Piper SENECA III User Manual

SECTION
9
PIPER
AIRCRAFT CORPORATION
SUPPLEMENT 19
PA-34-220T,
SENECA
IH
SECTION 2
-
LIMITATIONS
No
changes
to
the
basic
limitations
provided
by
Section 2
of
this Pilot's
Operating
Handbook
are
necessary
for this
supplement.
SECTION 3
-
EMERGENCY
PROCEDURES
No
changes
to
the
basic
Emergency
Procedures
provided
by
Section 3
of
this Pilot's
Operating
Handbook
are
necessary
for
this
supplement.
SECTION
4
-
NORMAL
PROCEDURES
(a)
EQUlPMENT
OPERATION
AND
CONTROLS
(1)
RDR-160XD/IN-232A
CONTROLS AND
DISPLAYS
Controls
and
displays for
the
RDR-160XD/
IN-232A Weather
Radar System
are
listed
in
Table
4-3,
with
a
functional
description.
Location
of the
controls
and
displays
is
shown
in
Figure 4-1.
All
operating
controls
and
displays
are
located
on
the
indicator.
BAG
FLASHESlN
INDICATES
INDiCATES
CURSOR
HOLD
SELECTED
RANGE
WHEN
FUNCTION
POSITION
CONDITION
MODE
SELECTED
SWITCH
IS
CT
ESIN
DE
SETA
RADAR
RECEIVER
TRACK
CURSOR
PRESS TO
SELECT
N
(BUTTON
POSITIONEDi
WEATI-IER
MODE
-
¯
PRESS TO
PRESS TO
SELECT
AETAIN
DISPLAY
WEATHER
ALERIN
RANGE
MARK
MODE
PRESS
TO
1NCREASE
PRESS To
SELECT
NGE
RANGE
GMROUND
MAPPING,
PRENSSTO
DECREASE
ENDICATES
NAV
-
Ti
T
BUTTON
PRESSED
BUT NAV
OPTION
NM
TRACH
PLT
LOG
.
NOT
CONNECTED
¯ll
ANTENNA
TILT
CONTROL
I
-
-
-
FUNCTION
SWFTCH
LOCKINGPAWL
LEFT
y
RIGHT
USED
ONLY
WITH
USED ONLY
WITH
PRESS
TO
MOÝE
OPTIONAL
SQUtPMENT
OPTIONAL
EQUIPMENT
TFACK CURSOR
DISPLAVS UP
TO
TEN
PILDT
NAL
PLUS
WEATHER)
PROGRAMMED
WAYPOINTS)
IN-232A
CONTROLS
AND
DISPLAYS
Figure 4-1
REPORT:
VB-IIIO
ISSUED:
FEBRUART25,
1982
9-126,
2
of 6

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