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Ford Thunderbird Engine Information
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The following technical bulletins were published by AERA.
 ENGINE SPECIFICATIONS
           Piston-To-Bore Clearance Specifications On
           1983 Ford Products With 2.3L (OHC) Engines

Ford Motor Company has provided AERA with specifications for
servicing pistons on 1983 model vehicles equipped with the 2.3L
(OHC) engine.

The specifications listed on the reverse side of this bulletin,
only apply to the following vehicles:

          Ford                     - Mustang and Thunderbird

          Lincoln-Mercury          - Capri and Cougar

Additional engine service information is also listed for your
use.

                     ENGINE  SPECIFICATIONS
                         2.3L 1-4 (OHC)

Piston

Piston
     Diameter
          Coded Red           3.7764-3.7770
          Coded Blue          3.7776-3.7782
          0.003 Oversize      3.7788-3.7794
     Piston-to-Bore Clearance 
     (select fit)                  .0030-.0038
Pin Bore Diameter                  0.9123-0.9126
     Pin Groove Width
          Compression (top)        0.080-0.081
          Compression (bottom)     0.080-0.081
          Oil                      .188-.189
Piston Pin
     Length                   3.010-3.040
     Diameter
          Standard            0.9118-0.9124
          0.001 Oversize      0.9130-0.9133
          0.002 Oversize      0.9140-0.9143
     Piston-to-Pin Clearance       .0003-.0005
     Pin-to-Rod Clearance          interference fit

Piston Rings
     Ring width
          Compression (top)        0.077-0.078
          Compression (bottom)     0.077-0.078

     Side Clearance
          Compression (top)        0.002-0.004
          Compression (bottom)     0.002-0.004
          Oil Ring            snug fit
          Service Limit       0.006 Max.
     
     Ring Gap
          Compression (top)        0.010-0.020
          Compression (bottom)     0.010-0.020
          Oil (Steel Rail)         0.015-0.055
 
Lubrication System

Oil Pump
     Relief Valve Spring Tension
     (Lbs Spec Length)             15.2-17.2 @ 1.20
     Drive Shaft-to-Housing
     Bearing Clearance             0.0015-0.0030
     Relief Valve-to-Bore Clrnce   0.0015-0.0030
     Rotor Assembly End Clearance
     (assembled)                   0.004 Max
     Outer Race-to-Housing Clrnce  0.001-0.013
     Oil Capacity                  5.0

Torque Specifications - Special Applications

Item                               Size N·m       Lb.Ft
Auxiliary Shaft Gear Bolt          M10  38-54     28-40
Auxiliary Shaft Thrust Plate Bolt  M6   8-12      6-9
Belt Tensioner (Timing Pivot)      M10  38-54     28-40
Belt Tensioner (Timing Adjustg)    M8   19-28     14-21
Camshaft Gear Bolt                 M12  68-96     50-71
Camshaft Thrust Plate Bolt         M6   8-12      6-9
Carburetor to Spacer Stud          M8   10-20     7.5-15
Carburetor to Spacer Nut           M8   14-19     10-14
Carburetor Spacer To Manifold
Bolt                               M8   19-28     14-21
Connecting Rod Nut                 M9   41-49     30-36
Crankshaft Damper Bolt             M14  136-192   100-120
Cylinder Head Bolt                 M12  108-122   80-90
Distributor Clamp Bolt             M10  19-28     14-21
Distributor Vacuum Tube to
Manifold Adaptor                        7-11      5-8
Exhaust Manifold to Cylinder Head
Bolt Stud or Nut                   M10  22-31     16-23
Flywheel to Crankshaft Bolt        M10  73-87     56-64
Fuel Pump to Cylinder Block        M8   19-28     14-21
Intake Manifold to Cylinder
Head Bolt Nut                      M8   19-28     14-21
Main Bearing Cap Bolt              M12  108-122   80-90
Oil Pressure Sending Wire 
To Block                                11-24     8-18
Oil Pump Pickup Tube to Pump       M18  19-28     14-21
Nut-Turbo to Manifold                   38-54     28-40
Nut-Oil Supply Line                     27-40     20-30
Nut-Oil Supply Line Fitting             12-16     9-12
Nut-Oil Return Fitting to Block         8-12      6-9
Bolt-Intake Manifold-Upper to Lower     19-29     14-21
Nut-Throttle Body to Upper Intake       19-29     14-21
Oil Pump to Block                  M8   19-28     14-21
Oil Pump Cover                          10-15     90-130
Oil Pan Drain Plug to Pan          M14  21-33     15-25
Oil Pan to Block                   M6   7-11      6-8
                                   M8   11-13     8-10
Oil Filter Insert to
Cylinder Block                          28-33     20-25
Oil Filter to Engine               
Rocker Arm Cover to Cyl Head       M6   7-11      5-8
Spark Plug to Cyl Head             M14  7-13      5-10
Temperature Sending Unit 
to Block                                11-24     8-18
Water Jacket Drain Plug to Block        32-37     23-28
Water Pump to Block Bolt           M8   19-28     14-21
EGR Valve to Spacer Bolt           M8   19-28     14-21
EGR Tube to Exhaust Manifold Conn       13-14     9-11
EGR Tube Nut                            13-14     9-11
Auxiliary Shaft Cover Bolt         M6   8-12      6-9
Water Outlet Connection Bolt       M8   19-28     14-21
Cylinder Front Cover Bolt          M6   8-12      6-9
Inner Timing Belt Cover Stud       M8   19-28     14-21
Outer Timing Belt Cover Bolt       M6   8-12      6-9
Rocker Arm Cover Shield Bolt       M10  38-54     28-40
Thermactor Check Valve
to Manifold                        17   24-27     17-20
Fuel Filter to Carburetor
Assembly-Bolt                           9-11      80-100

