Piper SENECA III - The same

PIPER
AIRCRAFT
CORPORATION
SECTION
I
PA-3&220T,
SENECA
III
GENERAL
Wind
The
wind velocities
recorded
as
variables
on
the charts of this
handbook
are
to
be
understood
as
the
headwind
or
tailwind
components
of
the
reported
winds.
(c)
Power
Terminology
Takeoff
Power
Maximum
power
permissible for
takeoff.
Maximum
Con-
Maximumpowerpermissiblecontinuously
tinuous
Power
during flight.
Maximum
Climb
Maximum
power
permissible during
Power
climb.
Maximum
Cruise
Maximum
power
permissible
during
Power
cruise,
(d)
Engine Instruments
EGT
Gauge
Exhaust
Gas Temperature Gauge
(el
Airplane
Performance
and
Flight
Planning Terminology
Climb
Gradient
The demonstrated
ratio
of
the change
in
height
during
a
portion
of
a
climb,
to
the
horizontal
distance
traversed
in
the
same
time
intervaL
Demonstrated
The
demonstrated
crosswind
velocity
isthe
Crosswind
velocity
of
the
crosswind
component
for
Velocity
which
adequate
control
of
the
airplane
(DE
MO
during
takeoff
and
landing
was
actually
X-WlND)
demonstrated
during
certification
tests.
Accelerate-Stop
The distance
required
to
accelerate
an
air-
Distance
plane
to
a
specified
speed
and.
assuming
failure
of
an
engine
at
the
instant
that
speed
is
attained,
to
bring
the
airplane
to
a
stop.
ISSUED:
JANUARY 8,
1981
REPORT:
VB-IIIO
1-9