Cessna 172P - Flight Load Factor Limits

insh¡otor,
certain
maneuvers
are
requlred
by tJre F,AA.
AU
of tJrese
ma,neuvgr8
are
pemltted
in
thls
allplane
wheu operated
in
the utirity
oategory.
In
the
utility
category,
the baggage
compartment
aud rear
seat must
not be
ocoupied-
No aerobatic
ma,neuvers
a,ro
epproved
except
thoge listed
þelow:
MANEUVEA,
RECOMMENDED
ENTR,Y
SPEED"
SECTION
2
LIMITATIONÞ
Flight
Load Factors
*Flaps
Up
rFlaps
Down
Clrandelles
Lazy
Eights
. .
Steep Turne
Spins
Stalls
(Except
\llhtp
Stalls)
CE88NA
MODEL 173P
. 10õ
knots
.
10õ knots
: : : : : : :
: dr.*ol*T3"*åti
.
Slow
Deoeleration
'Abrupt
use
of
the
controle
ie
prohibited
above
gg
knots.
a,ny
ma,neuver,
and care
should
always
be exercised to
avoid
excessive
speed which
in turn
can impose exceseive
loads. In
the execution
of
all
m&neuvers,
avoid abrupt use of
controls.
Intentional
spins
with
flaps
extended
are
prohibited.
FLIGHT LOAD
FACTOR LIMITS
NOBMAL
CATEGORY
Flight
Load Faotors
(Maximum
Takeoff
Weight
-
2400lbs.):
iFlaps
Up .
+3.89,
-1.õ2g
'Flaps
Down
.
+3.09
*The
design load factore are LóOVz of tJre
&bove, and in
all cases, the
structure meets or exceeds design
loads.
UTILITY
CATEGORY
Íï"i'TTi
1T":",T"'.'1',
. '..'o.o
lbe.):
+4.49,
-L.769,
+3,09
tThe
desiga load factors
are L6OVo
of the above, and in
all cases, the
structure meots
or exoeeds design
loade.
2-8
80
May
1980