Specifications

CHEROKEE SIX.3OO
E.
AIRSPEED
LIMITATIONS
AND
AIRSPEED INSTRUMENT
MARKINGS
(Calibrated
Airspeed)
F. MAXIMUM WEIGIIT 34OO
LBS
G. C. G. RANGE
The datum
used is
78.4 inches
ahead
of
the wing leadins
edge
at the intersection of
the
straight and
tapered section.
NEVER
EXCEED
MAXIMUM
STRUCTURAL CRUISE
MANEUVERTNG
FLAPS EXTENDED
MAXIMUM
POSITIVE
LOAD
FACTOR
MAXIMI.JM
NEGATIVE LOAD
FACTOR
AIRSPEED
INSTRUMENT
MARKINGS
Red
Radial
Line
(Never-Exceed)
Yellow
Arc
(Caution
Range)
(Smooth
Air
Only)
Green Arc
(Normal
Operating Range)
White
Arc
(Flap
Down)
2I2MPH
I68 MPH
I49 MPH
125
MPH
3.8
No inverted
maneuvers
approved
ZI?MPH
(184
KTS)
168
MPH to
212
MPH
(146
KTS to
184
KTS)
7l
MPH to 168 MPH
(62
KTS to
146
KTS)
63 MPH
to
125
MPH
(55
KTS
to
109 KTS)
Rearward
Limit
(In.
Aft
of Datum)
95.5
96.2
96.2
96.2
Weight
(Pounds)
3400
3300
2904
2400
Forward Limit
(In.
Aft of
Daturn)
91.4
89.0
80.0
76.0
Straight line
variation
between
points
given.
NOTE
It is
the responsibility
of
the
airplane
owner
insure
that
the airplane
is
properly
loaded.
Balurce Section
for
proper
loading
instructions.
H.
MANEIIVERS
No
acrobatic
maneuven
including
spins
approved.
REPORT: VB-562
PAGE
3-2
MODEL:
PA-32-300
and
the
pilot
to
See
Weight
and
FAA APPROVED
MAY
14,1973