Garmin GNS 430 User Manual

Page 210

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GNS 430(A) Pilot’s Guide and Reference

190-00140-00 Rev. P

12-12

SECTION 12

ADDITIONAL FEATURES

Pilots should be aware of TAS/TCAS system

limitations. If an intruder transponder does not respond
to interrogations due to antenna shading or marginal
transponder performance, it will not be displayed, or
display may be intermittent. Pilots should remain vigilant
for traffic at all times when using TAS/TCAS systems for
non-transponder equipped airplanes or unresponsive
airplanes.

TCAS I Surveillance Volume

Top and bottom mounted antennas allow an active

surveillance range of up to 12 nm (GTS 800) or 40 nm
(GTS 820/850) in the forward direction, and somewhat
reduced ranges to the sides and aft of own aircraft due
to the directional interrogation patterns. Interference
limiting in GTS 820/850 units may automatically reduce
range in high density traffic areas.

TA Alerting Conditions

The GTS 8XX automatically adjusts its TA sensitivity level

(Table 12-5) to reduce the likelihood of nuisance TA alerting
during flight phases likely to be near airports. Sensitivity
Level A (less sensitivity) TA is used when the aircraft’s radar
altimeter (if equipped) indicates own altitude is less than
2000 feet AGL. If no radar altimeter is present, Sensitivity
Level A is active when the landing gear is extended. Level A
is also active when groundspeed is less than 120 knots with
no radar altimeter present in a fixed gear aircraft.

Sensitivity

Level

Intruder

Altitude

Available

TA Alerting Conditions

A

Yes

Intruder closing rate provides less than 20 seconds of vertical and horizontal separation.

Or:

Intruder range is within 0.2 nm and vertical separation is within 600 feet.

A

No

Intruder closing rate is less than 15 seconds.

B

Yes

Intruder closing rate provides less than 30 seconds of vertical and horizontal separation.

Or:

Intruder range is within 0.55 nm and vertical separation is within 800 feet.

B

No

Intruder closing rate is less than 20 seconds.

Table 12-5 TA Sensitivity Level and TA Alerting Criteria

In all other conditions, Level B (greater sensitivity) TA
sensitivity is used to assess TA threats.

Traffic Symbology

Traffic information from the GTS 8XX is displayed

on the GNS 430 unit using TAS/TCAS symbology (Table
12-4) on a dedicated Traffic page, and on the moving Map
Page. The displayed traffic information generally includes
the relative range, bearing, and altitude of intruder aircraft.
The GTS 8XX also generates aural announcements heard
on the cockpit audio system.

Target altitude relative to own aircraft altitude (relative

altitude) is displayed (in hundreds of feet) for each target
symbol (Figure 12-20). If traffic is above own aircraft altitude
the relative altitude is shown above the target next to a ‘+’
symbol. If traffic is below own aircraft altitude the relative
altitude is shown below the target next to a ‘-’ symbol.

Altitude trend (Figure 12-20) is displayed as an up

arrow (≥ +500 fpm), down arrow (≤ -500 fpm), or no
symbol if less than 500 fpm rate in either direction.

Figure 12-20 Traffic Symbol Components

Relative

Altitude

Altitude

Trend

Traffic

Type

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