Cessna 152 - Page 20

SECTION
2
LIMITATIONS
CESSNA
MODEL
152
Aft: 36.5
inches
aft
of
datum
at
all
weights.
Reference
Datum:
Front
face
of
firewall.
MANEUVER
LIMITS
This
airplane
is
certificated
in
the
utility
category
and
is
designed
for
limited
aerobatic
flight.
In
the
acquisition
of
various
certificates
such
as
commercial
pilot
and
flight
instructor,
certain
maneuvers
are
required.
All
of
these
maneuvers
are
permitted
in
this
airplane.
No
aerobatic
maneuvers
are
approved
except
those
listed
below:
MANEUVER
Chandelles
.
Lazy
Eights
Steep
Turns
Spins
Stalls
(Except
Whip
Stalls)
RECOMMENDED
ENTRY
SPEED*
.95
knots
.95
knots
.95
knots
.
Use
Slow
Deceleration
.
Use
Slow
Deceleration
*Higher
speeds
can
be
used
if
abrupt
use
of
the
controls
is
avoided.
The
baggage
compartment
and/
or
child's
seat
must
not
be
occupied
during
aerobatics.
Aerobatics
that
may
impose
high
loads
should
not
be
attempted.
The
important
thing
to
bear
in
mind
in
flight
maneuvers
is
that
the
airpla:p.e
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.
FLIGHT LOAD FACTOR LIMITS
Flight
Load
Factors:
*Flaps
Up: +4.4g, -1.76g
*Flaps
Down:
+3.5g
*The
design
load
factors
are
150%
of
the
above,
and
in
all
cases,
the
structure
meets
or
exceeds
design
loads.
KINDS
OF OPERATION LIMITS
The
airplane
is
equipped
for
day
VFR
and
may
be
equipped
for
night
VFR
and/or
IFR
operations.
FAR
Part
91
establishes
the
minimum
required
instrumentation
and
equipment
for
'these
operations.
The
refer-
2-6 1
July
1978