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PIPER AIRCRAFT CORPORATION
SECTION 2
PA-28R-201T,
CHEROKEE
TURBO ARROW III
LIMITATIONS
SECTION 2
LIMITATIONS
2.1 GENERAL
This
section provides
the
"FAA Approved"
operating
limitations, instrument
markings, color coding
and basic
placards necessary
for
the
safe operation of
the
airplane and
its
systems.
Limitations
associated
with
those
optional
systems
and
equipment
which
require
handbook
supplements
can
be found in Section
9
(Supplements).
2.3 AIRSPEED LIMITATIONS
SPEED
KIAS
KCAS
Never
Exceed
Speed
(VNE)
-
Do
not exceed
this
speed
in
any operation.
183
186
Maximum
Structural
Cruising
Speed
GNo)
-
Do
not
exceed
this
speed except in smooth
air
and
then
only
with caution.
146
148
Design Maneuvering Speed
(VA)
-
Do
not make
full
or
abrupt
control movements
above
this
speed.
At 2900 LBS. G.W.
119
121
At
1865
LBS. G.W.
96
96
CAUTION
Maneuvering
speed
decreases
at
lighter
weight as
the
effects of
aerodynamic
forces
become
more
pronounced.
Linear
interpolation
may
be
used
for
intermediate
gross
weights.
Maneuvering
speed should
not be exceeded
while operating
in
rough air.
Maximum
Flaps Extended Speed
(VFE)
-
Do
not exceed
this
speed with
the
flaps
extended.
103
104
Maximum Landing
Gear Extension Speed
-
Do
not exceed
this
speed when extending
the
landing gear.
129
130
Maximum Landing
Gear Retraction Speed
-
Do not
exceed
this
speed when retracting
the
landing gear.
107
109
Maximum Landing
Gear Extended Speed
(Vu)
-
Do not
exceed
this
speed with
the
landing gear extended.
129
130
ISSUED:
DECEMBER
20, 1976
REPORT:
VB-800
2-1
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