Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION
1
PA-34-220T,
SENECA
III
GENERAL
l.3
ENGINE
(a)
Number
of
Engines
2
(b)
Engine
Manufacturer
Continental
(c)
Engine Model
Number
(1)
Left
TSIO-360K B
(2)
Right
LTSlO-360KB
T.O.
Power
Max. Cont.
5
Min. Limit
Power
(d)
Rated
Horsepower
220 BHP 200
BHP
(e)
Rated
Speed
(rpm)
2800
2600
(f)
Bore
(inches)
4.438
(g)
Stroke
(inches)
3.875
(h)
Displacement
(cubic
inches)
360
(i)
Compression
Ratio
7.5:1
(j)
Engine
Type
Six Cylinder,
Direct
Drive,
Horizontally
Opposed,
Air
Cooled
1.5
PROPELLER
STANDARD
ta)
Number
of
Propellers
2
(b)
Propeller
Manufacturer
Hartzell
(c)
Propeller
Hub
&
Blade
Models*
(1)
Left
BHC-C2YF-2CKUF|
FC8459-8R
(2)
Right
BHC-C2YF-2CLKUF|
FJC8459-8R
(d)
Number
of
Blades
2
(e)
Propeller
Diameter
(in.)
(1)
Maximum
76
(2)
Minimum
75
(f)
Propeller
Type
Constant Speed.
Hydraulically
Activated.
Full
Feathering
*The
propellers
have
the
same
designation
when
deicing boots
are
installed.
ISSUED:
JANUARY 8, 1981
REPORT:
VB-1110
I-3

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