Garmin GNS 530 Installatiehandleiding - Pagina 7

Blader online of download pdf Installatiehandleiding voor {categorie_naam} Garmin GNS 530. Garmin GNS 530 14 pagina's. Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
Ook voor Garmin GNS 530: Handleiding voor piloten (22 pagina's), Gebruiksaanwijzing (6 pagina's), Handleiding voor piloten Addendum (27 pagina's), Handleiding voor piloten Addendum (4 pagina's), Snelle referentie (16 pagina's), Brochure (1 pagina's), Snelle referentie (23 pagina's), Handleiding voor piloten Addendum (22 pagina's), Handmatig (35 pagina's)

1.3.7

Glideslope Specifications (GNS 530 Only)

Regulatory Compliance

(TAWS units only)

Sensitivity

Centering Accuracy

Selectivity

Standard deflection

Flag

1.3.8

TAWS Regulatory Compliance (TAWS units only)

TSO-C151b Class B

ETSO-C151b

Page 1-6

Rev S

TSO C34e, JTSO-C34e, RTCA DO-192, EuroCAE ED-47B

ETSO-2C34f

-87 dBm or less for 60% of standard deflection.

0 ±.0091 ddm or 0 ±7.8 mV.

The course deviation shall be 0 ddm ±.0091ddm when using

the Glideslope Centering Test Signal as the RF frequency is

varied ±17 kHz from the assigned channel.

At frequencies displaced by ±132 kHz or greater, the input

signal shall be at least 60 dB down.

a) With a standard deflection 'FLY DOWN' condition (90 Hz

dominant), the output shall be -78 mV ±7.8 mV.

b) With a standard deflection 'FLY UP' condition (150 Hz

dominant), the output shall be +78 mV ±7.8 mV.

The unit Flags:

a) When the level of a standard deviation test signal

produces 50% or less of standard deflection of the deviation

indicator.

b) In the absence of 150 Hz modulation.

c) In the absence of 90 Hz modulation.

d) In the absence of both 90 Hz and 150 Hz modulation.

e) In the absence of RF.

500 SERIES INSTALLATION MANUAL

190-00181-02