Cessna R182 - Page 17

CESSNA
MODEL
11182
CENTER
OF GRAVITY
LIMITS
SECTION
2
LIMITATIONS
Center
of
Gravity
Range:
Forward: 33.0 inches aft of datum
at 2250,1b9;,
or less,
with
gtraigh!
line
variation to
35.5 inches,aft of datum
at 27(X)
lbs., with straight
line
variation
to
40.9 inches aft
of datum
at
3100
lbs.,
Aft:
4?.0 inches
aft of datum
at all
weights.
'
'
I
,
,
Moment Change
Due To Retracting
Landing
Geari
+3052
lb.-ins.
Reference
Datum:
Front,face'of
firewall.
:
'
MANEUVER
LIMITS
This airplane
is certificated
in the
norlna-I.
gategory.
Thp
normal
category is
applicable
to aircraft
intended
foi
non-aerobatic
operations.
These
include &ny
maneuvers
ineidental
to
normal
flying, staus
(excePt
whip stalls),lazy
eights, chandelles,
and steep
tutns
in which the angle
of
bank is not more
tJran 600.
Aerobatic
maneuvers,
including spins,
a,re
not approved.
FLIGHT
LOAD
FACTOR
LIMITS
Flight
Load Factors:
*Flaps
Up:
+3.89,
-1.529
*FlaPs
Down:
+2.0g
*The
design
load factors
are tSwo
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-
ence
to types
of
flight operations
on
the operating
limitations
placard
reflects equipment
installed
at
the time
of
Airworthiness
Certificate
issuance.
Flight
into known
icing conditions
is
prohibited.
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