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Honda Aircraft Company
HA-420
SYSTEMS
POM
DESCRIPTION
Traffic Collision Avoidance System I (TCAS I)
The TCAS I system provides collision avoidance information from other
suitably-equipped aircraft within the reception range.
Traffic information can be displayed on a dedicated Display Pane or as
an overlay on the Map page. If the optional Synthetic Vision PFD
feature is installed, traffic will also be displayed on the PFD using
similar symbology. TCAS control is through the CDUs.
Traffic Collision Avoidance System II
The optional TCAS II system provides Resolution Advisories (RA) in
addition to the information provided by the baseline TCAS I system.
When a RA is encountered, fly-to and avoid instruction are provided
visually on the PFD as well as aurally.
Emergency Locator Transmitter
The Emergency Locator Transmitter is an Automatic Fixed COSPAS-
SARSAT ELT two-frequency transmitter. The ELT can be activated
either automatically when the LRU detects a high-G impulse (via an
internal shock sensor), or manually (via either a switch mounted on the
transmitter housing, or via a Remote Control Panel).
The ELT receives GPS position data, which (along with aircraft
identification data) is transmitted when the unit is activated, from the
Integrated Avionics units.
Selecting the ELT switch to the 'ON' position begins ELT transmissions.
In the 'NORM' position ELT will begin transmitting upon detection of
an activating impact by the G sensor. The 'RESET/TEST' position is
used to reset the unit, and to stop transmission, in case of unintentional
activation; or to initiate unit self-test.
HJ1-29000-005-001
October 30, 2016
1-214
FOR TRAINING PURPOSES ONLY
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