Garmin GTN 650 Panduan Pengguna - Halaman 13

Jelajahi secara online atau unduh pdf Panduan Pengguna untuk Tampilan Avionik Garmin GTN 650. Garmin GTN 650 22 halaman. Gps/sbas navigation system as installed in cessna 172r
Juga untuk Garmin GTN 650: Petunjuk Aktivasi (46 halaman), Panduan Pengguna (20 halaman), Suplemen Manual (31 halaman), Ralat (4 halaman), Panduan Penerbangan (49 halaman), Panduan Referensi Cepat (2 halaman), Panduan Pilot (28 halaman)

3.3

AUDIO PANEL

3.3.1 LOSS OF AUDIO PANEL FUNCTIONS (GMA 35 Only)

Audio Panel Circuit Breaker ........................................................................ PULL

This procedure will force the audio panel into fail safe mode

which provides only the pilot with communications and only

on a single COM radio. If any non GTN 750 COM is

installed, communication will be only on that radio. If only

a GTN 750 is installed in the aircraft, then the pilot will have

only the GTN 750 COM available. No other audio panel

functions including the crew and passenger intercom will

function.

3.4

3.4.1 DATA SOURCE - HEADING SOURCE INOPERATIVE OR

CONNECTION TO GTN LOST MESSAGE

Without a heading source to the GTN, the following system limitations will be

imposed:

 Map cannot be oriented to Heading Up.

 All overlaying traffic data from a TAS/TCAS I cannot be displayed on the

main map display. The flight crew must use the dedicated traffic page on

the GTN system to display TAS/TCAS I traffic data.

3.4.2 DATA SOURCE – PRESSURE ALTITUDE SOURCE

INOPERATIVE OR CONNECTION TO GTN LOST MESSAGE

Without a barometric altitude source to the GTN, the following system

limitations will be imposed:

 Automatic leg sequencing of legs requiring an altitude source. The flight

crew must manually sequence altitude legs, as prompted by the system.

RFMS, Bell 407 GTN GPS/SBAS System

FAA APPROVED

NOTE

190-01007-J4 Rev. 1

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