New And Used Drive Belt Tension Specifications
Belts have differing tension specifications depending on whether
they are Newly Installed (1) or Used (more than ten minutes of
engine operation). When belts are found to be below the allowable
minimum they must be RESET (adjusted). Specifications for these
situations are shown below.

Belt Type Belt Condition and Tension in Lbs
               Installed Reset Limits
1 4V           50-80     40-60
All other V    120-160   90-120

NOTE:     FIXED refers to systems with manually adjusted centers
          which are bolted in place and considered fixed.

1.   Newly Installed - refers to the condition of the NEW drive
     belt before the enginehas made no more than one rotation
                         and before the belt has had a chance to
                         stretch or seat into the pulley grooves.
2.   Time required for plunger to leak down 18 of travel with 50
     lb load leakdown fluidin lash adjuster.
3.   Distance in inches that front bearing is installed below
     front face of bearing tower.
4.   0.002 undersize - Add 0.001 to Standard Thickness
5.   Pin bore and crank bearing bore must be parallel and in the
     same vertical plane, within the specified total difference
     when measured at the ends of an 8 bar -4 on each side of
     rod centerline.
6.   Measure at the position pin bore, centerline - 90^ to the
     pin
7.   Add one pint with filter change
8.   On engine, temperature normal,curb idle, in neutral, brakes
     set
9.   Pump to tank return line pinched off, new fuel filter in
     line
10.  Smallest orifice = not less than 0.220 ID
11.  Torque in sequence in two steps:
     Step 1    34-41 N·m (25-30 lb ft)
     Step 2    41-49 N·m (30-36 lb ft)
12.  Torque cylinder head bolts in sequence in tow steps:
     Step 1    68-81 N·m (50-60 lb ft)
     Step 2    108-122 N·m (80-90 lb ft)
13.  Torque in sequence in two steps:
     Step 1    7-9 N·m (5-7 lb ft)
     Step 2    23-31 N·m (16-23 lb ft)
14.  Torque in sequence in two steps:
     Step 1    7-9 N·m (5-7 lb ft)
     Step 2    19-28 N·m (14-21 lb ft)
15.  Torque in sequence in two steps:
     Step 1    68-81 N·m (50-60 lb ft)
     Step 2    108-122 N·m (80-90 lb ft)
16.  12 turn after gasket contacts surface - oil gasket.
17.  Then rotate to position.
                                        



                                     The AERA Technical Committee


October 1983 - TB 294

##END##
 CRACKING FLEX COOLING FANS
                                            Cracking Flex Cooling Fans

AERA members who are installing engines or selling remanufactured engines to installers should be aware of the following dangerous situation.

As under hood temperatures have increased and engine noise in the passenger compartment has become less acceptable, many manufacturers have resorted to installing flex cooling fan assemblies.  This practice is also quite popular with RV and off road vehicles that may be pushed a little harder and can use the
extra air flow through the radiator.

On vehicles equipped with flex blade cooling fans, the National Highway Traffic Safety Administration (NHTSA) determined that: Blades may crack and may, over a period of time, loosen from the fan blade assembly.  Blade pieces may damage components under the hood.  If the hood is open while the engine is operating, persons standing nearby may be injured if the fan breaks.  Impending
blade failure may be evidenced by rattling or vibration.

