Garmin GTN 625 Kılavuz Eki - Sayfa 14

Aviyonik Ekran Garmin GTN 625 için çevrimiçi göz atın veya pdf Kılavuz Eki indirin. Garmin GTN 625 31 sayfaları. Gps/sbas navigation system as installed in cessna 172r
Ayrıca Garmin GTN 625 için: Etkinleştirme Talimatları (46 sayfalar), Kullanıcı Kılavuzu (20 sayfalar), Errata (4 sayfalar), Kullanıcı Kılavuzu (22 sayfalar), Uçuş El Kitabı (49 sayfalar), Pilot El Kitabı (28 sayfalar)

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151

Olathe, KS 66062 USA

Both Garmin GPS navigation receivers must be operating and providing GPS

navigation guidance for operations requiring RNP-4 performance.

Applicable to installations consisting of two GTNs: North Atlantic (NAT)

Minimum Navigational Performance Specifications (MNPS) Airspace operations

per AC 91-49 and AC 120-33 require both GPS/SBAS receivers to be operating

and receiving usable signals except for routes requiring only one Long Range

Navigation sensor. Each display computes an independent navigation solution

based on its GPS sensor.

Whenever possible, RNP and RNAV routes including Standard Instrument

Departures (SIDs) and Obstacle Departure Procedures (ODPs), Standard Terminal

Arrival (STAR), and enroute RNAV "Q" and RNAV "T" routes should be loaded

into the flight plan from the database in their entirety, rather than loading route

waypoints from the database into the flight plan individually. Selecting and

inserting individual named fixes from the database is permitted, provided all fixes

along the published route to be flown are inserted. Manual entry of waypoints

using latitude/longitude or place/bearing is prohibited.

It is not acceptable to flight plan a required alternate airport based on

RNAV(GPS) LP/LPV or LNAV/VNAV approach minimums. The required

alternate airport must be flight planned using an LNAV approach minimums or

available ground-based approach aid.

Navigation information is referenced to the WGS-84 reference system, and should

only be used where the Aeronautical Information Publication (including

electronic data and aeronautical charts) conform to WGS-84 or equivalent.

2.5

System Use

In installations with two GTNs and an external GPS annunciator (See Table 1) the

GTN connected to the external GPS annunciator must be used as the navigation

source for all operations.

The only approved sources of course guidance are on the external CDI, HSI, or

EHSI display. The moving map and CDI depiction on the GTN display are for

situational awareness only and are not approved for course guidance.

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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