Textron Cessna 172R - Flight Load Factor Limits; Kinds of Operation Limits; Normal Category; Utility Category

SECTION
2
LIMITATIONS
CESSNA
MODEL
172R
FLIGHT
LOAD
FACTOR
LIMITS
NORMAL
CATEGORY
Flight
Load Factors
(Maximum
Takeoff
Weight
-
2450
lbs.):
‘Flaps
Up
+3.8g,
-1
.52g
‘Flaps
Down
+3.0g
‘The
design
load
factors
are
150%
of
the
above,
and
in
all
cases,
the
structure meets
or
exceeds
design
loads.
UTILITY
CATEGORY
Flight
Load Factors
(Maximum
Takeoff
Weight
-
2100
lbs.):
‘Flaps
Up
+4.4g,
-1
,76g
‘Flaps
Down
+3.0g
‘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
as
delivered
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
reference
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.
2-10
Revision
7
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