Garmin GDL 84H, Rotorcraft Flight Manual Supplement

Page: 6 / 16

Garmin International
1200 E. 151
st
Street Olathe, KS 66062
USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
for STC SR02123SE
GARMIN GDL 84H/88H ADS-B TRANSCEIVER
190-01310-J2 Rev. 1 Page 6 of 16
FAA APPROVED
Section 2. NORMAL PROCEDURES
The procedures described below are specific only to the GDL 84H/88H.
Cockpit Reference Guides and Pilot Guides for interfaced displays will provide
additional operating information specific to the displays or other traffic systems.
2.1 Unit Power On
GDL 84H/88H Annunciations ....................................................
CONSIDERED
NOTE
The GDL 84H ADS-B Annunciator will flash on/off for
approximately 20 seconds after power up if a fault was
present during the previous power cycle. This indicates the
unit requires service but does not indicate that the unit will
not comply with 91.227.
The GDL 84H/88H only complies with 14 CFR 91.227 for
ADS-B Out when all required functions are operational as
indicated when the ADS-B annunciator is not illuminated.
2.2 Before Takeoff
GDL 84H/88H Annunciations .....................................................
CONSIDERED
TRAFFIC AURALS ON/OFF Switch ......................................... CONSIDERED
2.3 VISUAL/AURAL TRAFFIC ALERT
Traffic Alert Annunciation and Aural
Traffic……………….………………………….…….
VISUALLY ACQUIRE
Section 3. EMERGENCY PROCEDURES
3.1 Emergency Procedures
None.
Section 4. MALFUNCTION PROCEDURES
4.1 Malfunction Indications
The loss of a required input to the GDL 84H/88H may cause the GDL 84H/88H
to stop transmitting ADS-B Out data or providing ADS-B In functions.