2006 DODGE RAM SRT-10 Service Repair Manual

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DODGE RAM SRT-10 2006 Service Repair Manual CODE FAMILY NAME COMMON TRADE NAME TYPICAL APPLICATION
MPU FOAM POLYURETHANE MPU SPOILERS
PE POLYETHYLENE ALATHON, DYLAN,
LUPOLEN, MARLEX—
PP POLYPROPYLENE
(BLENDS)NORYL, AZDEL, MARLOX,
DYLON, PRAVE

CODE FAMILY NAME COMMON TRADE NAME TYPICAL APPLICATION
MPU FOAM POLYURETHANE MPU SPOILERS
PE POLYETHYLENE ALATHON, DYLAN,
LUPOLEN, MARLEX—
PP POLYPROPYLENE
(BLENDS)NORYL, AZDEL, MARLOX,
DYLON, PRAVEXINNER FENDER, SPOILERS,
KICK PANELS
PP/EPDM PP/EPDM ALLOY PP/EPDM SPOILERS, GRILLES
PUR POLYURETHANE COLONELS, PUR, PU FASCIAS, BUMPERS
PUR/PC PUR/PC ALLOY TEXIN BUMPERS
PVC POLYVINYL CHLORIDE APEX, GEON, VINYLITE BODY MOLDINGS, WIRE
INSULATION, STEERING
WHEELS
RIM REACTION INJECTED
MOLDED POLYURETHANERIM, BAYFLEX FRONT FASCIAS, MODULAR
WINDOWS
RRIM REINFORCED REACTION
INJECTED MOLDEDPUR, RRIM FASCIAS, BODY PANELS,
BODY TRIMS
TPE THERMO POLYETHYLENE TPE, HYTREL, BEXLOY-V FASCIAS, BUMPERS,
CLADDINGS
TPO THERMOPOLYOLEFIN POLYTROPE, RENFLEX,
SANTOPRENE, VISAFLEX,
ETA, APEX, TPO, SHIELDS,
CLADDINGSBUMPERS, END CAPS,
TELCAR, RUBBER, STRIPS,
SIGHT, INTERIOR B POST
TPP THERMO-POLYPROPYLENE TPP BUMPERS
TPU THERMOPOLYURETHANE,
POLYESTERTPU, HYTREL, TEXIN,
ESTANEBUMPERS, BODY SIDE,
MOLDINGS, FENDERS,
FASCIAS
PANEL SECTIONING
If it is required to section a large panel for a plastic
repair, it will be necessary to reinforce the panel. To
bond two plastic panels together, a reinforcement
must overlap both panels. The panels must be “V’d” at
a 20 degree angle. The area to be reinforced should
be washed, then sanded. Be sure to wipe off any
excess soap and water when finished. Lightly sand or
abrade the plastic with an abrasive pad or sandpaper.
Blow off any dust with compressed air or wipe with a
clean dry rag.
When bonding plastic panels, follow repair material
manufacturers recommendations. Be sure that enough
adhesive has been applied to allow squeeze out and
to fill the full bond line. Once the pieces have been
brought together, do not move them until the adhesive
is cured. The assembly can be held together with
clamps, rivets, etc. A faster cure can be obtained by heating with a heat lamp or heat gun. After the parts have been
bonded and have had time to cure, rough sand the seam and apply the final adhesive filler to the area being
repaired. Smooth the filler with a spreader, wooden tongue depressor, or squeegee. For fine texturing, a small
amount of water can be applied to the filler surface while smoothing. The cured filler can be sanded as necessary
and, as a final step, cleanup can be done with soapy water. Wipe the surface clean with a dry cloth allowing time
for the panel to dry before moving on with the repair.

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DODGE RAM SRT-10 2006 Service Repair Manual PANEL REINFORCEMENT
Structural repair procedures for rigid panels with large
cracks and holes will require a reinforcement backing.
Reinforcements can be made with several applications
of glass cloth

