Piper SENECA III User Manual

SECTION 4
.
PIPER
AIRCRAFT
CORPORATION
NORMAL
PROCEDURES
PA-34-220T,
SENECA
III
TAKEOFF
CAUTION
Fast
taxi
turns
immediately
prior
to
takeoff
run
should
be
avoided.
Adjust
mixture
prior
to
takeoff
from
high elevations.
Do
not
overheat.
Adjust
mixture only
enough
to
obtain smooth
engine
operation
Do
not
exceed
40
in. Hg.
manifold
pressure.
NOR
MAI
TAKEOFF
(Flaps
up)
Brakes..........
..
.
...........
apply and
hold
Flaps...........
.
...........UP
Brakes.............,..
... .
...
.............release
Accelerate
to
and
maintain
79 KIAS.
Cortrol
wheel
.............
.
..
......,...,
ease
back
to
rotate
to
climb attitude
After
obstacle
clearance,
accelerate
to
best
rate
of climb
speed
of92
KIAS.
Gear
...........
.
.
,............UP
SHORT
F1ELD
TAKEOFF
(25° Flaps)
Flaps
. . .
.
.
. . . .
. . . . . .
.
25°
(second
notch)
Stabilator
trim..........
. ..........
set
Brakes.............
..
......
.
........
apply
and
hold
Takeoff
power
before
brake release.
Brakes........
...- -
..........
release
Accelerate
to
64
KIAS.
Control
wheel
........
........
rotate
firmly
to
attain
66
KIAS
through
50
ft.
Gear
.......
.........UP
REPORT:
VB-lfl0
ISSUED:
JANEARY 8, 1981
4-10
REVISED:
FERRUARY
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