Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTlON 9
PA-34-220T,
SENECA
III
SUPPLEMENT
7
OFF
or
if there
is
an
electrical
system
failure,
the
slave engine will
return to
the
controlled
selected
RPM plus
approximately
25
RPM
"out
of
syn-
chronization"
regardless
of
the
position of
the synchrophaser switch.
SECTION 5
-
PERFORMANCE
No
changes
to
the
basic
perforrnance
provided
by
Section
5
of this
Pilot's Operating
Handbook
are
necessary
for
this
supplement.
ISSUED:
JANUARY 8,
1981
REPORT:
VB-1110
3
of
4,
9-57

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