Tas alerts, System status, Hazard avoidance – Garmin G1000 King Air C90GT User Manual

Page 402

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Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT

190-00663-01 Rev. A

388

HAZARD AVOIDANCE

SY

STEM

O

VER

VIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID

ANCE

AFCS

ADDITIONAL FEA

TURES

APPENDICES

INDEX

TAS ALERTS

NOTE:

Refer to the SKY899 documentation for information on alerts generated by the TAS equipment.

When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur:

• A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for 5 seconds and

remaining displayed until no TAs are detected in the area.

• The PFD Inset Map is automatically displayed with TA traffic.

Figure 6-110 Traffic Annunciation (PFD)

Inset Map

Displays When

TA is Detected

SYSTEM STATUS

The traffic mode is annunciated in the upper left corner of the Traffic Map Page.

Mode

Traffic Mode Annunciation

(Traffic Map Page)

Traffic Display Enabled Icon

(Other Maps)

TAS Self-test Initiated

TEST

TAS Operating

OPERATING

TAS Standby

STANDBY

(also shown in white in center of page)

TAS Failed*

FAIL

* See Table 6-17 for additional failure annunciations

Table 6-25 TAS Modes

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