLUGS
.......................................................... ii
Time to reach operating temperature of 850°C ............ 8 seconds
TURBO-CHARGER
.......................................................... Garrett T2
Maximum boost pressure ....................................... 48 H G (9.3 P.S.I.G.) measured at wastegate actuator
"T" piece
44
DIESEL FUEL SYSTEM -T U RB O C H A R G ED ENGINE
TURBO-CHARGER
The following list of oils is for emergency use only if the above oils arc not can be used for topping-up
without detriment, but if used for engine oil changing, they are limited to a maximum 5,000 (3,000 miles)
between oil and filter
Vanellus C3 15/40
CASTROL Dcusol RX Super 15/40
Hypergrade 15/50
ESSO Essolube XD-3 15/40
MOBIL Delvac Super 15/40
PETROFINA Fina Dilano HPD 15/40
SHELL X 15/40
TEXACO URSA Super Plus 15/40
Use only oils to or API Service levels C D or SECTION
MAINTENANCE SCHEDULE
The following additional maintenance is required for the turbo charged engine to that contained in main
for the non-Turbo Charged 2.5 Litre Diesel cngine.
Fitting
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11. Fit the raised bead side of a new gasket uppermost
to the exhaust manifold and fit and secure the
turbo-charger with the four nuts, tightening evenly
to the correct torque and secure with lock tabs.
Fit the exhaust elbow, using a new gasket, to
turbo-charger and retain with the five nuts
tightening evcnly to the correct torque.
46
DIESEL FUEL SYSTEM-TURBO C H A R G E D ENGINE
47
DIESEL FUEL SYSTEM- TURBO CHARGED ENGINE
48
COOLING SYSTEM
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ENGINE PROTECTION DRAIN AND FILL ENGINE COOLING SYSTEM
To prevent corrosion of the aluminium alloy engine WARNING: Do not remove the radiator filler cap when
parts it is imperative that the cooling system is filled the engine is hot because the cooling system is
with a solution of clean water and the correct type of pressurized and personal scalding could result.
anti-freeze, winter and or water and inhibitor
if frost precautions are not required. Never fill or 1. Remove the radiator filler plug.
top-up with water only, always add an inhibitor
(Marstons if anti-freeze is not used. NEVER
salt water with an inhibitor otherwise corrosion will
occur. In certain territories where the only available
water supply may have some salt content, use only
clean rainwater or distilled water.
Recommended solutions
Anti-freeze Universal Anti-freeze or
permanent type ethylene base, without methanol, with
a suitable inhibitor for aluminium engines and engine
parts.
Use one part of anti-freeze one part water.
Inhibitor Lubricants SQ36 inhibitor
concentrate.
Use 100 of inhibitor per litre of water.
Anti-freeze can remain in the cooling system and will
provide protection for two years provided
that the specific gravity of the coolant is checked before
onset second winter and topped-up with new 2. Remove radiator drain plug and allow
anti-freeze as required. coolant to drain, if neccssary, into suitable
Land Rovers leaving the factory have the cooling container. Refit drain plug and washer. The
system filled with 50% of anti-freeze mixture. This drain plug is situated on the left-hand side of
gives protection against frost down to minus 47°C radiator towards t h e bottom facing the engine
(minus 53°F). Vehicles so filled can be identified by a compartment.
label affixed to t h e windscreen and radiator.
After the second winter the system should be drained NOTE: Disconnect bottom hose to drain on radiators
and thoroughly flushed. adding new anti-freeze without a drain plug. Connect hose after draining.
examine all joints and renew hoses t o make
sure that the system is leakproof. Inhibitor solution
should be drained and flushed out and new
solution introduced every two years, or where
the purity of the water is qucstionablc.
See the ‘General specification data’ section for
protection quantities.