Piper SENECA III User Manual

PIPER
AIRCRAFT CORPORATION SECTION
I
PA-34-220T,
SENECA III
GENERAL
tc)
Oil
Viscosity
Aviation
S.A.E.
Grade
No.
(1)
Below
40°F
1065
30
(2)
Above
40°F
\ 100
50
When
operating
temperatures
overlap
indicated
ranges,
use
the
lighter
grade
of oil.
Multi-viscosity
oils meeting
Teledyne Conti-
nental
Motors'
Specification MHS-24A
are
approved.
1.11
MAXIMUM
WEIGHTS
(a)
Max.
Ramp
Weight
(lbs.)
4773
(b)
Max.
Takeoff
Weight
(Ibs.)
4750
(c)
Max.
Landing
Weight
(lbs.)
4513
(d)
Max.
Zero
Fuel
Weight
(Ibs.)
-
Std.
4470
le)
Max.
Weights
in Baggage
Compartment.(Ibs.)
(I)
Forward
100
(2)
Aft 100
1.13
STANDARD
AIRPLANE
WEIGHTS
Reíer
to
Figure
6-5
for the Standard
Empty
Weight
and
the
Useful
Load.
L15
BAGGAGE
SPACE
FORWARD
AFT
ta)
Maximum
Baggage
(Ibs.)
100 100
(b)
Baggage
Space
(cu.
ft.)
15.3
17.3
(c)
Baggage
Door
Size
(in.)
24
x
21
1.17
SPECIFIC
LOADINGS
(al
Wing
Loading
(lbs.
per sq.
ft.) 22.8
(b)
Power
Loading (lbs.
per
hp) 10.8
ISSCED:
JANUARY
8, 1981
REPORT:
VB-Il10
REVlSED:
AUGUST
9, 1982 1-5

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