Garmin GNS 430 Manuale operativo del pilota - Pagina 4

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Anche per Garmin GNS 430: Manuale del pilota (22 pagine), Manuale di istruzioni (6 pagine), Addendum al Manuale del Pilota (27 pagine), Addendum al Manuale del Pilota (4 pagine), Riferimento rapido (23 pagine), Addendum al Manuale del Pilota (22 pagine), Specifiche (2 pagine), Riferenza rapida (17 pagine), Manuale operativo (27 pagine)

Section 9

Supplements

6. The aircraft must have other approved navigation equipment

installed and operating appropriate to the route of flight.

7. The Garmin GNS 430 meets RNP5 (BRNAV) requirements of

AC 90-96 and is in accordance with AC 20-138, and JAA AMJ

20X2 Leaflet 2 Revision 1, provided it is receiving usable

navigation information from the GPS receiver.

8. Do not use the Terrain Display for navigation of the aircraft. The

Terrain Display does not provide TAWS capability and is intended

to serve as a situational awareness tool only and does not provide

the accuracy fidelity on which to solely base terrain or obstacle

avoidance maneuvering decisions.

Section 3 - Emergency Procedures

1. If GPS Navigator information is not available or is invalid, utilize

remaining operational navigation equipment as required.

2. If "RAIM NOT AVAILABLE..." or "RAIM POSITION WARNING"

message is displayed, continue to navigate using the GPS

equipment or revert to an alternate means of navigation

appropriate to the route and phase of flight. When continuing to

use GPS navigation, position must be verified every 15 minutes

using another IFR approved navigation system.

The GARMIN GNS 430 Navigator is available in single or dual

installations. Operating procedures for each unit of a dual installation

are identical. Refer to the GNS 430 Integration paragraphs in this

supplement for integration differences when single and dual units are

installed.

Normal operating procedures are outlined in the GARMIN

GNS 430 Pilot's Guide and Reference, P/N 190-00140-00, Revision F

dated July 2000 (or later appropriate revision).

Activate GPS

1. Battery Master Switch ............................................................... ON

2. Avionics Power Switch .............................................................. ON

3. Navigator Com/ Power Switch...................................... Rotate 'ON'

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Cirrus Design

SR20

P/N 11934-S22

Revision 2: 08-15-07