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GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151

Olathe, KS 66062 USA

When a TAWS CAUTION occurs, take corrective action until the alert ceases.

Stop descending or initiate either a climb or a turn, or both as necessary, based on

analysis of all available instruments and information.

3.2.6 TAWS INHIBIT

The TAWS Forward Looking Terrain Avoidance (FLTA) and Premature Descent

Alerts (PDA) functions may be inhibited to prevent alerting, if desired. Refer to

GTN Cockpit Reference Guide for additional information.

To Inhibit TAWS:

Home Hardkey ............................................................................................ PRESS

Terrain Button ............................................................................................. PRESS

Menu Button ............................................................................................... PRESS

TAWS Inhibit Button ..................................................... PRESS TO ACTIVATE

3.2.7 TER N/A and TER FAIL

If the amber TER N/A or TER FAIL status annunciator is displayed, the system

will no longer provide TAWS alerting or display relative terrain and obstacle

elevations. The crew must maintain compliance with procedures that ensure

minimum terrain and obstacle separation.

3.2.8 HEADING DATA SOURCE FAILURE

Without a heading source to the GTN, the following features will not operate:

GPSS will not be provided to the autopilot for heading legs. The autopilot

must be placed in HDG mode for heading legs.

Map cannot be oriented to Heading Up.

All overlaying traffic data from a TAS/TCAS I system on the main map

display. The pilot must use the dedicated traffic page on the GTN system to

display TAS/TCAS I data.

All overlaying StormScope® data on the main map display. The pilot must

use the dedicated StormScope® page on the GTN system to display

StormScope® data.

StormScope® must be operated in accordance with Section 7.8 when no heading

is available.

3.2.9 PRESSURE ALTITUDE DATA SOURCE FAILURE

Without a pressure altitude source to the GTN, the following features will not

operate:

Automatic leg sequencing of legs requiring an altitude source. The pilot must

manually sequence altitude legs, as prompted by the system.

190-01007-A2 Rev. 1

FAA APPROVED DATE: _________________

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

Street

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

MARCH 18, 2011

NAVIGATION SYSTEM

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