Piper cherokee WARRIOR - ENGINE SHUTDOWN AND SECURING; Engine Shutdown and Securing Procedures

CHEROKEE
WARRIOR
STOPPING
ENGINE
At the
pilot's
discretion,
the
flaps should
be raised
and the electric
fuel
pump
turned off.
After
parking.
the
radios
should
be
turned off
and the
engine stopped by
putting
the
mixture
control
in
idle cut-off. The
throttle
should be
left
full
aft to avoid
engine
vibration
while
stopping.
-fhe
magneto
and master
switches
should
be turned off arrd the
parking
brake set.
AIRSPEED DATA
All airspeeds
quoted
in this
manual are calibrated
unless
otherwise
noted. Calibrated
airspeed
is indicated
airspeed corrected
for instrument and
position
errors. The
following table
gives
the correlation
between
indicated
airspeed and calibrated airspeed if zero instrument
error
is assumed.
This calibration is
valid only
when
flown at maximum
gross
weight in level
flight.
AIRSPEED CORRECTION
TABLE
Flaps
0
"
IAS
-
MPH
CAS
-
MPH
Flaps
40
o
IAS
-
MPH
CAS
-
MPH
135t26lt7108
99
82
66
110
80
t0798
89
8l
65
80
60
70
74
70
73
90
90
90
150
140
130t2Qr10
r00
t44
60
100
MOORING
The
airplane
can be
moved on the
ground
with thc ajd of the optiorral nose whecl
tow bar
stowed in the baggage compartment.
Tie-down ropi-s may be
attached to
rings
under each wing
and
to the tail skid. The
aileron and stabilator
controls should
be
secured by looping
the seat
belt through the control
wheel and
pulling
it snug. The
rudder is
held
in
position
by' its
connection to the
nose
wheel steeriug and normally does
not have to be
secured. The
flaps are
locked
when
in the
full
up
position
and should
be left retracted.
WEIGHT
AND
BALANCE
It is the
responsibility
of the owner
and
pilot
to determine
that
the airplane
remains
within
thc allowable
weight vs.
center
of
gravitl'
etrvelope while in flight.
For weight
and
balance data,
see the
Weieht
and Balance Section
of this
manual.
OPERATING
IN
STRUCTI
ONS
REVISED: JULY
14.1975
7-9