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Piper Comanche PA-24 User Manual

Piper Comanche PA-24
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PIPER COMANCHE SERVICE MANUAL
FIGURE
7-17. REMOVING SEIZED SPARK PLUG
NOTE
Spark
plugs
should
not
be
used
if
they
have
been
dropped.
d.
Removal
of
seized
spark
plugs in
the
cylinder
may
be
accomplished
by
application
of
liquid
carbon
dioxide
by a conical
metal
funnel
adapter
with
a
hole
at
the
apex
just
large
enough
to
accomodate
the
funnel
of
a
C02
bottle.
(Refer
to
Figure
7-17.)
When
a seized
spark
plug
cannot
be
removed
by
normal
means.
the
funnel
adapter
is
placed
over
and
around
the
spark
plug.
Place
the
funnel
of
the
C02
bottle
inside
the
funnel
adapter
and
release
the
carbon
dioxide
to
chill
and
contract
the
spark
plug.
Break
the
spark
plug
loose
with
a
wrench.
A
warm
cylinder
head
at
the
time
the
carbon
dioxide
is
applied
will
aid
in
the
removal
of
an
excessively seized plug.
e.
Do
not
allow
foreign
objects
to
enter
the
spark
plug
hole.
7-51.
Inspection And Cleaning
Of
Spark Plug. .
a. Visually inspect
each
spark
plug
for
the
following
non-repairable
defects:
I. Severely
damaged
shell
or
shield
threads
nicked
up.
stripped
or
cross-threaded.
2.
Badly
battered
or
rounded
shell
hexagons.
3.
Out-of-around
or
damaged
shielding
barrel.
4.
Chipped.
cracked.
or
broken
ceramic
insulator
portions.
5.
Badly
eroded
electrodes
worn
to
approximately
50%
of
original
size.
b.
Clean
the
spark
plug
as
required.
removing
carbon
and
foreign
deposits.
c. Test the
spark
plug
both
electrically
and
for
resistance.
d.
Set
the
electrode
gap
at
.015
to
.018
of
an
inch
or
if a
smoother
operation
at
idle
speed
and
reduced
magneto
drop-off
is
desired.
set
at
.018
to
.022
of
an
inch.
However.
with
wide
gap
setting
the
plugs
must
be
serviced
at
more
frequent
intervals.
Fine
wire
platinum
or
iridium
electrodes
should
be
set
at
.015
to
.018
of
an
inch only.
ISSUED: 8/18/72
2B17
POWER PLANT

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Piper Comanche PA-24 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelComanche PA-24
TypeLight aircraft
First FlightMay 24, 1956
Number Built4, 857
Seating Capacity4
EngineLycoming O-360
Wingspan36 ft (11 m)
Length24 ft 8 in (7.5 m)
Stall Speed62 mph (100 km/h, 54 kn)
Height7 ft 6 in (2.3 m)

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