Parking; Tie-Down; Jacking; Flyable Storage - Cessna Hawk XP R172K Pilot Operating Handbook

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i
II
I
SECTION 8
HANDLING,
SERVICE
&
MAINTENANCE
CESSN!\
MODEL R17:~h
CJI';SSNA
M()DEL R172K
damage
to the gear will result.
If the airplane
is towed or pushe~
OVI'I
a rough
surface
during
hangaring,
watch that the normal
cushioning
action
of the nose strut does not cause excessive
vertical
movement
"I
the tail and the resulting
contact
with low hangar
doors or structure,
A flat nose tire or deflated
strut will also increase
tail height.
PARKING
When parking
the airplane,
head into the wind and set the parking
brakes.
Do not set the parking
brakes
during
cold weather
when ac-
cumulated
moisture
may freeze the brakes,
or when the brakes
are
overheated.
Install
the control
wheel lock and chock the wheels.
In
severe weather
and high wind conditions,
tie the airplane
down as out
lined in the following
paragraph.
TIE-DOWN
Proper
tie-down
procedure
is the best precaution
against
damage to
the parked
airplane
by gusty or strong winds.
To tie-down the ai rpl
am-
securely,
proceed
as follows:
(1) Set the parking
brake and install
the control
wheel lock.
(2) Install
a surface
control
lock over the fin and rudder.
(3) Tie sufficiently
strong
ropes
or chains
(700 pounds
tensile
strength)
to the wing, tail, and nose tie-down
fittings
and secure
each rope to a ramp
tie-down.
(4) Install
a pitot tube cover.
JACKING
When a requirement
exists
to jack the entire airplane
off the
ground,
or when wing jack points
are used in the jacking
operation,
refer to the Service
Manual
for specific
procedures
and equipment
re-
quired.
Individual
main gear may be jacked
by using the jack pad which is
incorporated
in the main landing
gear strut step bracket.
When using
the individual
gear strut jack pad, flexibility
of the gear strut will
cause the main wheel to slide inboard
as the wheel is raised, tilting
the
jack.
The jack must then be lowered
for a second jacking
operation.
Do not jack both main wheels
simultaneously
using the individual
main gear jack pads.
If nose gear maintenance
is required,
the nose wheel may be raised
off the ground
by pressing
down on a tailcone
bulkhead,
just forward
of
the horizontal
stabilizer,
and allowing
the tail to rest on the tail tie-
down ring.
8-8
: ;1':( "I'ION
8
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III
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I tv I ell;
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N /\ Nell;
NOTE
Do not apply pressure
on the elevator
or
r u r
t.l
u r.r
r
r
l
';1;11,,1
izer surfaces.
When pushing
on the ta.i
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Co
III',
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IV
iI\',
apply pressure
at a bulkhead
to avoid
bucl\IIIII',
II"
,1'"1
To assist
in raising
and holding
the nose wheot
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l.lu
1',1""1111
wuight down the tail by placing
sand-bags,
or
suitub!«
1"1'11',111'
""'
",I,
ulde
of the horizontal
stabilizer,
next to the Iu se larro.
"1',11,'"11<1,11
-hors are available,
the tail should
be securely
tied
<I0WII
NOTE
Ensure
that the nose will be held off the ground
1I11dl'l'
;i11
conditions
by means
of suitable
stands
or support«
11111 1",
weight
supporting
bulkheads
near the nose of tho n.i
J'
plane.
LEVELING
Longitudinal
leveling
of the airplane
is accomplished
by
i'
I;
Ii
I
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,I
level on leveling
screws
located
on the left side of the ta.i loo
I" ,11.,1,
1.118
nose tire and/or
lower or raise
the nose strut to properly
':"111,'1
II",
bubble in the level.
Corresponding
points
on both upper doo r
::111::
111.1\
be used to level the airplane
laterally.
FLYABLE STORAGE
Airplanes
placed
in non-operational
storage
for a rna.x
i
11111111" I
:II
days or those which receive
only intermittent
operational
11::"
1101 II".
first 25 hours
are considered
in flyable
storage
status.
EVl'r,\'
::1'"
11111
day during
these periods,
the propeller
should
be rotated
".\I I,,, 11<1
through
five revolutions.
This action
"limbers"
the oil
alld
1""'"
'III',
any accumulation
of corrosion
on engine
cylinder
walls,
IWARNING)
For maximum
safety,
check that the ignition
sw
i l.ch
I',
OFF, the throttle
is closed, the mixture
control
i:; III
1111
idle cut-off position,
and the airplane
is secured
I
JC'
I" '"
rotating
the propeller
by hand.
Do not stand w
i t.hu
i
II"
arc of the propeller
blades while turning
the p
J'(
'I
JC'
II,
'I
After 30 days, the airplane
should
be flown for 30
1111II III,..,
"I
,I
ground
runup
should
be made just long enough
to
produ.« ""
",I
temperature
within
the lower green arc range,
Excosxi v.:
1',I""lId
11111

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