Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION
SECTION 2
PA-34-220T,
SENECA
III
LIMITATIONS
MARKING
KIAS
Blue
Radial
Line
(One
Engine
in-
operative
Best
Rate
of
Climb (Speed)
92
Yellow
Arc
(Caution
Range
-
Smooth
Air Only)
166
to
205
Green
Arc
(Normal
Operating
Range)
67
to
166
White Arc
(Flap Down)
64
to
I15
2.7
POWER
PLANT
LIMITATIONS
(a)
Number
of
Engines
2
(b)
Engine
Manufacturer
Continental
(c)
Engine
Model Number
(1)
Left
TSIO-360KB
(2)
Right
LTSIO-360K B
(d)
Engine
Operating
Limits
T.O.
Power Max. Cont.
5
Min.
Limit Power
(I)
Rated
Horsepower
(BHP)
220
200
(2)
Max.
Rotational
Speed (RPM)
2800
2600
(3)
Max.
Manifold
Pressure
(Inches
of Mercury)
40
(4)
Max.
Cylinder
Head Temperature
460°F
(5)
Max.
Oil
Temperature
240°F
(e)
Oil Pressure
Minimum
(red
line)
10
PSI
Maximum
(red
line)
100
PSI
(f)
Fuel Flow (Pressure)
Normal
Operating
Range
(green
arc)
3.5
PSI
to
18.1
PSI
Maximum
at
Sea
Level
(red
line)
21
PSI
(g)
Fuel
Grade
(min.
grade)
100
or
100LL
Aviation Grade
(h)
Number
of
Propellers
2
ISSUED:
JANUARY 8,
1981
REPORT:
VB-1110
2-3

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