Piper SENECA III User Manual

PIPER
AIRCRAFT
CORPORATION SECTION
4
PA-34-220T,
SENECA
III
NORMAL PROCEDURES
Stahilator.........
.
... ...,_
frec
\nienna,
....
.... .....
.
........check
N
igation
and
hinding
lights..........
.
.........check
Rieht
static
sent
........ .
........
clear
BEFORE
STARTING
ENGINES
heats
....,....
....
........adiustetL
secure
Seat
belt,
and
harnem
....... ..
. .........
boten
adiust
-
check
inertia reel
PaEkmy
brake
.
......
..........
Nel
WAR/VING
\o
braking
will
occur
if
knob
is
pulled
before
brake
appitcation.
Circuit
breakers....................
........... -.
..........,.in
Radios
.......
...
........,
.. ..
.-..... .
...........
OFF
Con!
Dap,
....
......
..........OPEN
Abernate
air
..
... ..
.........
OFF
Alternators....
....
......
..
ON
STARTING
ENGINES
(AIRPLANE
EQUIPPED
WlTH STANDARD
PRIMER
SYSTEM)
Euci
selector
.
......
........
ON
Mnture
... .
.........FULI
RICH
Thmitle
.
........half
travel
Propcontrol
.........
..., ...
FULL
FORWARD
Bauen
switch
........
. ,,.....
ON
lynmon
swnchos
(mags)
......
.......,
ON
Propeller...
...... .
. .. ..
cicar
Starter.......,
..........engage
Prirner........
............as
required
thronie
.......
-........adjust
when
engine
starts
Oil
premure
..........
.
.
..........check
Repeat
for
opponne
engine
Alternators.........
........
....... . .. . .. .
.........check
Girosuction
.........
......
..... .. .. ..... ..
.........check
ISSUED:
JANUARY
8,
1981
REPORT: VB-IllO
REVISED:
FEBRUARY
10,
1984
4-5

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