Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 4
Nov 30/06
3I4
34-50-00
2. Tr
ansponder
WARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING
OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY
RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY
PUBLICATIONS.)
A. S/N’s 2842001 thru 2842108
A Garmin GTX-320 Transponder is installed as standard equipment. Maintenance of the
GTX-320 is “on condition” only and, with the exception of swapping complete units, should be
performed only by a qualified avionics shop in accordance with the Garmin GTX-320 Maintenance
Manual (Garmin P/N - 190-00133-02).
Information provided in this manual is intended solely to aid the removal and installation of the
GTX-320 transceiver/display unit, its associated wiring and antenna.
Removal and Installation
See 39-10-00.
B. S/N’s 2842109 thru 2842200
A Garmin GTX-327 Transponder is installed as standard equipment. Maintenance of the
GTX-327 is “on condition” only and, with the exception of swapping complete units, should be
performed only by a qualified avionics shop in accordance with the Garmin GTX-327 Maintenance
Manual (Garmin P/N - 190-00187-05).
Information provided in this manual is intended solely to aid the removal and installation of the
GTX-327 transceiver/display unit, its associated wiring and antenna.
Removal and Installation
See 39-10-00.
C. S/N’s 2842201 and up
A Garmin GTX-330 Transponder is installed as standard equipment. Maintenance of the GTX-330 is
“on condition” only and, with the exception of swapping complete units, should be performed only by
a qualified avionics shop in accordance with the GARMIN GTX-330 Maintenance Manual (Garmin
P/N - 190-00207-02).
Information provided in this manual is intended solely to aid the removal and installation of the
GTX-330 transceiver/display unit, its associated wiring and antenna.
(1) Removal and Installation
See 39-10-00.
(2) Post Installation Setup Procedure (PIR-PPS-60206 Rev. H.)
Access the Configuration Mode of the unit by depressing and holding the FUNC key while
applying power to the unit. Release the FUNC key when the display activates. The FUNC key
sequences forward through the configuration pages. The START/STOP key reverses through
the pages, stopping at the Menu page. The CRSR key highlights selectable fields on each
page. When a field is highlighted, the 0-9 keys enter numeric data and the 8 or 9 keys move
through list selections. Press the CRSR key to accept changes. When a field is highlighted,
pressing the FUNC key moves to the next configuration page without saving the changes. To
exit the configuration pages, turn the power off and then turn the unit on again without holding
the FUNC key for normal operation.
NO
TE: When the unit it turned on for the first time, or an invalid address is recognized, the
unit will prompt the user to enter a valid aircraft address. See Mode S Address
paragraph, below.

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)