Sea-Doo GTX Limited iS 2009 Инструкция по эксплуатации онлайн [21/555] 12053

Sea-Doo GTX Limited iS 2009 Инструкция по эксплуатации онлайн [21/555] 12053
INTRODUCTION
3. Twist bolt when inserting it to improve thread
conformation.
NOTE: NOT intended for engine stud repairs.
Repair of Small Holes/Fine Threads
Option 1: Enlarge damaged hole, then follow
STANDARD THREAD REPAIR
procedure.
Option 2: Apply FORM-A-THREAD on the screw
and insert in damaged hole.
Permanent Stud Installation (Light Duty)
1. Use a stud or thread on desired length.
2. DO NOT apply release agent on stud.
3. Do a STANDARD THREAD REPAIR.
4. Allow to cure for 30 minutes.
5. Assemble.
Gasket Compound Application
21
1
3
1
lmr2007-040-006_a
1. Proper
strength Loctite
2. Loctite Primer N (P/N 293 800 041) and Gasket Eliminator 518
(P/N 293 800 038) on both sides of gasket
3. Loctit
e Primer N only
1. Remove old gasket and other contaminants
with
LOCTITE CHISEL (GASKET REMOVER)
(P/N 413 708 500)
. Use a mechanical mean
if necessary.
NOTE:
Avoid grinding.
2. Clean both mating surfaces with solvent.
3. Spray Loctite Primer N on both mating surfaces
and on both sides of gasket. Allow to dry 1 or
2 minutes.
4. Appl
y
LOCTITE 518 (P/N 293 800 038) on both
side
s of gasket, using a clean applicator.
5. Place gasket on mating surfaces and assemble
immediately.
NOTE: If the cover is bolted to blind holes (above),
apply proper strength Loctite in the hole and on
threads. Tighten.
If holes are sunken, apply proper strength Loctite
on bolt threads.
6. Tighten as usual.
Threadlocker Application for Mounting
on Shaft
Mounting with a Press
A00A3UA
1
2
3
1. Bearing
2. Proper strength Loctite
3. Shaft
1. Clean sha
ft external part and element internal
part.
2. Apply a strip of proper strength Loctite on shaft
circumference at insert or engagement point.
NOTE: Retaining compound is always forced out
when applied on shaft.
3. DO NOT us
e antiseize Loctite or any similar
product
.
4. No curing period is required.
Mounting in Tandem
1. Apply r
etaining compound on internal element
bore.
2. Continue to assemble as shown above.
XVIII smr2009-011
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