Piper SENECA III - Airspeed for Safe Operations

SECTION
4
PIPER
AIRCRAFT CORPORATION
NORMAL
PROCEDURES
PA-34-220T, SENECA III
4.3
AIRSPEEDS
FOR
SAFE
OPERATIONS
The
following
airspeeds
are
those
which
are
significant
to
the
operation
of
the
airplane.
These
figures
are
for
standard
airplanes
flown
at
gross
weight under
standard
conditions
at
sea
level.
Performance
for
a
specific airplane
may vary
from
published figures
depending
upon
the
equipment
installed,
the
condition
of
the
engine,
airplane
and
equipment,
atmospheric
conditions
and
piloting technique.
(a)
Best
Rate
of
Climb
Speed
92
KIAS
(b)
Best
Angle
of
Climb
Speed
76
KIAS
(c)
Turbulent
Air
Operating
Speed
(See
Subsection 2.3)
140 KIAS
(d)
Maximum Flap Speed
i15
KIAS
(e)
Landing Final
Approach
Speed
(Flaps
40°)
Short
Field
Effort 82 KIAS
(f)
Intentional
One
Engine lnoperative
Speed
85 KIAS
(g)
Maximum
Demonstrated
Crosswind
Velocity
17
KTS
REPORT:
VB-1110
ISSUED:
JANUARY
8,
1981
4-2