M ANEUVERS
-
UT
I
LI
TY C
A
TEGOR
Y.
necessary.
Also,
plan
an
inspection
by
your Dealer
at 100
hours
or 180
days,
whichever
comes
first.
This inspection also
is performed
by
your
This
airplane
is not
designed
for purely
aerobatic flight.
However,
Dealer for
you
at
no charge.
While these
important
inspections
will
be
in
the
acquisition
of various
certificates such
as commercial
pilot,
in-
performed
for you by
any
Cessna Dealer,
in
most cases
you
will prefer
strument
pilot and
flight
instructor,
certain
maneuvers
are required
by
to
have the
Dealer from
whom
you purchased the airplane
accomplish
the FAA.
All
of
these
maneuvers
are permitted
in
this
airplane when
this work.
operated in
the
utility
category. In connection
with the
utility
category,
the following
gross weight
and
flight
load factors apply,
with
maximum
Federal
Aviation Regulations
require that all airplanes
have a
peri-
entry speeds
for
maneuvers
as
shown: odic
(annual)
inspection
as
prescribed by the
administrator, and
per-
formed
by a
person designated
by
the
administrator.
In
addition,
100-
Gross Weight
.
.
. - -
. .
. .
.
.
.
.
.
.
.
. 2000
lbs
hour periodic
inspections made
by
an
"appropriately-rated
mechanic"
Flight
Maneuvering Load
Factor
are required
if
the airplane is flown for
hire. The
Cessna Aircraft
Flaps
Up . . . . .
. . .
. .
.
. .
.
.4.4
-1.76
Company
recommends
the
100-hour
periodic
inspection
for your
air-
Flaps Down
. . . .
.
.
. . . . .
.
.
.+3.5 plane.
The procedure for this
100-hour
inspection has
been
carefully
worked
out by
the
factory
and
is
followed
by
the
Cessna
Dealer
Organ-
In
the
utility
category,
the
baggage compartment
and
rear seat must
ization.
The complete familiarity
of
the Cessna
Dealer
Organization
not
be
occupied.
No
aerobatic
maneuvers are
approved
except
those
list-
with Cessna
equipment
and with
factory-approved
procedures
provides
ed
below:
the
highest type of
service
possible
at
lower cost.
MANEUVER
MAXIMUM
ENTRY
SPEED
Chandelles . . . . . . .
.
.
.
. .
.
. .
.
122
mph
(106
knots)
Lazy
Eights . . .
.
. . . .
.
. . . . . .
122
mph
(106
knots)
Steep Turns . . .
.
. . . .
. .
. . . . .
122
mph (106
knots)
Spins................... SlowDeceleration
Stalls
(Except
Whip Stalls)
.
.
. .
. . . . . . Slow
Deceleration
Aerobatics that may
impose
high inverted loads
should
not be
attempt-
ed.
The important
thing
to bear in mind
in
flight maneuvers
is
that the
airplane
is
clean
in
aerodynamic design
and
will build
up
speed quickly
with
the
nose down.
Proper speed
control is an
essential requirement
for
execution of
any maneuver,
and care should always be exercised
to
avoid excessive speed
which
in turn
can
impose
excessive
loads. In the
execution of all
maneuvers,
avoid abrupt
use of
controls.
AIRSPEED
LIMITATIONS
(CAS).
The
following
is
a
list
of the
certificated
calibrated airspeed (CAS)
limitations for the airplane.
Never Exceed Speed
(glide
or
dive,
smooth
air) . . . . 174
MPH
Maximum
Structural
Cruising
Speed . . . . . . . .
. 140
MPH
4-5
3-2
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