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Piper SENECA III User Manual

Piper SENECA III
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SECTlON 2
PIPER AIRCRAFT
CORPORATION
LIMlTATIONS
PA-34-220T,
SENECA III
(i)
Propeller
Manufacturer
Hurtiell (Two
Blade)
(Standard)
Propeller
Hub
and Blade Models
a.
I.cft
BHC-C2YF-2CKUF
FCR459-8R
b.
Right
BHC-C2YF-2CLKUF
FJCB459-8R
or
c.
l.eft 32AF32C508-(
)
(
)-82NFA-6
d.
Right
32AF32C509-(
P
(
)-LS2NFA-6
NOTES
Avoid continuous operation
between 2000
and
2200 RPM
above
32 lN
HG.
manifold
pres-
sure.
Avoid
continuous
ground
operation
between
1700
and
2100
RPM
in
cross
and tail
winds
over
10 knots.
McCauley
(Three Blade)
(Optional)
Propeller Hub
and
Blade Models
a.
Left 3AF32C508
82NFA-6
b.
Right
3AF32C509
LR2NFA-6
(i)
Propeller
Diameter
(inches)
Maximum
76
Minimum
75
REPORT:
VB-1110
ISSUED: JANUARY
8, 1981
2-4
REVISED:
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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