Piper SENECA III - Engine; Propeller

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