Piper SENECA III User Manual

SECTION
4
PIPER
AIRCRAFT
CORPORATION
NORMAL
PROCEDURES
PA-34-220T,
SENECA
Ill
4.59
STALLS
The
loss
of altitude
during
a
power
off
stall
with
the
gear
and
flaps
retracted
may
be
as
much
as
400
feet.
The
loss
of
altitude
with
the
gear
down
and
40°
of
flaps
may
also be
as
much
as
400
feet.
A
power
on
stall
may
result
in
as
much
as
150 feet
of altitude
loss.
The
stall
warning
system
is
inoperative
with
the battery
switch
OFF.
REPORT:
VB-III0
ISSUED:
AUGUST 17, 1981
4-38

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