Piper ARCHER III Pilot Operating Handbook page 300

SECTION 9
SUPPLEMENT 18
SECTION 1 - GENERAL
This supplement supplies information necessary for the operation of the airplane
when the Garmin GTX 330 Transponder is installed in accordance with FAA
approved Piper data.
SECTION 2 - LIMITATIONS
A. Display of TIS traffic information is advisory only and does not relieve the
pilot responsibility to "see and a void"other aircraft. Aircraft maneuvers shall
not be predicated on the TIS displayed information.
B. Display of TIS traffic information does not constitute a TCAS I or TCAS II
collision avoidance system as required by 14 CFR Part 121 or Part 135.
C. Title 14 of the Code of Federal Regulations (14 CFR) states that "When an
Air Traffic Control (ATC) clearance has been obtained, no pilot-in-command
(PIC) may deviate from that clearance, except in an emergency, unless he
obtains an amended clearance."Traffic information provided by the TIS up-
link does not relieve the PIC of this responsibility.
D. The 400/500 Series Garmin Display Interfaces (Pilot's Guide Addendum)
P/N 190-00140-13 Rev. A or later revision must be accessible to the flight
crew during flight.
E. 400/500 Series Main Software 4.00 or later FAA approved software is
required to operate the TIS interface and provide TIS functionality.
SECTION 3 - EMERGENCY PROCEDURES
To transmit an emergency signal:
• Mode Selection Key - ALT
• Code Selection - SELECT 7700
To transmit a signal representing loss of all communications:
• Mode Selection Key - ALT
• Code Selection - SELECT 7600
REPORT: VB-1611
9-100, 2 of 4
PA-28-181, ARCHER III
ISSUED: JULY 12, 1995
REVISED: JANUARY 5, 2004