Garmin GDL 84H, Rotorcraft Flight Manual Supplement

Page: 11 / 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 11 of 16

Winds Aloft

Aviation Data

TFRs

NOTAMs
Capabilities
As installed in this rotorcraft, the Garmin GDL 84H/88H system complies with
the requirements of AC 20-165A.
The GDL 84H/88H ADS-B OUT system has been shown to meet the equipment
requirements of 14 CFR 91.227
The GDL 88H meets the requirements of TSO-C195a Class C1, C2, C3, C5,
TIS-B Services TSO-C166b Class A1, and FIS-B TSO-C157a for ADS-B In
Operation and AC 20-172A for Airworthiness Approval for ADS-B In Systems
and Applications
Installation Configuration
This rotorcraft is equipped with a GDL 84H/88H system with the following
interfaces/ features (appropriate boxes will be checked):
Equipment Installed:

GDL 84H

GDL 88H
Interfaced Active Traffic System (GDL 88H Only):

Yes

No
Interfaced Heading Source(s):

Yes

No
PABI Control

External Switch

Transponder control (move from ALT to ON)

Controlled via display