Piper SENECA III User Manual

APPLICABILITY
Application
of
this
handbook
is
limited
to
the
specific
Piper
PA-34-220T
model
airplane
designated by
serial number
and
registration
number
on
the
face
of the
title
page
of
this
handbook.
This
handbook
cannot
be
used for
operational
purposes
unless
kept
in
a
current
status.
REVISIONS
The
information
compiled
in the
Pilors
Operating
Handbook, with
the
exception
of
the
equipment
list,
will
be
kept
current
by
revisions distributed
to
the
airplane
owners.
The
equipment
list
was
current
at
the
tinie
the
air-
plane
was
licensed by
the
manufacturer
and
thereafter
must
be
maintained
by
the
owner.
Revision
material
will
consist
of
information
necessary
to
update
the
text
of
the
present
handbook
and/or
to
add
information
to
cover
added
airplane
equipment.
L
Revisions
Revisions
will
be
distributed
whenever
necessary
as
complete
page
replacernents
or
additions
and
shall
be
inserted
into
the
handbook in
accordance
with
the
instructions
given
below:
1.
Revision
pages
will
replace
only
pages
with
the
same
page
number,
2.
Insert
all
additional
pages
in
proper
numerical order
within
each
section.
3.
Page
numbers
followed by
a
small letter
shall be
inserted
in
direct
sequence
with
the
same
common
numbered
page.
IL
Identification
of
Revised
Material
Revised
text
and
illustrations
shall
be
indicated by
a
black
vertical
line
along
the
outside
margin
of
the
page,
opposite
revised,
added
or
deleted
material. A
line
along
the
outside
margin of
the
page
opposite the
page
number
will
indicate that
an
entire
page
was
added.
REPORT:
VB-1110
lii

Piper SENECA III Specifications

General

Manufacturer	Piper Aircraft
Model	Seneca III
Engine Type	Piston
Engine Model	Continental TSIO-360-KB
Seating Capacity	6
Cruise Speed	188 knots (216 mph, 348 km/h)
Length	28 ft 7 in (8.71 m)
Max Takeoff Weight	4, 750 lb (2, 155 kg)
Horsepower	220 hp each
Service Ceiling	25, 000 ft (7, 620 m)
Height	9 ft 11 in (3.02 m)
Propellers	2-bladed constant speed