Garmin GNS 530 Manual - Página 7

Navegue en línea o descargue pdf Manual para Pantalla de aviónica Garmin GNS 530. Garmin GNS 530 35 páginas. Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
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DA 40 AFM

The Main software version is displayed on the GNS 530 self test page immediately

after turn-on for 5 seconds. The remaining system software versions can be verified

on the AUX group sub-page 2, 'SOFTWARE/DATABASE VER'.

IFR en route and terminal navigation predicated upon the GNS 530's GPS

Receiver is prohibited unless the pilot verifies the currency of the data base or

verifies each selected waypoint for accuracy by reference to current approved

data.

Instrument approach navigation predicated upon the GNS 530's GPS Receiver

must be accomplished in accordance with approved instrument approach

procedures that are retrieved from the GPS equipment data base. The GPS

equipment database must incorporate the current update cycle.

(1)

Instrument approaches utilizing the GPS receiver must be conducted in

the approach mode and Receiver Autonomous Integrity Monitoring

(RAIM) must be available at the Final Approach Fix.

(2)

Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other

type of approach not approved for GPS overlay with the GNS 530's GPS

receiver is not authorized.

(3)

Use of the GNS 530 VOR/ILS receiver to fly approaches not approved

for GPS requires VOR/ILS navigation data to be present on the external

indicator.

Doc. # 6.01.01-E

Rev. 0

01 Dec 2001

Supplement A21

GNS 530

Page 9 - A21 - 6