PIPER AIRCRAFT CORPORATION SECTION 7
PA-28-161, WARRIOR II DESCRIPTION & OPERATION
7.33
PIPER
EXTERNAL POWER*
An
optional
starting
installation known as
Piper
External
Power(PEP)
is
accessible
through
a receptacle located
on
the right side
of
the fuselage.
forward
of
the wing. An external battery
can
be connected
to
the socket, thus
allowing the
operator
to
crank
the engine without having
to
gain access to
the airplane's battery. Instructions on a placard located
on
the
cover
of
the
receptacle should be followed before using the external power.
For
instruc-
tions on the use
of
the
PEP
see
STARTING
WITH
EXTERNAL
POWER
SOURCE
in Section
4-
Normal
Operating
Procedures.
7.35 EMERGENCY LOCATOR TRANSMITTER*
The
Emergency
LocatorTransmitter(EL
T). when installed.
is
located
in
the aft
portion
of
the
fuselage
just
below the
stabilator
leading edge and
is
accessible
through
a plate
on
the right side
of
the
fuselage. This plate
is
attached with slotted-head nylon screws for ease
of
removal; these screws
may be readily removed with a variety
of
common
items such as a dime. a
key, a knife blade, etc. If there are no tools available in
an
emergency. the
screw heads may be
broken
off by any means.
TheEL
T meets the require-
ments
of
FAR
91.52.
A battery replacement
date
is
marked
on
the
transmitter
to comply with
FAA
regulations. the battery must be replaced
on
or
before this date. The
battery must also be replaced if the transmitter has been used in
an
emergency
situation
or,
if the accumulated test time exceeds
one
hour,
or
if the unit has
been inadvertently activated for
an
undetermined time period.
NOTE
If for
any
reason a test transmission is
necessary,
the
test transmission should be
conducted only
in
the first five minutes
of
any
hour
and
limited to three
audio
sweeps.
If
the
tests must be made
at
any
other time, the tests
should
be coordinated with the nearest
FAA
tower
or
flight service station.
*Optional
equipment
ISSUED: AUGUST 13,
1982
REVISED: JULY 15,
1983
REPORT:
VB-1180
7-23