Piper ARCHER III Pilot Operating Handbook page 194

SECTION7
DESCRIPTION & OPERATION
7.15 GARMIN GlOOO AVIONICS SYSTEM
The latest appropriate rev1s1on of the Garmin
G 1000 Cockpit Reference Guide for the Piper
PA-28-181 Archer (Garmin PIN 190-02131-02),
and the Garmin G 1000 Pilot's Guide for the Piper
PA-28-181 Archer (Garmin PIN 190-02130-02),
contain operational information and detailed
descriptions of rhe Garmin G l 000 avionics system,
the annunciator system (CAS and Non-CAS) and
all warnings, cautions and advisories.
The Garmin GI 000 Integrated Avionics System consists of a Primary
Flight Display (PFD), Multi-Function Display (MFD), Audio Panel, Air
Data / Attitude and Heading Reference System (ADAHRS), and the sensors
and computers to process night and engine information for display to
the pilot. The system contains dual GPS SBAS receivers, dual VOR/ILS
receivers, dual VHF communications transceivers, a transponder, and an
integrated crew alerting system (CAS) 10 alert the pilot via status /advisory
messages, caution messages and warning messages. The G 1000 system also
provides system messages which alert the pilot to abnormalities associated
with the G 1000 system. The 01000 system
Traffic Information Service (TIS) and FliteCharts. Optional avionics equipment
include ADF, DME, Class B TA WS, Automatic Dependent Surveillance­
Broadcast (ADS-B out), Traffic Advisory System (TAS), Jeppesen ChartView,
System 55X autopilot, Synthetic Vision, AOPA Facilities Directory, and the
Garmin DataJink (GDL) for XM weather.
REPORT: VB-274 9
7- 8
PA-28-181, ARCHER ID
NOTE
has a terrain proximity system,
also
ISSUED: December 22, 2017
REVISED: June 17, 2019
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