EasyManuals Logo

Eclipse EA500 User Manual

Eclipse EA500
304 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #279 background imageLoading...
Page #279 background image
ADS-B OUT WITH GPS 3 - DESCRIPTION AND OPERATION
AMM-34-50-21-081-801
1. Introduction
A.
The Automatic Dependent Surveillance – Broadcast Out (ADS-B Out) provides air traffic
controllers with real-time position information.
B. ADS-B Out with GPS 3 system have these components:
One GPS antenna (GPS 2) (Combination Antenna)
One GPS 2 Antenna Splitter
One GPS/Wide Area Augmentation System (WAAS) sensor GPS 3 (GDL 88)
One ADS-B fail annunicator
2.
Description
A.
ADS-B OUT System with Dual Transponder System (Diversity or Non-Diversity).
(1) The Dual Transponder System, both transponders are the Enhanced Mode S
transponders with or without the antenna diversity by Garmin, models GTX–33(D).
Both transponders, XPDR 1 and XPDR 2, are located behind the Instrument Panel
(IP).
(2) The GPS 3 (GDL 88) unit is located beneath the cabin floor on the left side of the
aircraft.
(3) The GPS 2 Antenna Splitter is located under the aft baggage compartment floor.
(4) ADS-B system failure annunciation (based on the GPS 3 position source failure) is
located in the cockpit on the lower left instrument panel.
3.
Operation
A.
The ADS-B OUT system utilizes the Extended Squitter (ES) capability of the
transponders.
GPS 3 (GDL 88) with internal GPS provides the necessary ADS-B OUT compliant
position data to the already installed transponders. GPS 3 outputs the ADS-B OUT
compliant GPS data to both transponders via a dedicated RS-232 line.
B. GPS 3 (GDL 88) makes use of the GPS 2 antenna through the GPS 2 Antenna Splitter,
which is located below the aft baggage compartment floor.
C. The ADS-B system failure indicator provides an advisory message to the pilot via a white
ADS-B FAIL indication if any of the following events occur:
GPS 3 loses its integrity
During R Smoke Clear procedure
Manually pulling ECB
Battery-only Load shed
Unintended power loss
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-34-030
34-50-21
Page 1
Sep 30/20
© 2020 Eclipse Aerospace, Inc.

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Eclipse EA500 and is the answer not in the manual?

Eclipse EA500 Specifications

General IconGeneral
BrandEclipse
ModelEA500
CategoryAircrafts
LanguageEnglish

Related product manuals