
4-1
SECTION IV
DISASSEMBLY
4-1. GENERAL. .
4-2. AIRCRAFT PARTS AND ACCESSORIES.
4-3. Instructions in this section are based on the
assumption that all parts attached by the aircraft
manufacturer, except optional pumps, have been
removed.
4-4. Accessories supplied by the engine manufacturer
may be serviced according to instructions supplied by
the applicable accessory manufacturer.
4-5. EXTENT OF DISASSEMBLY. Line drawings
reproduced in this section are identical to those used
in the parts catalog, except for order of index numbers
assigned to components. Index numbers herein
indicate the order of disassembly. In many instances
the location of components and attaching parts in the
illustration will be sufficient to enable personnel to
accomplish disassembly operations. In such instances
such disassembly is to be accomplished, even though
there are no printed instructions to that effect,
excepting those parts which need to be removed only
for replacement. Such parts include studs, bushings,
and other tight fit inserts. The identity of these will be
obvious.
4-6. PARTS TO BE DISCARDED. Discard all
shakeproof washers, lockwires, tab washers, rubber
seal rings, oil seals, gaskets, cotter pins, hose
connectors and magneto coupling (rubber) bushings in
such manner that they will not be used again
inadvertently. Care should be taken in removing
gaskets from aluminum parts by scraping. Such
removal should be delayed until the part is to be
cleaned.
4-7. DISASSEMBLY STAND. For greatest ease of
disassembly, this engine should be mounted on an
engine stand with a tilting bed. See the installation
drawings for necessary dimensions for mounting
engine on stand.
4-8. PRELIMINARY CLEANING. Spray, or apply
with a brush, a solvent used for general cleaning of
engine parts. Remove caked dirt on bolt heads and
nuts especially. At the same time the oil sump drain
plugs should be removed to drain any remaining oil.
CAUTION
Do not use a caustic or even mild
alkaline cleaning solution for external
pre-cleaning, as these solutions will also
remove the "alodized" finish of certain
aluminum parts.
4-9. DISMANTLING.
4-10. IGNITION SYSTEM.
a. Disconnect cables from spark plugs.
b. Detach ignition cable retaining clamps from fuel
discharge brackets.
c. Detach clip from cable bracket on top of crankcase.
Disengage band clamps.
d. Detach high tension cable outlet plates from
magnetos and withdraw them to free cable assemblies.
e. Remove two attaching nuts, lockwashers and
holding washers from each magneto. Withdraw
magnetos forward from the crankcase.
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