PANEL REINFORCEMENT
Structural repair procedures for rigid panels with large
cracks and holes will require a reinforcement backing.
Reinforcements can be made with several applications
of glass cloth saturated with structural adhesive. Semi-
rigid or flexible repair materials should be used for
semi-rigid or flexible backing reinforcement and open
meshed fiberglass dry wall tape can be used to form a
reinforcement. The dry wall tape allows the resin to
penetrate through and make a good bond between the
panel and the adhesive. Structurally, the more dry wall
tape used, the stronger the repair.
Another kind of repair that can be done to repair large
cracks and holes is to use a scrap piece of similar
plastic and bond with structural adhesive. The rein-
forcement should cover the entire break and should
have a generous amount of overlap on either side of
thecrackedorbrokenarea.
When repairing plastic, the damaged area is first “V’d”
out, or beveled. Large bonding areas are desirable
when repairing plastic because small repairs are less
likely to hold permanently. Beveling the area around a
crack at a 20 degree angle will increase the bonding
surface for a repair. It is recommended that sharp
edges be avoided because the joint may show
through after the panel is refinished.
Panel repair for both flexible and rigid panels are
basically the same. The primary difference
between flexible panel repair and rigid panel
repair is in the adhesive materials used.
The technician should first decide what needs to
be done when working on any type of body
panel. One should determine if it is possible to
return the damage part to its original strength
and appearance without exceeding the value of
the replacement part.
When plastic repairs are required, it is recom-
mended that the part be left on the vehicle when ever possible. That will save time, and the panel will remain
stationary during the repair. Misalignment can cause stress in the repairareas and can result in future failure.

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DODGE RAM SRT-10 2006 Service Repair Manual VISUAL INSPECTION
Composite materials can mask the severity of an acci-
dent. Adhesive bond lines, interior structure of the
doors, and steel structures need to be inspected care-
fully to get a true

Page 4348 of 5267

DODGE RAM SRT-10 2006 Service Repair Manual PANEL PATCH FABRICATIONS
A patch can be fabricated from any rigid fiberglass
panel that has comparable contour with the repair
area. Lift gates and fenders can be used to supply
patch material. If exi

PANEL PATCH FABRICATIONS
A patch can be fabricated from any rigid fiberglass
panel that has comparable contour with the repair
area. Lift gates and fenders can be used to supply
patch material. If existing material is not available or
compatible, a patch can be constructed with adhesive
and reinforcement mesh (dry wall tape). Perform the
following operation if required:
1. Cover waxed paper or plastic with adhesive backed
nylon mesh (dry wall tape) larger than the patch
required.
2. Tape waxed paper or plastic sheet with mesh to a
surface that has a compatible contour to the repair
area.
3. Apply a liberal coat of adhesive over the reinforce-
ment mesh. If necessary apply a second or third
coat of adhesive and mesh after first coat has cured. The thickness of the patch should be the same as the
repair area.
4. After patch has cured, peel waxed paper or plastic from the back of the patch.
5. If desired, a thin film coat of adhesive can be applied to the back of the patch to cover mesh for added strength.
PANEL PATCH INSTALLATION
1. Make a paper or cardboard pattern the size and
shape of the cutout hole in the panel.
2. Trim 3 mm (0.125 in.) from edges of pattern so
patch will have a gap between connecting sur-
faces.
3. Using the pattern as a guide, cut the patch to size.
4. Cut scrap pieces of patch material into 50 mm (2
in.) squares to use as patch supports to sustain the
patch in the cutout.
5. Drill 4 mm (0.160 in.) holes 13 mm (0.5 in.) in from
edge of cutout hole.
6. Drill 4 mm (0.160 in.) holes 13 mm (0.5 in.) away
from edge of patch across from holes drilled
around cutout.
7. Drill 3 mm (0.125 in.) holes in the support squares
13 mm (0.5 in.) from the edge in the center of one
side.
8. Scuff the backside of the body panel around the cutout hole with a scuff pad or sandpaper.
9. Mix enough adhesive to cover one side of all support squares.
10. Apply adhesive to cover one side of all support squares.
11. Using number 8 sheet metal screws,secure support squares to back side of body panel with adhesive sand-
wiched between the panel and squares.

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DODGE RAM SRT-10 2006 Service Repair Manual 12. Position patch in cutout against support squares
and adjust patch until the gap is equal along all
sides.
13. Drill 3 mm (0.125 in.) holes in the support squares
through the pre-drilled holes in t

Page 4350 of 5267

DODGE RAM SRT-10 2006 Service Repair Manual 17. Using a 125 mm (5 in.) 24 grit disc grinder, grind
a50mm(2in.)to75mm(3in.)wideand2mm
(0.080 in.) deep path across the gaps around the
patch. With compressed air, blow dust from
around patch.
18. A

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DODGE RAM SRT-10 2006 Service Repair Manual SPECIFICATIONS
TORQUE
Description Nꞏm Ft. Lbs. In. Lbs.
A-pillar trim/grab handle bolts 6 — 55
Body Isolator/cab bolts 81 60 —
Cargo box bolts 108 80 —
Cargo box tie down/cleat bolts 34 25 —

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DODGE RAM SRT-10 2006 Service Repair Manual Description Nꞏm Ft. Lbs. In. Lbs.
Load floor/rear seat bolts 40 30 —
Lower seat belt anchor bolt - quad cab 40 30 —
Overhead/b-pillar grab handle bolts 6 — 55
Radiator and condenser to radiato

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