Piper SENECA III User Manual

SECTION 4
PIPER
AIRCRAFT
CORPORATION
NORMAL
PROCEDURES
PA-34-220T,
SENECA III
When
engúne
fires:
Starter.........
.........lease
engaged
Primer button
...
..... .
..
......
tap
until
rhythmic
firing
Starter.
......-..
.........release
Throttk
.,.,..,..
.
.........halftrasel
Oil
pressure
........... .. .
......check
H
engine
begins
to
falter:
Primer
button
......... ..........
tap
Throttle
..........
.. ........
1000 RPM
Auxiliary
fuel
pump
........... .
........OFF
after
start
complete
STARTING
ENGINES WITH
EXTERNAL POWER
Batiers
switch
........ . . .........
OFE
All
ekctricalequipment............
.. ..........
OFF
Terminals..........
.
...........connect
External
power
plug.......
... .. .........
insert
in fuselage
ŸroCCed
WÍ\b
normal
start.
Throttics............
. ..........
lowest
possible
RPM
External
power
plug.......
. .
.........
disconnect from
fuselage
Batters
switch
..
. .. ....
ON
check
ammeter
Oil
pressure
. . . . . . . . . . .
.
check
WARM-UP
Throilles.....
-. ........
1000
to
|200
RPM
TAXIING
Chocks
......
........
remored
Parking
brak.c
. .
..
........
release
Taxi
area
.... .
........
clear
Throttle
........
.........apply
slowly
Brakes.........
........check
Steering
.......
.
......
.check
Instrurnen>
......
.
.....
.check
Heater
and
detroster
..
.. .
....
..--.
.check
Fuel
selector
. . . . . .
.
. . . . . . . .
ON.
check
crossteed
Autopilot
.......
...
.
OEE
REPORT:
VB-llI0
ISSUED:
JANTARY
8.
1981
4.8
REVISED:
FERRUA.RY
10, 1984

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