Consequently, the Ford Motor Company was asked to recall 1977 Thunderbird, Cougar, LTD II and Ranchero automobiles equipped with 5.0, 5.8 & 6.6L (302, 351M & 400 CID) engines with A/C.  Also recalled were 1978-79 Granadas and Monarchs equipped with 4.1L (250 CID) engines with A/C.  A revised design cooling fan was to be installed on these vehicles.  

The next time you or your customer installs an engine, take a careful look at the cooling fan assembly.  Maybe it too needs to be replaced.  In either case, avoid leaning over or standing next to the cooling fan of an operating engine.

                                                                           The AERA Technical Committee
 OVERSIZE HOUSING BORES
                                Oversize Main Bearing Housings On Some
                                             Ford 2800 CC V6 Engines

Oversize main bearing housings have been found in some Ford 2800 cc V6 engines.  the subject engines had main bearing saddles in the block with .015 oversize housings.

Ford Motor Co. supplies .015 oversize OD bearings for this engine with Standard, .010, .020 and .030 undersize ID.

                                                                          The AERA Technical Committee
 BEARING FAILURES
                                                Bearing Failures On
                                Ford 5.0 & 5.7L (302 & 351W CID) Engines

AERA members have experienced premature crankshaft bearing failures on 5.0 & 5.7L Ford engines.

Investigating these failures disclosed that all of the machined components were on size and the proper tolerances had been achieved.  Closer inspection of other engine components revealed a crack in the exhaust crossover passage on the bottom side of the intake manifold.

Exhaust gases entering the crankcase through the crack not only contaminate the engine oil, but the oil itself is super heated to the point where it no longer lubricates resulting in contact between the bearing and the crankshaft journal.

Pressurizing the crankcase with exhaust gases should also overwhelm the PCV system leading to excessive oil consumption or oil in the air cleaner.

For additional information see AERA Technical Bulletins: TB 519 &
SB 146

                                                                      The AERA Technical Committee
 OIL IN THE COOLING SYSTEM
                                          Oil In The Cooling System On
                                           Ford 3.8L (232 CID) Engines

AERA member machine shops have reported multiple instances of vehicles with cooling systems contaminated by engine oil.

One possible cause cited in many of the reported cases was that the engines were permitted to freeze up during cold ambient temperatures.  Usually one or more of the core plugs was pushed out of the cylinder block, but the damage is not limited to that alone.  The ice inside of the cylinder block water jacket expands and partially crushes an oil gallery.

When the core plugs are replaced and the cooling system is refilled, oil finds its way into the radiator.  The cylinder block is no longer serviceable and must be replaced.

                                                                     The AERA Technical Committee
 INTAKE MANIFOLD COOLANT & VACUUM LEAKS
                         Intake Manifold Coolant & Vacuum Leaks On
                                Ford 5.0L, 5.0L HO and 5.8L Engines

Intake manifold coolant and vacuum leaks have been found to be quite common on Ford 5.0L, 5.0L HO (High Output) and 5.8L engines.  For this engine, following the proper intake manifold torque values and torque sequence is very critical.

Installation of the aluminum intake manifold should proceed as follows:

    Clean all gasket surfaces of debris and oil residue.

    Apply a 1/8 bead of silicone sealer in the 4 corners where the cylinder heads 
    meet the cylinder block (Figure 1).

    Install the intake manifold side and end gaskets and apply a 1/16 bead of 
    silicone sealer in the 4 joints formed by the gaskets.

    Mount the manifold and torque the bolts in sequence to 15-20 lbs.ft (Figure 2).

    Torque the bolts in sequence to 23-25 lbs.ft.

    After the engine has reached operating temperature, retorque the intake 
    manifold bolts to 23-25 lbs.ft.

                                                                                  The AERA Technical Committee
 IGNITION FIRING ORDER ON HO ENGINES
                                     Ignition Firing Order On
                            Ford 5.0L HO (High Output) Engines

There seems to be much confusion about the firing order on Ford 5.0L HO (High Output) engines. 

Contrary to the plain 5.0L engine, the HO (High Output) version uses the same firing order as the 5.8L engine.  This is probably the case because early 5.0L HO engines used a 5.8L marine camshaft.

The firing order for the standard 5.0L is: 1-5-4-2-6-3-7-8.  The firing order for the HO engine is: 1-3-7-2-6-5-4-8.  The rotor inside the distributor rotates counterclockwise on both engines (see illustration).

Using the plain 5.0L firing order on the HO engine does work, however the engines will have low vacuum and very poor idle.  At higher rpm it appears to smooth out, but is very low on horse power, not at all what the customer will expect from this potent power plant. 

                                                                        The AERA Technical Committee