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Cessna Hawk XP - Power Plant Instrument Markings; Center of Gravity Limits; Weight Limits

Cessna Hawk XP
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SECTION
2
LIMIT
A
TIO
NS
CESSNA
MODEL
R172K
POWER
PLANT
INSTRUMENT
MARKINGS
Power
I?lar:t
instrument
markings
and
their
color
code
significance
are
shown
in
figure
2-3.
RED LINE
GREEN ARC
RED
LI
NE
INSTRUMENT
MINIMUM
NORMAL
MAXIMUM
LIMIT
OPERATING
LIMIT
Tachometer - - -
2200 -
2600
RPM
2600
RPM
Manifold
Pressure
- - -
15 - 25
- - -
in.
Hg
11
Oil Temperature - - -
100°
-
240°F
240°F
Cylinder
Head
- - -
300°
-
460°F
460°F
I
Temperature
Fuel
Flow
(Pressure)
(3
psi)
4.5 - 11.5 gal/hr
17
gal/hr
(17
psi)
Oil
Pressure
10
psi
30 - 60
psi
100
psi
Figure
2-3.
Power
Plant
Instrument
Markings
WEIGHT
LIMITS
NORMAL
CATEGORY
Maximum
Takeoff
Weight:
2550
lbs.
Maximum
Landing
Weight:
2550
lbs.
Maximum
Weight
in
Baggage
Compartment:
Baggage
Area
1
(or
passenger
on
child's
seat)-Station
82
to
2-6
108: 200
lbs.
See
note
below.
Baggage
Area
2 -
Station
108
to
142: 50
lbs.
See
note
below.
NOTE
The
maximum
combined
weight
capacity
for
baggage
areas
1
and
2
is
200
lbs.
r
~
I.
I
l
CESSNA
MODEL
R172K
SECTION
2
LIMIT
A
TIO
NS
UTILITY
CATEGORY
Maximum
Takeoff
Weight:
2200
lbs.
Maximum
Landing
Weight:
2200
lbs
.
Maximum
Weight
in
Baggage
Compartment:
In
the
utility
category,
the
baggage
compartment
and
rear
seat
must
not
be
occupied.
CENTER OF
GRAVITY
LIMITS
NORMAL
CATEGORY
Center
of
Gravity
Range:
Forward:
35.0
inches
aft
of
datum
at
1950
lbs.
or
less
,
with
straight
line
variation
to
41.0
inches
aft
of
d'
atum
at
2550
lbs.
Aft: 47.3
inches
aft
of
datum
at
all
weights.
Reference
Datum:
Lower
portion
of
front
face
of
firewall.
UTILITY
CATEGORY
Center
of
Gravity
Range:
Forward:
35.0
inches
aft
of
datum
at
1950
lbs.
or
less,
with
straight
line
variation
to
37.5
inches
aft
of
datum
at
2200
lbs.
Aft: 40.5
inches
aft
of
datum
at
all
weights.
Reference
Datum:
Lower
portion
of
front
face
of
firewall.
MANEUVER
LIMITS
NORMAL
CATEGORY
This
airplane
is
certificated
in
both
the
normal
and
utility
catego-
ry.
The
normal
category
is
applicable
to
aircraft
intended
for
non-aero-
batic
operations.
These
include
any
maneuvers
incidental
to
normal
flying
,
stalls
(except
whip
stalls),
lazy
eights,
chandelles,
and
turns
in
which
the
angle
of
bank
is
not
more
than
60°.
Aerobatic
maneuvers
,
including
spins,
are
not
approved.
UTILITY
CATEGORY
This
airplane
is
not
designed
for
purely
aerobatic
flight.
Howev
er,
in
the
acquisition
of
various
certificates
such
as
commercial
pilot
,
in-
strument
pilot
and
flight
instructor,
certain
maneuvers
are
required
by
the
FAA
.
All
of
these
maneuvers
are
permitted
in
this
airplane
when
operated
in
the
utility
category.
2-7

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