Garmin GNS 530 Manuel d'installation - Page 5

Parcourez en ligne ou téléchargez le pdf Manuel d'installation pour {nom_de_la_catégorie} Garmin GNS 530. Garmin GNS 530 14 pages. Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
Également pour Garmin GNS 530 : Manuel du pilote (22 pages), Manuel d'instructions (6 pages), Addendum au manuel du pilote (27 pages), Addendum au manuel du pilote (4 pages), Référence rapide (16 pages), Brochure (1 pages), Référence rapide (23 pages), Addendum au manuel du pilote (22 pages), Manuel (35 pages)

1.3.5

VOR Specifications (GNS 530 Only)

Regulatory Compliance

(TAWS units only)

Receiver Audio Sensitivity

Course Deviation Sensitivity

Flag

AGC Characteristics

Spurious Response

VOR OBS Bearing Accuracy

Audio Output

Audio Response

Audio Distortion

Page 1-4

Rev S

TSO C40c, JTSO-2C40c, RTCA DO-196, EuroCAE ED-22B

ICAO Annex 10 Volume I (Radio Navigation Aids) Par. 3.3.8

ETSO-2C40c

At -103.5 dBm (S+N)/N shall not be less than 6 dB.

-103.5 dBm or less for 60% of standard deflection.

The VOR Course Deviation Flag must be flagged:

a) in the absence of an RF signal.

b) in the absence of the 9960 Hz modulation.

c) in the absence of either one of the two 30 Hz

modulations.

d) When the level of a standard VOR deviation test signal

produces less than a 50% of standard deflection.

From -99 dBm to -13 dBm input of a Standard VOR Audio

Test Signal, audio output levels shall not vary more than 3

dB.

Greater than 80 dB.

The bearing information as presented to the pilot shall not

have an error in excess of 2.7° as specified by RTCA DO-196

and EuroCAE ED-22B.

A minimum 100 mW into a 500 Ω load.

Less than 6 dB of variation between 350 and 2500 Hz.

Except the 1020 Hz Ident Tone is at least 20 dB down in

voice mode.

The distortion in the receiver audio output shall not exceed

10% at all levels up to 100 mW.

500 SERIES INSTALLATION MANUAL

190-00181-02