Piper SENECA III User Manual

SECTION 4
PIPER
AIRCRAFT
CORPORATION
NORMAL
PROCEDURES PA-34-220T,
SENECA IH
APPROACH
AND
LANDING
Gear
warning
horn..............
.
.............check
Seat
backs
............
.
. . .............
erect
Belts barness..........
.. .
..............
fasten
adjust
Fuel
selectors...............
.
.... ..
.. ..............
ON
Cowl flaps
............ .
. .
.
................as
required
Auxiliary
fuel
pumps
............. .................
OFF
Mixture
controls...............
..
..
..............
rich
Prop
controls................
............
FULL
FORWARD
Landing
gear
..............................DOWN,
130 KIAS
max.
Flaps...............
.
..............
set,
I15 KIAS
max.
Approach
speed
............... . ..............
90 KIAS
or
above
GO-AROUND
Full
takeoff
power,
both
engines.
(40
in.
Hg.
maximum
manifold
pressure)
Establish
positive
climb.
Flaps...............~
.
. .... . .............
retract
Gear
................ . . .. . ...
................UP
Cowl
flaps
.............
.
. . . . ...
..............
adjust
AFTER
LANDING
Clear
of
runway.
Flaps...........
.
.............
retract
Cowl
flaps
...........,
...
..........
fully
OPEN
SHUTDOWN
Heater
(if
ON)..........
..........
FAN,
2
min.
then
OFF
Radios
&
electrical
.............
............
OFF
Throttle
.............
.............full
aft
Mixture
............
. .
..........
idle
cut-off
Magnetos
.......-....
.............
OFF
Battery
switch
.......... ..
.............
OFF
REPORT:
VB-1110
ISSUED:
JANUARY
8, 1981
4-12
REVISED: AUGUST
17,
1981

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