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Piper SENECA III User Manual

Piper SENECA III
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SECTION I
PIPER
AIRCRAFT
CORPORATION
GENERAL
PA-34-220T,
SENECA
III
OPTIONAT
(a)
Number
of
Propellers
2
(b)
Propeller
Manufacturer
McCauley
(c)
Propeller
Hub & Blade
Models*
(1)
Left
3AF32CSOS
82NFA-6
(2)
Right
3AF32C509
LR2NFA-6
or
(3) I
eft
32AF32C508-(
)
(
)-82NFA-6
(4)
Right
32AF32C509-(
)
(
)-LS2NFA-6
(d) Number
of
Blades
3
(el
Propeller
Diameter (in.)
(1)
Maximum
76
(2)
Minimum 75
(f) Propeller Type
Constant
Speed,
Hydraulically Activated.
Full
Feathering
L7
FUEL
(a)
Fuel Capacity (LLS. gal
)
(total)
(1)
Without optional
tanks 98
(2)
With
optional
tanks 128
(b)
l½able Fuel
(LS
gat)
(total)
(!)
Without
optional
tanks
93
(2)
With
optional
tanks
123
(c)
Fuel
(I)
Minimum Grade
!00
Green
or
100LL
Blue Aviation
Grade
(2) Alternate
FueW
Refer
to
latest
revision
of
Continental
Senice
Bulleún
"Fuel and
Oil
Grades."
L9 OIL
(a)
Oil Capacits
(I
S.
ytsj
(per
engine)
8
(b)
Oil
Specification Refer
to
latest
revision
of
Continental
Service
Bulletin
"Fuel
and O
Grades
"
*The propellers
have
the
same
designanon when
deicing
boots
are
installed.
REPORT: VB4110
ISSUED: JANUARY
8.
1981
04
REVlSED: SEPTEMBER
23,
1983

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Piper SENECA III Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelSeneca III
Engine TypePiston
Engine ModelContinental TSIO-360-KB
Seating Capacity6
Cruise Speed188 knots (216 mph, 348 km/h)
Length28 ft 7 in (8.71 m)
Max Takeoff Weight4, 750 lb (2, 155 kg)
Horsepower220 hp each
Service Ceiling25, 000 ft (7, 620 m)
Height9 ft 11 in (3.02 m)
Propellers2-bladed constant speed

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