Garmin GNC 420 Apéndice del Manual del Piloto - Página 10

Navegue en línea o descargue pdf Apéndice del Manual del Piloto para Pantalla de aviónica Garmin GNC 420. Garmin GNC 420 22 páginas. 400/500 series gts 8xx interface
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GTS 8XX Interface

1.4

AURAl AleRTS

A TA consists of a displayed traffic symbol (solid yellow circle) and an aural alert.

The aural alert announces "traffic", followed by the intruder aircraft' s position, altitude

relative to own aircraft ("high", "low", or "same altitude"), and distance from own

aircraft; e.g. "traffic, 12 o'clock, high, 3 miles".

1.5

The GTS 8XX automatically performs a self-test upon power up. The self-test

checks internal parameters and calibrates components of the GTS 8XX. The self-test

can also be initiated by the user during normal operation.

Check for the following test criteria on the Traffic Page during power-up:

• If the GTS 8XX passes the power-up test; and the aircraft both has a squat

switch and is on the ground, the Standby Screen is displayed (Figure 2).

• If the GTS 8XX passes the power-up test and the aircraft both has a squat

switch and is airborne, the Traffic Page is displayed on the 6-nm display range

and in the normal altitude display mode.

• If the GTS 8XX passes the power-up test and the aircraft does not have a squat

switch, the Standby Screen is displayed (Figure 2).

• If the GTS 8XX fails the power-up test (as indicated by a FAILED screen),

the GTS 8XX is inoperable, see the GTS 8XX Installation Manual for detailed

information on Failure Response.

NOTE: The FAILED message is displayed when the system detects an error

that prohibits further traffic display operation.

NOTE: When the system is in standby, the GTS 8XX does not transmit,

interrogate, or track intruder aircraft.

400/500 Pilot's Guide Addendum for GTS 8XX Interface

190-00140-78 Rev. A