Piper SENECA III User Manual

SECTION
5
PIPER
AIRCRAFT
CORPORATION
PERFORMANCE
PA-34-220T,
SENECA
HI
The
information
provided
by
paragraph 5.5
(Flight Planning
Example)
outlines
a
detailed
flight
plan
using
the
performance
charts
in
this
section.
Each
chart
includes
its
own
example
to
show
how
it is
used.
WARNING
Performance
information
derived
by
extrapo-
lation
beyond the
limits shown
on
the
charts
should
not
be
used
for flight
planning
purposes.
REPORT:
VB-Ill0
ISSUED:
JANUARY
8, 1981
5-2

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